rexresearch.com
Bruno MICHEL, et al.
High-Concentration Photovoltaic-Thermal System
Concentrates sunlight 2000x, converts 80%
to useful energy, desalinates water, & refridgerates...
http://www-03.ibm.com/press/us/en/pressrelease/40912.wss#release
ZURICH - 22 Apr 2013: Today on Earth Day, scientists have
announced a collaboration to develop an affordable photovoltaic
system capable of concentrating solar radiation 2,000 times and
converting 80 percent of the incoming radiation into useful
energy. The system can also provide desalinated water and cool air
in sunny, remote locations where they are often in short supply.
A three-year, $2.4 million (2.25 million CHF) grant from the Swiss
Commission for Technology and Innovation has been awarded to
scientists at IBM Research (NYSE: IBM); Airlight Energy, a
supplier of solar power technology; ETH Zurich (Professorship of
Renewable Energy Carriers) and Interstate University of Applied
Sciences Buchs NTB (Institute for Micro- and Nanotechnology MNT)
to research and develop an economical High Concentration
PhotoVoltaic Thermal (HCPVT) system.
Based on a study by the European Solar Thermal Electricity
Association and Greenpeace International, technically, it would
only take two percent of the solar energy from the Sahara Desert
to supply the world's electricity needs*. Unfortunately, current
solar technologies on the market today are too expensive and slow
to produce, require rare Earth minerals and lack the efficiency to
make such massive installations practical.
The prototype HCPVT system uses a large parabolic dish, made from
a multitude of mirror facets, which are attached to a sun tracking
system. The tracking system positions the dish at the best angle
to capture the sun's rays, which then reflect off the mirrors onto
several microchannel-liquid cooled receivers with triple junction
photovoltaic chips -- each 1x1 centimeter chip can convert 50
watts, on average, over a typical eight hour day in a sunny
region.
The entire receiver combines hundreds of chips and provides 25
kilowatts of electrical power. The photovoltaic chips are mounted
on micro-structured layers that pipe liquid coolants within a few
tens of micrometers off the chip to absorb the heat and draw it
away 10 times more effectively than with passive air cooling.
The coolant maintains the chips almost at the same temperature for
a solar concentration of 2,000 times and can keep them at safe
temperatures up to a solar concentration of 5,000 times.
The direct cooling solution with very small pumping power is
inspired by the hierarchical branched blood supply system of the
human body and has been already tested by IBM scientists in high
performance computers, including Aquasar. An initial demonstrator
of the multi-chip receiver was developed in a previous
collaboration between IBM and the Egypt Nanotechnology Research
Center.
"We plan to use triple-junction photovoltaic cells on a
micro-channel cooled module which can directly convert more than
30 percent of collected solar radiation into electrical energy and
allow for the efficient recovery of an additional 50 percent waste
heat," said Bruno Michel, manager, advanced thermal packaging at
IBM Research. "We believe that we can achieve this with a very
practical design that is made of lightweight and high strength
concrete, which is used in bridges, and primary optics composed of
inexpensive pneumatic mirrors -- it's frugal innovation, but
builds on decades of experience in microtechnology.
"The design of the system is elegantly simple," said Andrea
Pedretti, chief technology officer at Airlight Energy. "We replace
expensive steel and glass with low cost concrete and simple
pressurized metalized foils. The small high-tech components, in
particular the microchannel coolers and the molds, can be
manufactured in Switzerland with the remaining construction and
assembly done in the region of the installation. This leads to a
win-win situation where the system is cost competitive and jobs
are created in both regions."
The solar concentrating optics will be developed by ETH Zurich.
"Advanced ray-tracing numerical techniques will be applied to
optimize the design of the optical configuration and reach uniform
solar fluxes exceeding 2,000 suns at the surface of the
photovoltaic cell," said Aldo Steinfeld, Professor at ETH Zurich.
With such a high concentration and a radically low cost design
scientists believe they can achieve a cost per aperture area below
$250 per square meter, which is three times lower than comparable
systems. The levelized cost of energy will be less than 10 cents
per kilowatt hour (KWh). For comparison, feed in tariffs for
electrical energy in Germany are currently still larger than 25
cents per KWh and production cost at coal power stations are
around 5-10 cents per KWh.
Water Desalination and Cool Air
Current concentration photovoltaic systems only collect electrical
energy and dissipate the thermal energy to the atmosphere. With
the HCPVT packaging approach scientists can both eliminate the
overheating problems of solar chips while also repurposing the
energy for thermal water desalination and adsorption cooling.
To capture the medium grade heat IBM scientists and engineers are
utilizing an advanced technology they developed for water-cooled
high performance computers, including Aquasar and SuperMUC. With
both computers water is used to absorb heat from the processor
chips, which is then used to provide space heating for the
facilities.
"Microtechnology as known from computer chip manufacturing is
crucial to enable such an efficient thermal transfer from the
photovoltaic chip over to the cooling liquid," said Andre Bernard,
head of the MNT Institute at NTB Buchs. "And by using innovative
ways to fabricate these heat transfer devices we aim at a
cost-efficient production."
In the HCPVT system, instead of heating a building, the 90 degree
Celsius water will be used to heat salty water that then passes
through a porous membrane distillation system where it is
vaporized and desalinated. Such a system could provide 30-40
liters of drinkable water per square meter of receiver area per
day, while still generating electricity with a more than 25
percent yield or two kilowatt hours per day -- a little less than
half the amount of water the average person needs per day
according to the United Nations**, but a large installation could
provide enough water for a town.
Remarkably, the HCPVT system can also provide air conditioning by
means of a thermal driven adsorption chiller. An adsorption
chiller is a device that converts heat into cooling via a thermal
cycle applied to an absorber made from silica gel, for example.
Adsorption chillers, with water as working fluid, can replace
compression chillers, which stress electrical grids in hot
climates and contain working fluids that are harmful to the ozone
layer.
Scientists envision the HCPVT system providing sustainable energy
and potable water to locations around the world including southern
Europe, Africa, Arabic peninsula, the southwestern part of the
United States, South America, and Australia. Remote tourism
locations are also an interesting market, particularly resorts on
small islands, such as the Maldives, Seychelles and Mauritius,
since conventional systems require separate units, with consequent
loss in efficiency and increased cost.
A prototype of the HCPVT system is currently being tested at IBM
Research - Zurich. Additional prototypes will be built in Biasca
and Rueschlikon, Switzerland as part of the collaboration.
http://www.youtube.com/watch?v=J_zzE8xMdZc
Bruno Michel, a research scientist at IBM Research - Zurich,
explains his latest invention--a technique for concentrating solar
radiation to create a much more effective system for harvesting
energy from the sun. His hope is that this technique will prove to
be so successful that we'll be able to use it to replace all
fossil fuel and nuclear energy with solar. The work is being done
in conjunction with the Egypt Nanotechnology Center:
http://www.egnc.gov.eg
On Earth Day 2013 scientists announced a collaboration to develop
an affordable photovoltaic system capable of concentrating, on
average, the power of 2,000 suns, with an efficiency that can
collect 80 percent of the incoming radiation and convert it to
useful energy. The proposed system can be built anywhere
sustainable energy, drinkable water and cool air are in short
supply at a cost of three times lower than comparable systems.
PATENTS
PHOTOVOLTAIC THERMAL HYBRID SYSTEMS AND
METHOD OF OPERATION THEREOF
US2013255753
A method is disclosed for operating a photovoltaic thermal hybrid
system having a hybrid solar receiver with a photovoltaic module,
operatively coupled to the system to deliver an electrical output
power for a power user, a thermal collector distinct from the
photovoltaic module, wherein the photovoltaic module and/or the
thermal collector are movably mounted in the system, a collector
thermal storage thermally connected to the thermal collector to
store heat collected at the thermal collector, and a positioning
mechanism adapted to move the photovoltaic module and/or the
thermal collector. The method includes instructing the positioning
mechanism to move the photovoltaic module and/or the thermal
collector to change a ratio of an intensity of radiation received
at the photovoltaic module to an intensity of radiation received
at the thermal collector.
BACKGROUND
[0002] The present invention generally relates to photovoltaic
thermal hybrid solar systems and methods of operation thereof.
[0003] Definitions of certain terms discussed herein are as
follows:
[0004] Photovoltaics (PV) generate electrical power by converting
solar radiation into direct current electricity through
semiconductors exhibiting the photovoltaic effect;
[0005] A photovoltaic cell (or PV cell, also "solar cell" or
"photoelectric cell") is a solid state device that converts energy
of light directly into electricity by virtue if the photovoltaic
effect;
[0006] A photovoltaic module (also "solar module", "solar panel"
or "photovoltaic panel") is an assembly of connected photovoltaic
cells;
[0007] A photovoltaic system typically includes an array of
photovoltaic modules, an inverter and interconnection wiring;
[0008] A thermal collector (also "solar thermal collector")
collects heat by absorbing radiations, such as sunlight;
[0009] A heat exchanger is a device/piece of equipment to
efficiently transfer heat from one medium to another;
[0010] In electronic systems, a heat sink is a component to cool a
device by dissipating heat into a surrounding medium;
[0011] Solar thermal energy (STE) concerns technologies for
harnessing solar energy for thermal energy (heat). STE differs
from and is acknowledged to be much more efficient than
photovoltaics, which converts solar energy directly into
electricity;
[0012] Concentrated solar power (also "concentrating solar power"
or CSP) systems use mirrors or lenses that concentrate a large
area of solar thermal energy onto a small area, such that
electrical power (also "power") can be produced when concentrated
light is converted to heat, which drives a heat engine (e.g., a
steam turbine) connected to a power generator. Common forms of
concentration are: parabolic trough, dish Stirlings, concentrating
linear Fresnel reflector and solar power tower.
[0013] Concentrated photovoltaic (CPV) systems use optics (e.g.,
lenses) to concentrate a large amount of sunlight onto a small
area of solar photovoltaic materials to generate electricity.
Concentration allows for production of smaller areas of solar
cells.
[0014] CPV should not to be confused with CSP: in CSP concentrated
sunlight is converted to heat, and then heat is converted to
electricity, whereas in CPV concentrated sunlight is converted
directly to electricity using the photovoltaic effect;
[0015] Photovoltaic thermal hybrid solar collectors (also "hybrid
PV/T systems" or PVT) are systems converting solar radiation into
thermal and electrical energy. Such systems combine a photovoltaic
cell, which converts photons into electricity, with a solar
thermal collector, which captures the remaining energy and removes
waste heat from the PV module. Two categories of PVT collectors
are generally known:
[0016] PV/T fluid collector (air or liquid). In liquid collectors,
a typical water-cooled design uses conductive-metal piping or
plates attached to the back of a PV module. The working fluid is
typically water or glycol. The heat from the PV cells are
conducted through the metal and absorbed by the working fluid,
which assumes that the working fluid is cooler than the operating
temperature of the cells. In closed-loop systems this heat is
either exhausted (to cool it) or transferred at a heat exchanger,
where it flows to its application. In open-loop systems, this heat
is used, or exhausted before the fluid returns to the PV cells;
[0017] PV/T concentrator (CPVT), wherein a concentrating system is
provided to reduce the amount of solar cells needed. CPVT can
reach very good solar thermal performance compared to flat PV/T
collectors. However, main obstacles to CPVT are to provide good
cooling of the solar cells and a durable tracking system.
[0018] A disadvantage of PV systems compared to other energy
sources is the unpredictable nature of the direct solar radiation.
This leads to intermittent power delivery, which has much less
value than on demand power and leads to grid instabilities.
Storage of electrical energy in e.g. batteries is prohibitively
expensive so that the cost for a storage unit for a full day
production costs much more than the solar power station.
Concentrated solar power systems (CSP) that can store the
collected heat can produce electricity on demand until the stored
heat is dissipated. Concentrated photovoltaic (CPV) power plants
have higher conversion efficiencies than PV and CSP but still
suffer from intermittent power production. Concentrated
photovoltaic thermal (CPVT) systems have a higher system
efficiency because of the improved cooling but reject the heat to
the ambient or produce low grade heat with limited utility.
SUMMARY
[0019] In one embodiment, a method is disclosed for operating a
photovoltaic thermal hybrid system having a hybrid solar receiver
with a photovoltaic module, operatively coupled to the system to
deliver an electrical output power for a power user, a thermal
collector distinct from the photovoltaic module, wherein the
photovoltaic module and/or the thermal collector are movably
mounted in the system, a collector thermal storage thermally
connected to the thermal collector to store heat collected at the
thermal collector, and a positioning mechanism adapted to move the
photovoltaic module and/or the thermal collector. The method
includes instructing the positioning mechanism to move the
photovoltaic module and/or the thermal collector to change a ratio
of an intensity of radiation received at the photovoltaic module
to an intensity of radiation received at the thermal collector.
[0020] In another embodiment, a photovoltaic thermal hybrid system
includes a hybrid solar receiver, having a photovoltaic module
designed for electrical output power delivery; a thermal collector
distinct from the photovoltaic module, wherein the photovoltaic
module and/or the thermal collector are movably mounted in the
system; a collector thermal storage thermally connected to the
thermal collector to store heat collected at the thermal
collector; a positioning mechanism adapted to move the
photovoltaic module and/or the thermal collector; and a control
unit configured to instruct the positioning mechanism to move the
photovoltaic module and/or the collector to change a ratio of an
intensity of radiation received at the photovoltaic module to an
intensity of radiation received at the thermal collector.
BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS
[0021] FIG. 1 shows an exploded 3D view of a multilayer
cooling device for a photovoltaic device;
[0022] FIG. 2 focuses on a specific channel portion
pattern, designed for a given layer of the device of FIG. 1;
[0023] FIG. 3 depicts a 3D tree structure representing an
arrangement of orifices and channel portions of a cooling
device;
[0024] FIG. 4 shows a side view of a photovoltaic device
mounted on a cooling device;
[0025] FIG. 5 is a 3D view of such a photovoltaic device,
mounted on a cooling device;
[0026] FIG. 6 is a 3D view of a thermal collector for a
photovoltaic device;
[0027] FIG. 7 is a partial view of FIG. 6, showing a
section of the thermal collector;
[0028] FIG. 8 is a section view of a photovoltaic thermal
hybrid solar receiver;
[0029] FIG. 9 is a section view of another photovoltaic
thermal hybrid solar receiver;
[0030] FIG. 10 is a side view of a photovoltaic thermal
hybrid solar system;
[0031] FIG. 11 is a flowchart of steps implemented in
methods of operation of a photovoltaic thermal hybrid solar
system such as depicted in FIG. 10;
[0032] FIGS. 12-13 are simplified representations of
photovoltaic thermal hybrid solar systems;
[0033] FIGS. 14-15 are block diagram representations of
additional photovoltaic thermal hybrid solar devices-based
systems;
[0034] FIG. 16 is a graph showing the radiation intensity
distribution at the level of an input plane of a hybrid
receiver, while displacing the hybrid receiver along the optical
axis of the system;
[0035] FIG. 17 is a graph showing the total irradiance
captured by a thermal collector and a PV chip of a hybrid
receiver, while displacing the hybrid receiver along the optical
axis of the system;
[0036] FIG. 18 is a graph comparing dispatched delivery of
electrical power by various CPVT systems;
[0037] FIG. 19 is a simplified representation of a system
for short-term local weather prediction using tracker solar
sensor information; and
[0038] FIG. 20 schematically depicts an example of a
control system-a computerized unit, suitable for implementing
steps of methods of operation of systems such as depicted in
FIGS. 10, 12-15, and 19.
DETAILED DESCRIPTION
[0039] According to a first aspect, a method of operating a
photovoltaic thermal hybrid system is disclosed, the latter
comprising a hybrid solar receiver, having a photovoltaic module,
operatively coupled to the system to deliver an electrical output
power for a power user; and a thermal collector distinct from the
photovoltaic module, wherein the photovoltaic module and/or the
thermal collector are movably mounted in the system; and a
collector thermal storage thermally connected to the thermal
collector to store heat collected at the thermal collector; and
positioning mechanism adapted to move the photovoltaic module
and/or the thermal collector. The method includes: instructing the
positioning mechanism to move the photovoltaic module and/or the
thermal collector to change a ratio of an intensity of radiation
received at the photovoltaic module to an intensity of radiation
received at the thermal collector.
[0040] Embodiments of the invention may include one or more of the
following features: the method further includes receiving data
indicative of an electrical power demand; and instructing the
positioning mechanism is carried out based on a comparison of the
output power with the power demand; instructing the positioning
mechanism includes instructing the positioning mechanism to move
the photovoltaic module and/or the thermal collector to decrease
the ratio if the comparison indicates that the output power is
larger than the power demand; the method further includes
instructing to deliver an output power generated by the
photovoltaic module to a power user, to meet the power demand if
the output power matches the power demand. The system further
includes a heat engine, thermally connected to the collector
thermal storage, the method further comprising instructing the
heat engine to start a process of thermal-to-electrical conversion
of heat stored in the collector thermal storage if an output power
generated by the photovoltaic device is lower than the power
demand. The method further includes: instructing to trigger a
desalination process and/or an adsorption cooling process, in
order to dissipate heat from the collector thermal storage. The
system further includes: a first heat circuit connecting the
photovoltaic module to a photovoltaic thermal storage distinct
from the collector thermal storage, to cool the photovoltaic
module; and a second heat circuit, distinct from the first heat
circuit, and connecting the collector thermal storage to the
thermal collector.
[0041] The system further includes a heat exchanger, thermally
connected to the photovoltaic thermal storage, and the method
further includes instructing to provide heat stored in the
photovoltaic thermal storage to a thermal user via the heat
exchanger; in the system, the heat exchanger is further thermally
connected to the collector thermal storage, the method further
comprising instructing to provide additional heat stored in the
collector thermal storage to the heat exchanger while providing
heat stored in the photovoltaic thermal storage to the thermal
user via the heat exchanger. The system further includes an
additional heat exchanger thermally connected to the heat engine
and a given thermal user, the given thermal user being further
thermally connected to the photovoltaic thermal storage or to both
the photovoltaic thermal storage and the collector thermal
storage, via the heat exchanger, and the method further includes
instructing the heat engine to start a process of
thermal-to-electrical conversion of heat stored in the collector
thermal storage using the given thermal user as a low temperature
pool. In the system, a temperature in the collector thermal
storage is substantially larger than a temperature in the
photovoltaic thermal storage, preferably by more than 30[deg.] C.,
more preferably by more than 50[deg.] C.; in the system, the
photovoltaic thermal hybrid solar receiver is movably mounted in
the system, such that the positioning mechanism can move the
photovoltaic thermal hybrid solar receiver as a whole;
[0042] In the system, the thermal collector extends in a first
plane and includes an aperture; and the photovoltaic module
includes a photo-active area within an area of the photovoltaic
module that extends in a second plane, at a distance of the
aperture, the photo-active area being vis-à-vis the aperture, a
projection of the aperture perpendicularly to the second plane
essentially corresponding to the photo-active area, and the
thermal collector further preferably includes one of or both the
following components: one or more minor elements provided in an
intermediate section between the first plane and the second plane,
the mirror elements preferably thermally connected to the
collector thermal storage, by a same heat circuit that connects
the thermal collector to the collector thermal storage; and a band
pass filter arranged at the level of the aperture;
[0043] The system further includes a concentrator, arranged to
concentrate radiation towards an optical focus thereof, and the
positioning mechanism is adapted to move the photovoltaic module
in or out of the optical focus.
[0044] According to another aspect, the invention is embodied as a
photovoltaic thermal hybrid system, comprising: (i) an hybrid
solar receiver, having a photovoltaic module designed for
electrical output power delivery and a thermal collector distinct
from the photovoltaic module, wherein the photovoltaic module
and/or the thermal collector are movably mounted in the system;
(ii) a collector thermal storage thermally connected to the
thermal collector to store heat collected at the thermal
collector; and (iii) positioning mechanism adapted to move the
photovoltaic module and/or the thermal collector; and further
comprising (iv) a control unit configured to instruct the
positioning mechanism to move the photovoltaic module and/or the
collector to change a ratio of an intensity of radiation received
at the photovoltaic module to an intensity of radiation received
at the thermal collector, e.g., based on a comparison of the
output power with a power demand as received at the control unit.
[0045] Devices, systems, methods of operating such devices and
systems, as well as computer program functions partly implementing
embodiments of the present invention will now be described, by way
of non-limiting examples, and in reference to the accompanying
drawings.
[0046] The present invention forms part of comprehensive CPVT
solutions. Such solutions revolve around novel photovoltaic
thermal hybrid receivers. Aspects of these solutions concern such
receivers, cooling devices for such receivers, photovoltaic
thermal hybrid systems and operation methods.
[0047] The present invention proposes novel systems and methods
for operating a photovoltaic thermal hybrid system. Such systems
and methods rely on a hybrid solar receiver, equipped with a
photovoltaic (or PV) module capable of delivering an electrical
output power, and a thermal collector distinct from the PV module.
The PV module and/or the thermal collector are movably mounted in
the system. Furthermore, a collector thermal storage is
(thermally) connected to the thermal collector, in order to store
heat collected at the latter. In addition, positioning mechanism
are provided, which are adapted to move the PV module and/or the
thermal collector. Then, instructing the positioning mechanism to
move the PV module and/or the thermal collector results in
changing the ratio of the intensity of radiation received at the
PV module to the intensity received at the thermal collector.
Thus, excess radiation received at the PV module (i.e., larger
than necessary to meet a power demand) can advantageously be used
to heat up the thermal circuit and store heat at the thermal
storage.
[0048] The accompanying drawings are organized as follows:
[0049] Cooling devices 25 such as depicted FIG. 1-4 can
advantageously be used to cool PV receivers, as shown in FIGS. 4
and 5. PV receivers 21 can advantageously be complemented by
thermal collectors 22 such as depicted in FIGS. 6, 7. This results
in hybrid receivers such as depicted in FIGS. 8, 9. The hybrid
receivers can in turn be used in systems 10 such as depicted in
FIGS. 10, 12-15.
[0050] The systems 10 can be complemented to enable short-term
weather prediction, FIG. 19. The above systems 10 can be operated
according to a method such as captured in the flowchart of FIG.
11. A control system to implement such a method is depicted in
FIG. 20.
[0051] In FIGS. 1-5, the following notations are used:
[0052] Ll denotes the ithlevel out of L total levels;
[0053] At level 1: Oih denotes the hthorifice of the inlet circuit
(Ooh is its counterpart for the outlet circuit);
[0054] Similarly, CPih represents the hthchannel portion of the
inlet circuit, (CPoh pertains to the outlet circuit). For example,
CPi1 denotes the first channel portion of the inlet circuit, at
level 1;
[0055] At level 2: Ohihk represents the kthorifice arising from
CPih; CPohk denotes the corresponding channel portion;
[0056] At level 3: Oihkl represents the lthorifice arising from
CPihk, CPihkl denotes the corresponding channel portion, etc.
[0057] The number of indices hkl . . . used to tag a particular
orifice or channel portion corresponds to the level that the
orifice or channel belongs to. For example, Oihk belongs to level
2, while Oihkl belongs to level 3.
[0058] Referring to FIGS. 1-5 in general and more particularly to
FIGS. 1 and 3, a chip module cooling device (or cooler) 25 as
involved in embodiments includes two fluid circuits: an inlet
fluid circuit i and an outlet fluid circuit o. Each circuit
includes an arrangement of orifices Oi, Oo and channel portions
CPi, CPo. The orifices are also referred to as nozzles in some
places below: they can indeed be given various appropriate shapes
such as injection nozzles. This arrangement can be regarded as
forming (or reflecting) a tree structure. An example of such a
tree structure is depicted in FIG. 3, wherein: branches represent
the orifices Oi, Oo and nodes represent the channel portions CPi,
CPo.
[0059] As generally known in tree structures, a branch links a
node to one child node only; nodes sharing a same parent node are
called siblings, or sibling nodes. Thus, channel portions
corresponding to sibling nodes may be called sibling channel
portions.
[0060] Each fluid circuit extends through L levels (i.e., L1 to L3
in FIG. 1) of the tree structure. The concept underlying the
present cooling devices requires at least L>3 levels. L can be
larger, see e.g., FIG. 3. In FIG. 1, level L4 could be regarded as
an additional level of the tree structure. However, L4 includes a
modified orifice structure; it further includes channel portions
of a heat exchanger, which shall be described later.
[0061] The circuits connect to each other at (or after) a final
level (i.e., a lowest level of the tree structure), via channel
portions corresponding to leaf nodes of the tree structure. The
connection of the fluid circuits can be realized directly via the
final "leaf" channel portions, or not. The connection may for
instance involve additional orifices or any sort of connecting
structure (channels, slits, etc.) "after" the leaf channel
portions in the tree structure. Examples are given below. The
additional mechanism need not be reflected in the above tree
structure. Fluid communication from the inlet to the outlet fluid
circuit is nonetheless enabled via a lowest level of the tree.
[0062] Now, for each of the two fluid circuits, the channel
portions corresponding to sibling nodes have to fulfill two
conditions:
[0063] First, they are parallel to each other, i.e., the principal
directions (or lines) of extension of sibling channel portions are
parallel to each other. Parallel is here to be understood
according to Euclid's definition of parallelism, i.e., it means
strictly parallel and refers to two parallel distinct channel
portions. In the example of FIG. 1, it can be seen that sibling
channel portions are parallel; this for example is the case:
[0064] At level 2 (L2): for channel portions CPi11, CPi12, and
CPi13 for inlet circuit i. The same occurs for the corresponding
outlet channel portions CPo11, CPo12, and CPo13; or
[0065] At level 3 (L3) : for channel portions CPo131, CPo132,
etc.;
[0066] Note that at level 1 (L1), there is only one channel
portion (CPi1 or CPo1) per circuit (i or o), forming only one
channel.
[0067] Second, channel portions corresponding to sibling nodes
extend along respective directions, none of which is parallel to
the direction of extension of the channel portion corresponding to
the parent node (compare e.g., L3-channel portions to L2-channel
portions or L2-channel portions to L1-channel portions).
[0068] Provided that the directions do not intersect either (which
shall improve compactness in fine), it follows that, each of the
channel portions corresponding to sibling nodes extends along a
direction which, together with a direction of extension of their
parent node, form a pair of skew lines. This condition could be
fulfilled at a given level, preferably more, of the tree structure
and for each of the two fluid circuits. Siblings may span a plane
parallel to the parent node of the sibling nodes. A sibling can
thus be described as being "rotated", preferably by 90[deg.] (as
is the case in FIG. 1 or 3), with respect to their parent channel
portion. The extent of the rotation depends on the pattern drawn
by the orifices, as to be explained in detail below.
[0069] Channel portions may advantageously fulfill the additional
conditions below:
[0070] Third, the channel portions corresponding to sibling nodes
are preferably strictly parallel to channel portions corresponding
to a grandparent node of the sibling nodes, if any. This is
notably the case in FIG. 1 for all L3-channel portions (CPo131,
CPo132, etc.) that are parallel to CPo1 or CPi1 of level 1. It can
be realized that this third condition allows for improved
compactness, simplifies the design and thus eases the manufacture
of the device, all the more if L>3. However, this is not a
strict condition (especially if L=3). For example, L3-channel
portions could extend not parallel to their L1-grand-parent
channel portions, without critically impacting essential
properties of the device. This could for instance be the case if
other constraints (components, manufacture) oblige to shift
grand-parent channel portions from their ideal direction of
extension.
[0071] Fourth, channel portions corresponding to sibling nodes
preferably span a plane parallel to channel portions corresponding
to a parent node. Again, this may improve compactness and/or
simplify the design and manufacture. This fourth condition is
however not strict as the parent channel portions could extend in
a same plane as the sibling channel portions (though rotated with
respect to the latter). In particular, in FIG. 1, it can be seen
that:
[0072] Channel portions CP,i11, CPi12, and CPi13 are open on an
upper plane of component 211, which upper plane is (strictly)
parallel to the main direction of extension of channel portion
CPi1 (the parent node of CPi11, CPi12, and CPi13).
[0073] However, the main direction of extension of CPi1 is close
to or can even be included in the average plane spanned by the
main directions of extension of CPi11, CPi12, and CPi13. Because
there are only one inlet channel and one outlet channel at level
1, the latter can nonetheless be easily integrated in a same
device block 251 as their child channel portions. Yet, because of
the layer structure adopted in the example of FIG. 1, channel
portions of level 3 do not belong to the same layer as the channel
portions of level 2. Channel portions corresponding to sibling
nodes of level 3 now span a plane strictly parallel to channel
portions corresponding to a parent node. Thus, one understands
that sibling channel portions may advantageously span a plane
parallel to their parent, subject to other constraints.
[0074] Finally, channel portions of the inlet circuit (for example
CPi11, CPi12, and CPi13) are parallel to and interdigitated with
channel portions of the outlet circuit (for example CPo11, CPo12,
and CPo13). Interdigitation means an interlinking, evoking fingers
of two hands locked together, as illustrated in FIG. 1 or FIG. 3.
Owing to the conditions that the device already fulfills,
Interdigitation involves channel portions corresponding to a same
level of the tree structure.
[0075] A similar arrangement is shown in FIG. 3. What FIG. 3
actually depicts is a 3D tree structure, i.e., a tree abstraction,
representing an arrangement of orifices and channel portions.
However, it should be realized that a cooling device may be
embodied with a geometry of channels as depicted in FIG. 3. In
FIG. 3, for each of the inlet/outlet fluid circuits (i, o),
channel portions corresponding to sibling nodes fulfill the same
conditions as described earlier. Namely:
[0076] First, siblings are parallel to each other, as for example
is the case for: Channel portions CPi11 and siblings; the same
occurs for their outlet counterparts (channel portions are not all
referenced, for clarity); or Channel portions CPi111 and parallel
siblings; and again, at level 1, there is only one channel portion
CPi1 for the inlet circuit (and similarly for the outlet circuit).
Second, they are not parallel to channel portions corresponding to
a parent node of the sibling nodes (compare e.g., CPi111 to
CPi11); they are instead rotated by 90[deg.]. Third, siblings are
further parallel to channel portions corresponding to a
grandparent node of the sibling nodes. This is notably the case
for all channel portions of level 3 (CPi111 and siblings, inlet
circuit) that are parallel to their unique grand-parent channel
(CPi1, level 1, inlet circuit). Fourth, channel portions
corresponding to sibling nodes (e.g., CPi11 and siblings, inlet
circuit) span a plane, which, in the embodiment of FIG. 3, is
strictly parallel to channel portions corresponding to a parent
node (e.g., CPi1, inlet circuit).
[0077] A structure such as described above allows for achieving a
dense and homogeneous arrangement of channels at the heat exchange
level, i.e., "after" the leaf level. In some cases at least, the
third condition above further improves final compactness. The
fourth condition may be omitted, depending on the number of
grand-parents. Interdigitation results in a homogeneous
distribution of channels and allows for minimizing fluid
trajectory. The fractal-like pattern that results from channel
subdivisions and rotations makes it possible, notably, to optimize
heat exchange. In addition, particular implementations allow for
minimizing the required pumping power for the coolant flow.
Detailed examples are given below.
[0078] In addition, such a structure and its building principle
are easily scalable, which is advantageous for e.g., multichip
photovoltaic cells as the dimensions of the latter can
substantially exceed typical integrated circuit (IC) chips.
[0079] Tests performed by the present inventors have shown that
usual chip cooling devices (wherein fluid circuits can be seen as
subdividing into a single level of multiple nozzles/channels) can
be successfully used to cool down classical IC chips, without
unreasonable pumping effort. Scalability is therefore not an issue
for cooling classical IC chips. Now, classical IC chip cooling
devices are not suitably dimensioned for multichip photovoltaic
cells. Should one nonetheless want to use classical cooling
devices for (larger) multichip photovoltaic devices, one may first
be tempted to parallelize such classical cooling devices, owing to
the dimensions of multichip photovoltaic devices compared to usual
IC chips. However, experiments have shown that this is
inappropriate, because some regions of the multichip photovoltaic
devices shall not be satisfactorily cooled, due to the
inhomogeneous cooling obtained by the parallel cooling devices.
Next, should one want to scale a classical IC chip cooling device
to typical multichip photovoltaic device's dimensions (wherein
dimensions are likely multiplied by a factor >5 compared to a
typical IC chip), another issue arises. In that case, present
inventors have realized that scaled cooling devices require a
(too) large pumping effort.
[0080] On the contrary, a cooling device comprising a multilevel
and interdigitated arrangement of orifices/channel portions as
described earlier is scalable, by construction. Such a building
principle further allows for reaching a dense arrangement of
channel portions at the leaf level, owing to the successive
rotations of channel portions. Dimensions of cross-sections of
both the channels and nozzles shall likely decrease from one level
to the other, as the number of channel portions and nozzles
increases from one level to the other. It can be realized that the
height of the channels is not that critical: for instance, in
embodiments, the height of the channels extends perpendicularly to
the thickness of a layer wherein the channel is provided. However,
the width of the channel portions (in the cross-section,
perpendicular to the in-channel flow direction) shall typically
decrease. In other words, if the density of the channels is
maximal at level n, the channel sections shall likely be larger at
level n-1 than at level n. A structure as described above allows
for reducing the flow path to and within the heat transfer
structure; it further allows for scalability while keeping a
moderate pumping effort.
[0081] Typically, each of the two fluid circuits includes, at each
level Ll (1<=l<=L-1):
Nl orifices (or nozzles), each leading to a respective channel
portion. An orifice typically branches in the middle of the
respective channel portion, except at edges of the device. Other
branching geometry can be contemplated, which however are expected
to be less efficient; and
Nl parallel channel portions. In turn, each of the Nl channel
portions shall enable fluid distribution to Bl+1 orifices of the
next level Ll+1, where Bl+1 is a branching factor, defined by
Bl+1=Nl+1/Nl. Successive subdivisions of the channel circuits
require B2>=2 and B3>2; B1 can be assumed to be equal to 1.
For example, in FIG. 3:
[0084] Oi1 leads to CPi1 (level 1, B1=1);
[0085] CPi1 subdivides via Oi11, Oi12 and Oi13 into respective
channel portions (CPi11 and siblings, level 2, B2=3);
[0086] Each of the L2-channel portions (CPi11 and siblings) leads
to four channel portions. For example, CPi11 leads to CPi111 (via
Oi111), as well as to three other parallel channel portions
(siblings) via respective orifices; CP112 leads to CPi121 as well
as to three other parallel channel portions (siblings), etc. Thus,
at level 2: each channel portion of the inlet circuit enables
fluid distribution to B3=4 inlet orifices (e.g., Oi11k, k=1, 2, 3,
4) of the next level L3. The same holds for channel portions of
the outlet fluid circuit.
[0087] In other words, the tree structure underlying each fluid
circuit is typically balanced, as i1lustrated in FIG. 3, i.e., the
branching factor Bm+1 is preferably the same for each channel
portion at a given level Lm, whereby both the design and the
manufacture of the device are made easier.
[0088] Next, the arrangement of orifices/channel portions can be
designed such that each circuit has exactly the same geometry,
which simplifies the manufacture and assembly of the device.
Meanwhile, the arrangement can be designed to optimize the fluid
distribution at a leaf level, i.e., in the vicinity of the heat
exchanger. One possibility is to have, at a given level Lm
(2<=m<=L), the positions of orifices of one fluid circuit
correspond to a first set of discrete points of a first finite
array. In analogy with 2D crystallography, this first array may be
regarded as generated by a set of discrete translations R, i.e.,
defined by R=n1a1+n2 a2, where n1 and n2 are integers and a1 and
a2 are linearly independent vectors (as defined in linear
algebra). Channel portions at level Lm-1 extend along or parallel
to a1 and channel portions at levels Lm extend along or parallel
to a2. Finally, the positions of orifices of the other fluid
circuit may correspond to second set of discrete points of a
second finite array, translated from the first array by a
translation r defined by r=x1a1+x2a2, with 0<x1<1 and
0x2<1. Preferably, on chooses x1=x2=1/2, which optimizes the
homogeneity of the fluid distribution at the level of the heat
exchange. Choosing x1or x2<>1/2 would instead induce
heterogeneity in the set of trajectories throughout the fluid
structure and therewith would cause heterogeneous fluid
distribution within the heat exchanger, resulting in heterogeneous
cooling. Note that for m<=L-1, we have 0<x1<1 and
0<x2<1, while for m=L, we have 0<=x1<1 and
0<x2<1 or 0<=x1<1 and 0<=x2<1. Also, as a
consequence of the above arrangement, the N1 channel portions at
level L1 are rotated with respect to channel portions of the
next/previous level, typically by an angle [alpha]=[pi]/2 for a
square lattice, as illustrated in FIG. 3.
[0089] Should the basis unit of the lattice differ (e.g., oblique
lattice), then channel portions corresponding to child nodes of a
given parent node would be rotated by an angle [alpha] with
respect to the parent channel portion and grand-child channel
portions would preferably be rotated by an angle [pi]-[alpha], to
be in phase with the parent.
[0090] For example, in FIG. 3, at level L3, the positions of {,
Oi111, Oi121, Oi112, . . . } map onto a first array, generated by
translations R=n1a1+n2a2. Channel portions at level L2 (e.g.,
CPi11 and siblings) extend along or parallel to a1 and channel
portions at levels L3 extend along or parallel to a2. Finally, the
positions of orifices of the other fluid circuit (not referenced
for clarity) correspond to a second set of discrete points of a
second array, at any level. L1 to L3 outlet orifices are
translated from the first array by r=(a1+a2)/2. Next, in order to
take account of edge effects, L3-channel portions are modified:
the leftmost inlet channel portions are reduced (compare CPi111 to
CPi121) and the corresponding orifices branch at one end thereof;
the outlet structure is simply rotated with respect to the inlet
circuit ([pi]-rotation around Oi1) and is still shifted. As a
result, L4 outlet orifices are translated from the first array by
r=a1/2 only, consistently with the fact that for m=L, the
condition for x1 and x2 becomes 0<=x1<1 and 0<x2<1 or
0<x1<1 and 0<=x2<1, as noted above. Such an
arrangement has several advantages: (i) it makes it possible for
the inlet and outlet circuits to have exactly the same structure
(outlet circuit is simply rotated with respect to inlet circuit);
(ii) it furthermore equalizes the fluid trajectories from one
circuit to the other at level 4 (the fluid path length between one
inlet orifice to the closest outlet orifice is ¦a1¦/2; and (iii)
the two circuits have the same footprint (square lattice).
[0091] Next, depending on the orifice arrangement, subsets of
channel portions may rejoin to draw channel lines, at a given
level (e.g., CPi111, CPi121 and CPi131 form one such subset at
level 3 in FIG. 3), or at several levels. Typically, two adjoining
channel portions in any such subset are cousins (e.g., CPi111 and
CPi121). Accordingly, it can be concluded that, in this example,
any two channel portions at any level are either strictly parallel
(like CPi111 and CPi112 siblings) or extend along a same line
(like CPi111 and CPi121 cousins). In that respect, since a line
can be defined by a point and a direction vector and two lines can
be defined as parallel if their direction vectors are, two
identical lines are parallel according to this definition, even if
they are not according to Euclid's definition (where two parallel
distinct lines are called strictly parallel). Thus, any two
channel portions at any level are at least non-strictly parallel.
[0092] Note that a design option such as discussed in the previous
paragraph might be implied by the positions of the orifices, in
particular if the latter map onto an array as discussed above. In
all cases, this design option substantially simplifies the
geometry and manufacture of the cooling device, as subsets of
channel portions extend along a same direction. A given channel
line shall include channel portions arranged in-line, wherein
fluid communication is possibly enabled from one channel portion
to another. Whether to do so shall actually depend on various
parameters, flow rates, channel sections, etc. For example, each
of the fluid circuits i, o may include (at least in one level L1
thereof): N1 channel portions forming Nci strictly parallel
channel lines Ci, Co, wherein each of the Nci channel lines
includes channel portions arranged in-line. In fact, at a given
level, sibling channel portions are strictly parallel (e.g., FIG.
3, CPi111 and CPi112, level 3), but some of the channel portions
that have different parents (e.g., CPi111, CPi121 and CPi131) may
be arranged in-line, resulting in Nci parallel channels (Nc3=4 at
level 3 in the example of FIG. 3). The channel portions arranged
in-line are not necessarily in fluid connection: one may for
example have walls between the channel portions arranged in-line
or the channel portions. Note that one necessarily has
Bl<=Ncl<=Nl, from the above definitions.
[0093] A particularly simple design is obtained by setting Ncl=B1,
whereby Ncl parallel channel lines correspond to Ncl parallel
lines of orifices, as i1lustrated in FIG. 3, level 3. Accordingly,
each of the fluid circuits may include Nl channel portions forming
Bl strictly parallel channel lines. In that case, each channel
line includes Bl-1 channel portions arranged in-line (and this,
possibly at each level Ll). Again, channel portions in a given
channel line may be connected to enable fluid communication from
one channel portion to another. Now, one channel line may include
a unique channel portion. For example, at level 1, one has
Ci1=CPi1, assuming Bo=1 in that case; at level 2, one has
Ci11=CPi11, etc., since B1=1. However, at level 3, there are
Nc3=B3=4 parallel channel lines (for each fluid circuit), which
lines correspond to respective parallel lines of orifices and
include, each, 3 orifices and 3 respective channel portions
(B2=3).
[0094] In addition, it is desirable to further improve the
compactness of the arrangement, to minimize the fluid
trajectories. To that aim, Ncl strictly parallel channel lines Ci
of the inlet fluid circuit may advantageously be interdigitated
with No strictly parallel channel lines Co of the outlet fluid
circuit, at a given level Lm (1<=m<=L). Accordingly, each
channel line of the inlet fluid circuit results to be parallel to
each channel line of the outlet fluid circuit at that level Lm.
Interdigitation of channel lines can actually be provided at
several levels, and more preferably at each level where channel
portions can form channel lines), to increase compactness. In that
respect, it should be borne in mind that FIGS. 1 and 3 depict
simple examples, but additional levels (and layers) of channel
portions may actually be contemplated.
[0095] Next, a specific pattern of channel portions shall be
discussed in reference to FIG. 1 (enlarged "B" area) and FIG. 2
(focusing on the specific pattern shown in the enlarged "B" area,
designed for sublayer sL32 of the device of FIG. 1). Namely, at a
given level Lm and for each of the fluid circuits, at least some
of the Nm channel portions may be designed to have a non-constant
cross-section. As seen in FIG. 2, inlet and outlet channel
portions can be suitably shifted (i.e., interdigitated) to
maintain a compact arrangement (compare e.g., CPi124 to CPo124).
More specifically, the channel portions may, each, include an
enlarged area vis-à-vis a respective one of the Nm orifices, to
improve fluid distribution from/to orifices of the respective
channel portions (at a given level Lm).
[0096] Additional design options can be contemplated, which take
account of edge effects. For example, at a given level Lm (e.g.,
L3 in FIG. 1) two sets of orifices (e.g., Oi11k and Oo13k, k=1, 2,
. . . ), each comprising Bm orifices, are arranged in
correspondence with respective outermost channels (e.g., CPi11 and
CPo13) of a previous level Lm-1. Then, each of the Bm orifices of
the two sets and/or each of their respective channel portions may
have reduced dimensions along a particular direction of extension
of the channels at level Lm (i.e., direction x in FIG. 1).
[0097] The cooling device may further include a heat transfer
structure 24, in addition to a manifold system, to supply and
drain liquid to and from the heat transfer structure, as
i1lustrated in FIG. 1 and FIG. 4. In variants, the heat transfer
structure 24 could be first integrated to a photovoltaic module,
and later be connected to the cooling device. In all cases, the
heat transfer structure 24 can be configured to connect one of the
fluid circuits to the other. The heat transfer structure
preferably includes silicon, and is more preferably entirely made
of silicon, for reasons that will be discussed later.
[0098] The heat transfer structure may for instance include heat
transfer channel portions (e.g., CPt1311, CPt1312 in FIG. 1,
enlarged area "D"). Each of the transfer channel portions connects
at least one channel portion (e.g., CPi131 in FIG. 1)
corresponding to a leaf node of the inlet fluid circuit to one
channel portion (e.g., CPo131 in FIG. 1) corresponding to a leaf
node of the outlet fluid circuit.
[0099] Preferably, each heat transfer channel portion extends
along a direction rotated with respect to a direction of extension
of the channel portions that it connects, following the same
principle as already discussed in respect of the tree-structured
channel portions of the cooling device.
[0100] Similarly, heat transfer channel portions may connect the
lowest-level channel portions via slits (e.g., Si131 and So131 in
FIG. 1), following the same principle as for orifices nozzles
discussed thus far, except that the dimensions typically involved
at the level of the heat transfer structure make it preferable to
have a slit instead of a dense in-line arrangement of orifices,
for manufacturability reasons. Yet, a slit can be seen as the
asymptotic limit of such an arrangement. In that sense, the heat
transfer structure can be regarded as forming or completing an
additional level of the tree structure underlying each fluid
circuit, e.g., level 4 in FIG. 3.
[0101] Next, the cumulated width of all orifices (in
cross-sectional areas) of one of the levels is preferably kept
substantially equal (e.g., to +-15%) to the cumulated width in
cross-sectional area of all orifices of another, e.g., a
contiguous level (and preferably of all of the other levels), in
order to limit the pumping effort.
[0102] In an example, at a given level Lm:
[0103] the length of a channel portion (not at an edge) is
Lm=(L1-Wmin)/Bm-1; and
[0104] the width of a channel portion is Wm=Lm-1/Bm/2-Wmin,
[0105] wherein Wm is a width of the channel portions at level m
and Wmin is a minimal wall thickness. The above dimensions are
valid if Wm is the same for inlet and outlet channel portions and
if it is constant for each portion, subject to edge effects.
[0106] The height of the channels may for instance be independent
from one level to each other. Assuming that all levels should have
the same footprint, the relationship between the lateral
dimensions of the channels from one level to the next shall
notably depend on the branching factor.
[0107] In terms of manufacturability, it may be advantageous to
have one or more levels embodied, each, as superimposed sub-layers
(e.g., sL31 and sL32 for level 3 in FIG. 1). In FIG. 1: a first
sub-layer sL31 includes orifices, whereas the second sub-layer
sL32 includes channel portions. Both the orifices and channel
portions can be machined as through holes in their respective
sub-layers, which makes the manufacture process easier.
Superimposed layers may be made of different materials, if
necessary, since the different dimensions and shapes of the
channel portions vs. orifices may more easily be processed using
different materials.
[0108] A cooling device such as described above is advantageously
used together with a photovoltaic receiver 20, such as depicted in
FIG. 8 or 9. This receiver may include a photovoltaic module 21,
such as depicted in FIG. 4 or 5. The receiver shall further
include a heat circuit portion 71a (FIG. 8, 9), connected to the
photovoltaic module and the cooling device 25, the latter forming
part of the heat circuit portion 71a.
[0109] Preferably, the above cooling device is used together with
a photovoltaic thermal hybrid solar receiver 20, such as
i1lustrated in FIG. 8 or 9. The latter further includes thermal
collector 22, distinct from the photovoltaic module 21 of the
receiver. In that case, the heat circuit portion 71a is a first
heat circuit portion 71a, distinct from a second heat circuit
portion 72a, that connects to the thermal collector. Such a
photovoltaic thermal hybrid solar receiver 20 shall be described
in detail below.
[0110] Cooling Devices: Specific Implementation Details
[0111] The cooling device is preferably designed to allow for
cooling the cell package with elevated temperatures of the coolant
while keeping the cell at a moderate temperature (<100[deg.]
C.). This way the collected thermal energy is of high value due to
its elevated temperature level.
[0112] For this purpose the cooling device is preferably designed
to have minimal thermal resistance between the PV cells and the
cooling fluid. A cooling device such as described above may
provide thermal resistance of less 0.11 cm<2>K/W. Assuming
the PV cell is connected to the cooling device by a solder
interface the total thermal resistance from the PV cell surface to
the liquid coolant is around 0.17 cm<2>K/W. This allows
cooling for heat flux densities of more than 400 W/cm<2
>while keeping the cell at less than 100[deg.] C. (assuming the
fluid inlet temperature is 30[deg.] C.).
[0113] The cooler can be optimized to operate at low pumping
powers, thereby reducing the energy needed to operate the system.
The above solutions allow a homogenous cooling performance over an
extended area ([Delta]T<+-0.2 K) that can be easily scaled.
[0114] Reliability of the package may also be considered. A
solution using silicon as substrate material allows a good thermal
coefficient of expansion match between the PV cells (typically
germanium) and the cooler, which reduces stress on the cells. Use
of silicon further allows for using MEMS processes to structure
cooler surface and implement sensing elements in the cooler
(temperature, radiation, pressure . . . ).
[0115] Minimizing pumping power while maximizing temperature
homogeneity across the cooler surface can be both achieved with an
efficient manifold such as described above, i.e., a hierarchical
fluid distribution/collection system with two main paths (fluid
inlet and outlet).
[0116] A layer-wise implementation of distribution channels
(manifold) and injection orifices (nozzles) allows for: using
different materials and fabrication methods to cover the broad
range of structure dimensions (e.g., from 20 [mu]m to 20 mm or
more); using different materials, which in turn allows for
achieving low thermo-mechanical stress in the cooling layer,
increasing the lifetime of the package, and scalability.
[0117] The cooler package is preferably fabricated using MEMS
technology, taking advantage of definition and processing of
microstructures, batch processing, bonding techniques, integration
of sensing elements, etc.
[0118] In reference to FIG. 1, 4 or 5, this package typically
includes a layer 21, on top, comprising PV cells 211, forming a
multichip module 212, the PV cells connected by electrical
interconnects (see below); bypass electrodes 213; and an
electrical layer (214), to connect the bottom electrodes of the PV
cells. Layer 21 may further contain: a sensor layer with a network
of resistive temperature devices to map the temperature over the
entire package right at the bottom of the PV cell (not shown); an
insulation layer, to insulate the sensor layer to electrical layer
(not shown). These layers are typically processed using thin film
deposition techniques as well as galvanic processes. Solders can
be applied by a galvanic process too or any conventional process
like screen printing.
[0119] In the cooling sub-layers, micro channels can be fabricated
by DRIE to enhance heat removal. These channels can be also
fabricated using multiple dicing saws. In an orifice sub-layer
(e.g., sL31 in FIG. 1): orifices can be fabricated by DRIE. Die
casting and other mass production processes can also be used to
fabricate such a sub-layer.
[0120] A multichip module package including a cooling device as
described above may include high efficiency triple junction solar
cells (or "3JPV", commercially available) soldered onto a
substrate with a minimal distance between each other; a cooler
package (or heat sink) having a micro machined silicon wafer 24,
i.e., a heat exchanger and carrier of electrical network, with a
micro machined heat transfer structure on the bottom side,
comprising channels (such as CPt1311 in FIG. 1 or 4); integrated
temperature sensors; an electrical network consisting of
electrically conductive pads (214) which connect to the bottom
electrode of a PV cell; a manifold system, for fluid distribution
and collection, with one substrate combining orifice sub-layer
sL41 and manifold sub-layer sL32 and one substrate with orifice
sub-layer sL31. With such a (specific) design, two sub-layers can
be combined in a single substrate to take advantage of the
specific process of double side DRIE. Doing so the number of
components and interfaces can be reduced. In general layers should
be combined if the process and the design allow, in order to
reduce fabrication costs.
[0121] Electrical interconnects (including conductive pad 214,
connection 216, etc.) which connect a top electrode of one cell to
a top electrode of another cell in case of a parallel connection
or which connect a top electrode of one cell to a electrically
conductive pad 214 which is again connected to the bottom
electrode of another cell in case of a serial connection (see
below, 300 [mu]m wire bond, soldered or welded Cu ribbon or lead
frame). A carrier 251 for mechanical support and interface to
larger system includes a manifold layer (embodying both levels L1
and L2), made of polymer, metal, composite materials, etc.
[0122] In reference to FIG. 5, a multichip module receiver package
shall typically include, in addition to components described
earlier, a shield 215 to protect components not meant to be
exposed to radiation. In addition, the shield encapsulates the PV
cell package to protect against dust, humidity, etc. The shield
further includes a cover window 215a that can be used to filter
radiation, if needed, see section 2.2. Shield walls 215b can be
used as secondary reflectors to homogenize incoming radiation. The
shield has a heat recovery system that can be coupled to the
cooling loop, in series, or to a separate heat circuit, as
described in detail below
[0123] Photovoltaic Thermal Hybrid Solar Receivers
[0124] In reference to FIGS. 6-10, novel photovoltaic thermal
hybrid solar receivers 20 are now described. In each case, the
hybrid receivers first include a thermal collector 22. The latter
extends in a first plane 220, which plane typically is a main
plane of extension of the thermal collector, i.e., the plane onto
which radiation can be received and collected. The location of the
first plane is preferably taken at the level of the average plane
of the thermal collection panel of the collector, as depicted in
FIG. 8 or 9. This thermal plane can therefore also be referred to
as a 'shield', as done in some places below. In addition, the
thermal collector includes an aperture 68.
[0125] The receivers 20 further include a photovoltaic module 21.
Such a module is designed for delivering an electrical output
power Po, in operation, as known per se. The module notably
includes a photo-active area 212 that extends in a second plane
210. The latter typically is a main plane of extension of the area
212, e.g., the average plane of the photo-active pane of the
module. It is furthermore preferably parallel to the first plane,
for both simplicity and efficiency reasons, though parallelism is
not a requirement at all. In all cases the second plane 210 is
located at a distance 232 (see FIG. 8 or 9) of the first plane 220
and the area 212 is located vis-à-vis the aperture 68. The
projection of the aperture, i.e., perpendicularly to the second
plane 210, corresponds to the photo-active area (or essentially
corresponds to it). Here, 'essentially' means that the
photo-active area may represent 80 to 100% of the projected area
of the aperture.
[0126] The above design, wherein plane 210 is distant from the
plane 220 and area 212 is set vis-à-vis aperture 68, allows for
easily varying a ratio of radiation exposure of the photovoltaic
module 21 to the thermal collector 22, e.g., by simply translating
the device perpendicularly to plane 210, with respect to a
radiation focus point or plane. This device accordingly makes it
possible to rapidly "switch" from PV power delivery to thermal
power storage.
[0127] Another advantage is that: when the light beam is
defocused, the PV electrical output becomes smaller but the
thermal output on the front target is larger. A benefit can
therefore follows even with a misalignment. Thus, a less accurate
tracker and a higher maximal optical concentration with a lower
cost mirror can be reached.
[0128] In addition, the thermal collector and the photovoltaic
module may be configured to protect peripheral regions of the
photovoltaic module from radiation hitting the thermal collector.
Namely, the thermal collector may be designed to protect
peripheral regions of the main plane of the photovoltaic module
and at least partly shields radiation received from a light source
at the photovoltaic module, e.g., to protect passive diodes or
passive components in the photovoltaic module.
[0129] Preferably, a hybrid receiver further includes a first heat
circuit portion (ref. 71a in FIG. 8 or 9), thermally connected to
the photovoltaic module (at the back thereof), and a second heat
circuit portion (72a) thermally connected to the thermal
collector. The circuit portions can be connected to respective
heat circuit portions, typically closed-loop, as to be discussed
below. The circuit portions 71a and 72b can be thermally insulated
from each other, if necessary. Portion 71a or 72a, or both
portions 71a and 72a could for instance be embodied as a cooling
device such as described earlier, in section 2.1, see e.g., ref.
25 in FIG. 1 or 4.
[0130] Typically, the first circuit portion 71a is inserted in a
first heat circuit 71, configured to cool the PV receiver, and the
second circuit portion 72a is inserted in a second circuit 72,
independent from the first circuit, and connecting in turn to a
thermal storage, to serve a purpose described in the next section.
In variants, the first portion 71a and the second portion 72a may
be thermally connected, in series, in a same heat circuit, subject
to additional constraints to be discussed later. For completeness,
FIGS. 8, 9 show inlet/outlet circuit sections 71i, 71o, 72i, 72o,
of respective circuits 71, 72.
[0131] The distance 232, as well as the distance 231 between the
area 212 and a lower end 68a of aperture 68 both depend on a
number of design and system options, which are discussed later in
details (desired insulation, circuitry dimensions, presence of a
homogenizer, a filter, a concentrator and characteristics thereof,
translational speed and desired reactivity of the system, etc.).
[0132] For instance, the end 68a of the aperture 68 that is the
closest to the photo-active area 212 is preferably kept at a
(small) distance from this area 212, as i1lustrated in FIG. 8, to
ensure thermal insulation. Typically, this end of the aperture 68
is located at a distance larger than or equal to 0.2 mm, which may
already suffice to insulate the thermal collector from the PV
receiver, as tests have demonstrated (air can be used as
insulating medium). However, depending on the PV module size and
cooling circuit temperature used, this distance may need to be
larger than or equal to 0.5 mm, and/or other insulating material
may be used. On the other hand, this distance is preferably
smaller than or equal to 3.0 mm. Indeed, it can be realized that
this gap needs to be small enough so that light cannot "escape".
Namely, light exiting the aperture has a defined angle, the above
distance is therefore designed small enough so that outcoming rays
shall not hit the periphery of the active area. Depending on other
device specifications, this distance may more preferably be
smaller than or equal to 2.0 mm, and even more preferably 1.0 mm.
The accompanying figures are obviously not to scale, at least not
in respect of every feature shown.
[0133] Now, it can be realized that, since (i) minimal thermal
circuit sections typically have a diameter of 5 mm, and (ii) the
end 68a is located at a distance larger than 0.2 mm, then the
minimal distance 232 need be larger than 2.7 mm. Instead, using a
6 mm circuit diameter would bring this value to 3.2 mm. This
minimal distance is increased if, in addition, an intermediate
homogenizer is used (e.g., at least 10 mm, optimally 60 mm long
for an aperture of approximately 35*35 mm and an light incidence
angle of 53[deg.], the rim angle of the parabolic dish). More
generally, if no homogenizer is provided, the minimal distance
232, FIG. 8, is determined by the dimensions of the thermal
collector (that includes thermal circuit 72a, panels, etc.).
[0134] Note that, at variance to FIG. 8 or 9, the thermal
collector 22 may include a tapered aperture section, i.e., with a
non-constant cross section. In that case, the end 68a of the
aperture 68 would correspond to a smallest cross sectional area of
the non-constant cross section.
[0135] As evoked earlier, the thermal collector may further
include one or more minor elements 74 (see FIG. 6, 7 or 9), for
example a light homogenizer or, more generally, optics, i.e.,
secondary optics (beyond a concentrator), in an intermediate
section 75 between the first plane 220 and the second plane 210.
Such mirror elements can be configured to specifically reflect
incoming light 90a-c and distribute reflected light 90b-c onto the
photo-active area 212, as i1lustrated in FIG. 9. For example,
minor elements may be configured to homogenize and/or further
concentrate reflected radiation 90b-c onto area 212. To that aim,
simple possibilities consist of having at least three or four
mirror elements 74, forming a closed hollow section 75, as
depicted in FIG. 6, 7, or 9. Yet, a single tubular minor could be
used.
[0136] Advantageously, the one or more minor elements 74 are
thermally connected to the second heat circuit portion 72a, such
as to benefit to a corresponding heat circuit. In that case,
optimal results shall be obtained if a part, at least, of the
circuit portion 72a is coiled around the minor elements, as shown
in FIG. 9 or 10. The needed circuitry can for instance be suitably
molded or arranged in an insulating body, as better seen in FIG.
7, wherein sections 72a1-7 of the second heat circuit portion are
visible.
[0137] Interestingly, the thermal collector may further include a
bandpass filter 76 (see FIG. 7 or 9), e.g., at the level of an
upper end of the aperture 68 and fit within the aperture, to
specifically select a bandwidth where conversion efficiency of the
PV cells is optimal. A passband which is optimal for purposes
described later is 350-1500 nm, i.e., it corresponds to the
spectrum where preferred PV cells have a conversion efficiency
larger than 80%. Preferred PV cells are typically multi junction
solar cells, e.g., from Boing Spectrolab, Emcore, Azur Space
amongst others.
[0138] Advantageously, the filter can further be designed to
thermally absorb radiation wavelengths outside the passband, i.e.,
to benefit again to a heat circuit, preferably the second heat
circuit 72, in form of higher grade thermal energy.
[0139] In that respect, the filter may include a hollow cavity
filled with a cooling fluid 77 (see FIG. 7), in fluid
communication with a heat circuit, e.g., circuit 72. Other options
are discussed later.
[0140] Next, hybrid receivers 20 such as described above can
advantageous be used in an apparatus 10 such as depicted in FIG.
10 (or more schematically in FIG. 12 or 13). Such an apparatus
shall further include a concentrator 27. The latter is designed
and configurable to concentrate radiation towards an optical focus
80, as known per se. The optical focus 80 is a region of maximal
intensity of concentrated light, e.g., essentially located to
small volume or confined close to a plane, e.g., plane 80,
depending on actual implementations.
[0141] The apparatus (or the concentrator device itself) further
includes positioning mechanism 27a, 27b, 30, which can have
various purposes. In that respect, the receiver and/or the
concentrator can be movably mounted in the apparatus via the
positioning mechanism.
[0142] For example, the positioning mechanism may be configured to
change a ratio of intensity of radiation 90b,c received at the
photovoltaic module to intensity of radiation 90a received at the
thermal collector. Because of their relative dimensions, it shall
likely be simpler to make the hybrid receiver movably mounted in
the apparatus 10 via positioning mechanism 30 rather than the
concentrator. The receiver can further be movable with respect to
the optical focus 80. Accordingly, the receiver and/or the
concentrator are movable (e.g., along bi-directional axis 84) by
the positioning mechanism from a position where the photovoltaic
module 21 is in the optical focus 80 to a position where the
thermal collector 22 is in the optical focus.
[0143] Changing the ratio of intensity evoked just above is
accordingly very easily obtained, e.g., via a simple translation
of the receiver and/or the concentrator. In this regard, the
positioning mechanism may simply be embodied as one of: a linear
actuator, such as a rack and pinion; or a vehicle, such as a
wheeled vehicle, a tracked vehicle, or a railed vehicle, for
example comprising a trolley, a bogie, etc. more generally, the
positioning mechanism 30 preferably enables bidirectional motion
along an axis 84 perpendicular to second plane 210. The mechanism
30 is preferably specifically dedicated to the task of changing
the above ratio, and possibly to that task only. Usual tracking
systems do not enable suitable bidirectional motion along axis 84,
in operation. Indeed, in prior systems, the receiver's position is
refined during setup but it is then fixed (definitively) for the
life of the system for standard systems.
[0144] Now, the concentrator 27 or one or more elements 271
thereof may further be movably mounted in the apparatus via other
positioning mechanism 27a, 27b, as schematically depicted in FIGS.
10, 12, and 13.
[0145] FIGS. 12-13, which are simplified representations of two
hybrid systems, illustrate the variation of the spot geometry at
the receiver. In each case, the upper drawing represents a
configuration for which the spot is focused at the receiver plane,
while the spot is defocused in the lower drawing. In addition, in
FIG. 12, a classical parabolic concentrator (minor) 27 is used,
while in FIG. 13, the concentrator includes a plurality of mirrors
271, which can be actuated by respective positioning mechanism
27b, to change the spot geometry at a receiver plane (210 or 220,
in FIG. 8-9).
[0146] As schematically i1lustrated, the spot geometry at a
receiver plane can be changed by:
[0147] FIG. 12: displacement of the receiver along the optical
axis 84, e.g., in a rotational symmetric parabolic concentrator,
should a homogenizer be involved or not; and/or
[0148] FIG. 13: changing the shape of the primary concentrator,
for example by tilting of one or more (flat) elements 271 of a
faceted minor.
[0149] In addition, one may defocus the spot by changing the
curvature of the main mirror or the one of secondary optics in a
folded beam arrangement.
[0150] As touched above, to move the receiver module 20 out of
focus, the receiver can be mounted on a movable stage. The stage
can be actuated by a shaft and a stepper motor that are themselves
mounted in a fix position in reference to the focal plane of the
concentrator system. This adjustable receiver positioning unit
represents a control element 30, symbolically represented by
reference 30 in FIG. 10. Alternatively the stage with the receiver
can be moved using a hydraulic or pneumatic actuated piston, etc.
[0151] FIG. 16 shows typical cross sections of the intensity
distribution (normalized intensity) at the PV receiver module
plane (ref. 220 in FIG. 8-9), when using a rotational symmetric
parabolic primary concentrator, for a receiver module displaced
along the optical axis of the system. The x-axis represents a
distance r (mm) along a section passing through the aperture,
where r=0 corresponds to a center of the aperture (typically a
symmetry center). The darker gray box corresponds to the aperture,
while the lighter gray boxes denotes the shield, i.e., the thermal
panel of the collector 22 extending parallel 220 to the receiver
PV module plane 220. As indicated by the various curves
represented in FIG. 16, a light beam can be focused such that the
radiation intensity distributes mostly or essentially within a
zone corresponding to the aperture (this intensity shall
accordingly be converted to electrical power thanks to the PV
cells).
[0152] Defocusing the spot (or altering the mirror shape/elements)
results in widening the intensity profile, such that radiation
becomes essentially collected at the shield.
[0153] In that respect, the shield 22a (FIGS. 6-9) is preferably
made substantially larger than the aperture 68. Typically, the
aperture's dimensions (e.g., between 10*10 and 30*30 mm) reflect
that of the PV-MCM, while the overall shield dimension can reach
200*200 mm or more (e.g., 500*500 mm is possible).
[0154] FIG. 17 shows the total irradiance (normalized power)
captured by the thermal collector (dotted curve) and the PV
receiver (full line) while displacing the element along the
optical axis (distance d (mm) in abscissa) towards the primary
concentrator. Typically, ~30% of the solar radiation reaching the
PVT receiver can be converted to electrical energy while the
remaining 70% can be captured as heat, which together with the
irradiance captured by the thermal collector contributes to a
storage system. The design point of the system is preferably set
to be between 90-20% of the load on the PVT receiver.
[0155] A number of conceptual variants can be contemplated. For
instance, the thermal collector may have a conical shape. The
thermal collector and the homogenizer could be one and a same
element, provided with a suited shape to both collect solar
radiation and distribute/concentrate reflected light as
appropriate onto the PV receiver. When using a flat facetted
mirror concentrator (as in FIG. 13), some of the facets could be
fixed, others could be moved. Facets of the primary mirror can be
tilted to redirect light on the periphery of the receiver 20,
where the thermal receiver panel is placed.
[0156] Additional variants may include light cones mounted
directly on the PV chips with cooling (high temperature) that
eliminate inactive surfaces on 3JPV chip array. Such cones are
arranged such as to redirect that light that would otherwise hit
contact pads of the solar cells and the gap between them. Light is
redirected to the photoactive area, thereby increasing the
electrical efficiency of the system. A front electrode grid with
reflective surfaces may prevent shading of sensitive PV surface.
Antireflection surfaces using, e.g., moth eye patterns may be
combined with front electrode grating that contributes to the
wavelength filtering function by reflecting UV/blue light back to
the homogenizer, to serve the more general functions of adsorption
enhancement and filtering, as described earlier. Switchable
absorbers, depending on humidity (large humidity and early
morning/late evening may increase red shift and underload blue
diode. Additional red absorbers may also be included.
[0157] The various features recited above, in respect of hybrid
receivers, can be advantageously combined, in several manners. For
example, exergetic recovery can be optimized by having a separate
cooling loop 71 for the multichip receiver cooling 25 and for the
homogenizer and shield cooling 72. As explained, electrical output
can be controlled by moving the assembly along the optical axis
closer to the minor and away from the focal plane. Exergy
optimization can further use a wavelength selective reflective
filter to avoid exposure of the PV chips, e.g., a multichip module
(or MCM) triple junction chips with light they cannot convert (UV,
and far IR). The inactive area between the chips is advantageously
reduced by having triangular reflectors placed on the front
electrodes and the connection mesh (not shown for clarity).
[0158] A dispatched delivery scenario of electrical power by a
CPVT system as contemplated herein can for example be briefly
described, in reference to FIG. 18. FIG. 18 shows three curves,
representing:
[0159] Full line: the morning power demand peak and the evening
demand peak;
[0160] Dotted (gauss-like curve): a typical PV 2 hour design
power, having a maximum around 13:00;
[0161] Short-dashed: a typical CPV 6 hours design power; and
[0162] Dash: an 8-9 hour design power, as can be achieved thanks
to embodiments of the invention. An 8-9 hour design power can
indeed be achieved, i.e., output power can now be maintained over
8-9 hours instead of just 2 hours like for flat PV. In particular,
the hybrid receiver can be moved out of the focal plane to reduce
optical intensity, as explained earlier. A feedback loop can move
the receiver back to the focal plane to compensate for temporary
irradiation loss (e.g., light clouds) or to meet higher power
output demand, as to be explained in more details in the next
section. The excess energy is harvested as heat, thanks to the
thermal collector and associated circuit and used to bridge the
morning and evening peak demands, e.g., using a Rankin engine with
stored hot (and pressurized) water (e.g., 150[deg.] C.). Depending
on the actual size of the thermal collector, this temperature
cannot be too large, otherwise this would lead to radiative losses
from the large area thermal collector.
[0163] More details as to operation methods and system description
shall be given in the next section.
[0164] Photovoltaic Thermal Hybrid Systems and Methods of
Operation Thereof
[0165] The present section focuses on methods to operate
photovoltaic thermal hybrid systems. An example of hybrid system
10 is shown in FIG. 10. Some components of or variants to this
system are depicted in FIGS. 1-9, 12-15, and 19-20.
[0166] Referring to FIGS. 1-20 in general and in particular to
FIG. 11, the methods generally rely on a system 10 comprising: a
hybrid solar receiver 20 such as described in section 2.2, i.e.,
wherein the receiver includes a photovoltaic module 21,
operatively coupled to the system 10 to deliver an electrical
output power PO, e.g., for a power user; and a thermal collector
22 such as described in section 2.2 too. Importantly, for the
purpose of implementing methods as described herein, the collector
must be distinct (e.g., thermally insulated) from the photovoltaic
module. In addition, the photovoltaic module and/or the thermal
collector are/is movably mounted in the system (e.g., on a stage).
[0167] The system further includes a collector thermal storage 42.
As discussed earlier too, the latter is thermally connected to the
thermal collector 22, typically via a closed-loop heat circuit 72,
such that heat collected at the thermal collector can be stored in
the storage 42. In this application, two components "thermally
connected" means the same as two components "thermally coupled",
i.e., heat can be exchanged from one component to the other.
Finally, system 10 includes positioning mechanism 30, which are
adapted to move the photovoltaic module and/or the thermal
collector.
[0168] Next, the operation methods include a step of instructing
(FIG. 11, step S30) the positioning mechanism 30 to move the
photovoltaic module 21 and/or the thermal collector 22 to change a
radiation intensity ratio. The ratio compares intensity of
radiation received (FIG. 11, step S10) at PV module 21 to
intensity received (S10) at the collector 22. One understands that
such methods can take advantage of devices such as described
herein.
[0169] Whether to instruct the positioning mechanism 30 to move
the photovoltaic module 21 and/or the thermal collector 22 is
typically decided at a control system/unit 100 such as depicted in
FIG. 20. This control system/unit shall be described in detail in
the next section. Note that decision S30 can be based on a power
demand as calculated, predicted, etc. but could also be based on
thermal demand (at least partly). A power demand is the power
needed from the grid at a particular time, e.g. noon peak or
evening peak.
[0170] For instance, referring in particular to FIG. 11, data
indicative of an electrical power demand PD may be received at a
step S80. Decision S30 may then be carried out based on a
comparison (steps S20, S22) of the PV output power PO (e.g., as
delivered by the PV module) with the power demand.
[0171] Note that in typical applications, power demand is AC
whereas the output power is DC. Thus, the system 10 shall
typically include an inverter 28, see FIG. 10, through which power
is processed before delivery to power user. In case, indirect
comparison might be needed (AC to DC), depending on the system's
logic 100. In general, PD is always AC power. Since a DC/AC
conversion ratio or calibration curve is usually known, it can
easily be integrated in the feedback loop. Conversion may change
with loading (e.g., 98% at 100% load and 96% at 50% load) but an
exact calibration curve is usually available.
[0172] In particular, decision S30 may be made to suitably move
the PV module and/or collector to decrease the radiation intensity
ratio if comparison S20 indicates that the output power PO is
larger than the power demand PD. Indeed, if PO is larger than PD,
it can be realized that leaving the configuration of the PV module
vs. collector unchanged is sub-optimal. On the contrary, with a
receiver 20 such as described above, the configuration of the
receiver 20 can be altered to favor thermal collection instead of
electrical power conversion.
[0173] Now, it can be instructed (step S24) to deliver the output
power PO generated by the PV module 21 to a power user, to meet
the power demand PD if PO matches the power demand PD, based on
the comparison carried out at steps S20, S22. In FIG. 11, Pd
denotes the actually dispatched power (step S24, S57 or S52).
Complete description of FIG. 11 shall be given later.
[0174] Typically, such comparisons S20, S22 are subject to a
tolerance, which depends on the system capacity, reactivity, etc.
This tolerance can be adjusted empirically, e.g., based on
trial-and-error process. Also, here again, consistent power values
are compared (e.g., AC to AC).
[0175] Additional components may be provided in the system 10 to
further optimize it. For instance, system 10 may further include a
heat engine 62, as depicted in FIGS. 14-15. The heat engine 62 is
thermally connected to the collector thermal storage 42.
[0176] In that case, present methods may further include steps of
instructing (FIG. 11, steps S50, S56) the heat engine 62 to start
a process of thermal-to-electrical conversion, to convert heat
stored in the collector thermal storage 42. Whether to do so is
typically decided based on comparisons S20, S22, i.e., if it turns
out that PO is lower than the power demand PD.
[0177] Note that the heat engine 62 can be any kind of
thermal-to-electrical converter suited for the present purposes,
e.g., to run a Rankine cycle, preferably an organic Rankine cycle
(ORC), which uses an organic fluid such as n-pentane or toluene in
place of water and steam. This allows for using lower-temperature
heat sources, which typically operate at around 70-90[deg.] C.,
but works still better at higher temperatures such as
120-150[deg.] C. as presently contemplated. Suitable fluids can be
chosen among Hydrochlorofluorocarbons (HCFC), Chlorofluorocarbons
(CFC), Perfluorocarbons (PFC), Siloxanes, Alcohols, Aldehydes,
Ethers, Hydrofluoroethers (HFE), Amines, Fluids mixtures
(zeotropic and azeotropic), Inorganic fluids. Examples are:
R245fa, R123, n-butane, n-pentane and R1234yf, Solkatherm, R134a,
R600, carbon dioxide, R152a, R600a, R290, etc. A comparison of the
critical temperatures of the fluids vs. optimal operation
conditions of systems as contemplated herein allows for refining
the choice. In particular, experiments conducted in the context of
the present invention have shown that fluids R134a, followed by
R152a, R600, R600a and R290 are most suitable fluids for
low-temperature applications driven by heat source temperature
below 90[deg.] C. In variants, a thermoelectric generator is
relied upon, which converts heat to electrical power without
working fluid and moving parts. Yet, thermoelectric generators
currently have lower conversion efficiency for kW to MW sized
converters.
[0178] A control system (FIG. 20, ref. 100) with feedback loop is
used to adapt the electrical power output to the actual demand
required, e.g., by a grid control station. FIG. 11 shows an
example of a main control process for a dispachable power mode. In
this example, the generated electrical power is the main control
variable and is adapted to the demand using the receiver
positioning system. The positioning response is in the range of
seconds, while the start of a Rankine cycle can be predicted and
therefore kept with the same response time.
[0179] Even more valuable than dispatched power is the function of
grid services. A photovoltaic unit with motorized receivers can
take this function when a feedback loop is closed between the
phase angle [phi] in the grid (indicating the load situation) and
the position of the receiver.
[0180] The smaller the angle [phi] the more is the receiver moved
away from the focus; the larger the angle [phi] the closer the
receiver is moved to the receiver. Most valuable are grid services
that can react very fast i.e. within seconds, a thing that can be
achieved thanks to embodiments of the present invention.
[0181] In this respect, an inverter can switch off an input
current in a matter of milliseconds, e.g., in a situation where
the grid fails (lightning or physical damage). In this situation
the receivers 20 can be moved to the minimum power position within
a few seconds; power can thus be dissipated in open circuit
voltage mode. The generated charges flow back in the PV diodes,
adding thermal load to the microchannel cooler. Accordingly, no
damage to the system is induced.
[0182] Next, additional optimization to the system 10 can be
achieved if the methods and systems integrate additional client
processes. For instance, the method may further include steps of
instructing (FIG. 11, step S42, S60) to trigger additional
processes to dissipate heat from the collector thermal storage.
This is preferably decided at step S42, if a heat storage
threshold of the collector thermal storage 42 is achieved.
[0183] The additional processes are preferably a desalination
process and/or an adsorption cooling process. More generally, a
variety of client processes can be integrated, e.g., a free
cooling process or a process to deliver heat for a chemical
application and/or process, etc. However, it can be realized that
combining present systems/methods with a desalination process or
an adsorption (e.g., water adsorption) cooling process has more
value in context such as contemplated in present embodiments,
i.e., the higher the solar radiation levels, the more valued is
the output of a desalination or a cooling process.
[0184] Moreover, as depicted in FIG. 10, the system 10 may further
include a first heat circuit 71 (typically closed-loop),
connecting the PV module to a PV thermal storage 41, wherein the
latter is distinct from the collector thermal storage 42. The PV
thermal storage 41 and circuit 71 are used to cool the PV module
(use can for instance be made of a cooling device 25 such as
described in section 2.1). A second heat circuit 72 (typically
closed-loop too) is also provided, distinct from the first heat
circuit 71, which connects the collector thermal storage 42 to the
thermal collector 22. Components 41, 42 also appear in FIGS. 14
and 15.
[0185] Note that in variants, the system may include a heat
circuit connecting both the PV module and the thermal collector to
a thermal storage, in series, such that fluid in a single heat
circuit first reaches the photovoltaic module to cool it down and
then reaches the thermal collector.
[0186] Any of the heat circuits contemplated herein (a single heat
circuit when using only one circuit or one of or both the two
circuits when using distinct heat circuits) could additionally be
used to cool any component in the system. Accordingly, part or all
of the components that dissipate heat can be included in the loop,
such as to contribute to the energy conversion efficiency of the
system.
[0187] Next, the system may further include a heat exchanger 61,
as shown in FIG. 14. The exchanger 61 is thermally connected to
the PV storage 41. Accordingly, it can be instructed to provide
heat stored in PV storage 41 to a thermal user 64, via the heat
exchanger 61.
[0188] Advantageously, heat exchanger 61 is further thermally
connected to the collector thermal storage 42. In that case, it
can be instructed to provide additional heat stored in the thermal
collector storage 42 to the heat exchanger 61, while providing
heat stored in the PV storage 41 to the thermal user 64, via
exchanger 61.
[0189] Heat exchanger 61 may actually include two heat exchangers
in series: a first one lifts up temperature and a second one
transfers heat to the user. The second heat exchanger can be an
integral part of the thermal user 64.
[0190] As i1lustrated in FIG. 14, the system 10 may further
include an additional heat exchanger 63, thermally connected to
heat engine 62 and thermal user 64.
[0191] Advantageously, a thermal user 64 (desalination, adsorption
heat pump) is furthermore thermally connected to the PV thermal
storage 41. It can furthermore be connected to collector thermal
storage 42, via heat exchanger 61. Then the method may
additionally include a step of instructing (FIG. 11, S60) the heat
engine to start a process of thermal-to-electrical conversion of
heat stored in the collector thermal storage 42, using heat
exchanger 63 as a low temperature pool.
[0192] The additional heat exchanger 63 may be connected to the
heat engine 62 and the thermal user 64 to provide the low
temperature pool for the Rankine cycle. For example: a saline feed
can be directly inputted to user 64 (step S64, FIG. 14), in which
case the Rankine cycle may use air as a low temperature pool; or
the saline feed may pass through heat exchanger 63 (preferred
option, step S63, FIG. 14) and thus serves as the low temperature
pool to increase a difference of temperature for the Rankine
cycle.
[0193] At present, a complete description of the method of FIG. 11
is given. FIG. 11 corresponds to a particular embodiment,
combining many aspects of the methods discussed above:
[0194] Step S10: solar radiation is received on the thermal
collector and/or the PV module;
[0195] Step S10: the actual PO is compared to the power demand PD,
thanks to data relating to the a power demand as received at step
S80 (e.g., power demand may vary rapidly; a corresponding data
flow may be received and processed at unit 100, FIG. 20). In
particular, if it appears that PO>PD, the process goes to S30.
As stated, this comparison is preferably subject to ad-hoc
tolerance and possibly a timer, to avoid too frequent actuations.
If this condition is not fulfilled (PO is not larger than PD), the
process goes to S22;
[0196] Step S30: as PO>PD, positioning mechanism are instructed
to move the photovoltaic module and/or the thermal collector, to
decrease the radiation intensity ratio and thereby favor radiation
collected at the thermal collector;
[0197] Step S22: unit 100 tests whether PO PD, in which case PO
can be dispatched, step S24, to meet the current power demand
(PO=Pd). If not, the process goes to S50;
[0198] Step S50: unit 100 checks whether heat stored in storage 42
is sufficient to start a thermal-to-electrical conversion and
thereby meet the power demand PD;
[0199] Step S56: if yes, the thermal-to-electrical conversion
process is started; electrical power accordingly produced can then
be dispatched, step S57, to meet the current power demand. If
necessary, the electrical power obtained by thermal-to-electrical
conversion may be "added" to the PV power available PO to meet the
demand. Yet, the "size" of the thermoelectrical converter shall
typically be 10-20% of the maximal power that the CPVT system can
deliver. This, in practice, is enough to satisfy demand overnight
but not during day.
[0200] Step S52: If not (i.e., if the heat stored in storage 42 is
not sufficient to start a thermal-to-electrical conversion), then
the process shall fail to meet the demand. Yet, the available PV
power can nonetheless be delivered;
[0201] Step S40: since at step S30, positioning mechanism may have
moved the photovoltaic module and/or the thermal collector to
favor radiation collected at the thermal collector, heat can
conveniently be stored (step S40). The current level of heat as
stored at S40 is used as input for S50;
[0202] Step S42: on the other hand, if the storage capacity
appears to be achieved (as monitored at S42), unit 100 may
instruct to start an additional, client process (e.g., free
cooling, desalination, adsorption cooling, etc.): the process goes
to S60. Now, if the storage capacity is not achieved yet,
additional heat can be stored, step S40.
[0203] Following this principle, a particular efficient scenario
is now described, referring notably to FIG. 14. Heat is collected
from the microchannel cooler (FIG. 1-5, ref. 25) into a low grade
heat tank 41 (FIG. 14), by way of heat circuit 71 (71i, 71o). Heat
is further collected from the homogenizer 74 (FIG. 9) and thermal
collector 22 (FIG. 9) into a high-grade heat tank 42 (FIG. 14),
thanks to circuit 72 (72i, 72o). The low grade heat tank directly
feeds power user, namely a desalination system (membrane
distillation) 64. Additional heat exchanger 61 can lift the
temperature using heat from the high grade tank when the low-grade
heat tank is partially or fully depleted. The high grade heat tank
feeds a Rankine process 62 to convert heat into electrical power
with an efficiency of 20-30%. The low temperature pool is derived
from the incoming salt water S63 or from an air cooler S64 (FIG.
14).
[0204] FIG. 15 shows another possible configuration for the system
10, whose underlying scheme allows for managing both electrical
power and water delivery on demand. FIG. 15 shows:
[0205] The same components 20, 41, 42, 62 and 64 as in FIG. 14,
except that the desalination system includes 64, 64a and 65.
Reference 64 now corresponds to the desalination process, 64a is
the corresponding feed of the process 64, and 65 refers to a
desalination water storage. The desalination water storage 65 is
connected to the desalination process 64 to provide water 66 on
demand;
[0206] A heat exchanger 63a, which is connected to feed 64a of the
desalination system and to the Rankine process 62, itself
connected to both storages 41 and 42 as before. Note that heat
exchanger 63a in FIG. 15 plays a similar role as heat exchanger 63
in FIG. 14;
[0207] The first heat circuit 71 connects to the first storage 41
as before. The circuit now branches to the desalination process 64
(via circuit portion 71b), which is otherwise aided by the storage
41 (via circuit portion 71c). Circuit portion 71c may include a
heat exchanger, if needed.
[0208] The above system allows for providing both electrical power
10a and water delivery 66 on demand, making optimal use of high
and low grade heat tanks.
[0209] Methods as described hereinbefore are all the more
efficient if the temperature in the collector thermal storage 42
is substantially larger than the temperature in the PV thermal
storage 41, i.e., more than 20[deg.] C. However, a temperature
difference of more than 30[deg.] C. substantially improve
performances of the systems. Ideally, temperatures differ by more
than 50[deg.] C., a thing that can be achieved in embodiments as
described herein.
[0210] The hybrid receiver 20 is preferably movably mounted in the
system 10, such that positioning mechanism 30 can move the
receiver 20 as a whole (e.g., the photovoltaic module and the
thermal collector are not movable independently from each other by
the positioning mechanism), by simple translation along the
optical axis, as described in section 2.2. This substantially
simplifies the design of the system. In addition, this allows for
integrated solutions that efficiently capture heat dissipated by
the various components of the receiver 20, e.g., via circuit 72.
In turn, the temperature difference between the two circuits 71,
72 can be optimized.
[0211] In variants, only the thermal collector panel 22a could be
moved (the PV module 21 is fixed). For instance: the thermal
collector panel may consists of essentially a 2D arrangement of
thermal circuits intermingled with an array of lenses, which
collector can be moved more or less close to the fixed PV module.
In addition, assuming a homogenous distribution of the radiation
on the photovoltaic receiver, this latter can be moved relatively
to the thermal receiver (or vice versa), in transverse direction
to incoming radiation, to cover a section of the photovoltaic
receiver and accordingly vary the energy captured in the thermal
circuit vs. the PV circuit. Accordingly, there are various
possible ways of embodying a photovoltaic module and/or a thermal
collector movably mounted in the system.
[0212] Weather Predictions, Predicted Electricity and Water on
Demand
[0213] The objective of some of the methods described herein is to
provide electricity on demand and at the same time fulfill other
core demands in a sunny location based on medium/high grade heat
delivered by the solar CPVT receiver: e.g., desalinated water and
cooling. Desalination and/or cooling can be operated directly or
from stored heat. A sufficient temperature level for desalination
and cooling can be reached thanks to the above methods. Hot water
can be stored during high irradiance, i.e., exceeding the need for
electricity. The coolant from the PV cooling unit is stored in the
warm water tank 41 for later use at power users 64 (desalination
and cooling). When more electrical energy is needed than available
from the PV receiver, a low-pressure organic Rankine process 62 is
activated. A microchannel heat exchanger 25 driven by the stored
heat creates vapor that drives a turbine and produces electrical
power.
[0214] Electrical demand curves in most locations show a peak
during noon and two smaller peaks in the morning and in the
evening. The demand during the night is typically 10 times
smaller. With an organic Rankine facility that is 10 times smaller
than the peak photovoltaic output the night time demand, and
together with the partial solar power the morning and evening
peaks can be covered.
[0215] In order to bridge the night about 30% of the daily thermal
input is collected at a high temperature level and converted to
electrical power by a high efficiency low temperature organic
Rankine cycle. Heat is stored in a hot water tank during day,
together with the lower ambient temperature at night the Rankine
cycle can convert the heat into electrical power with a fairly
good efficiency. The efficiency of the thermal-electrical
conversion will be improved by use of the solar concentrators to
radiate thermal energy to space at low or negative Centigrade
temperatures. Since thermal desalination provides a relative value
that is more than 30% of the electrical output, it can be realized
that it is the ideal candidate for a controlled output power
station. Thermal desalination processes can be easily regulated by
a factor of four and delivery of desalinated water can be
on-demand when a large output water storage tank is used.
[0216] To allow a concentrated photovoltaic thermal system to
store a week worth of energy for desalination and electrical
energy generation at reasonable prices two separate storage tanks
are needed: (i) a ~5000 m<3 >per MW warm water atmospheric
pressure storage pool and a ~1000 m<3 >pressurized hot water
storage tank. The warm water pool stores the 90[deg.] C. heated
coolant from the PV microchannel coolers whereas the hot water
tank stores the 150[deg.] C. coolant from the thermal collector
(panel+homogenizer). In variants, a single low pressure tank with
a volume of ~5000 m<3 >is needed for a sequential cooling
system (circuits 71 and 72 in series) that operates at ~120[deg.]
C. and 2 bars. The hot water storage can be used to drive a
low-pressure organic Rankine engine whereas the warm water storage
tank is used to drive the membrane desalination or adsorption
cooling processes (FIG. 14). A heat exchanger is devised to extend
the capacity of the warm water tank and the desalination capacity
by a factor of two in case electrical demand is low. Both tanks
use a layered storage approach to prevent temperature drops in
partially filled tanks.
[0217] More problematic are periods of bad (rainy) weather where
the direct solar radiation is very small. Fortunately, the demand
for desalinated water or cooling during these periods is
negligible. This means the whole thermal storage can be converted
to electricity using the organic Rankine facility. With improved
computer modeling weather prediction has become accurate over a
period of five days, i.e., a period for which thermal storage can
be achieved.
[0218] The efficiency of the thermal-electrical conversion will be
improved by use of solar concentrators to radiate thermal energy
to space at low or negative Centigrade temperature.
[0219] Referring to FIGS. 19 and 20: for areas with multiple solar
power stations the stations that face the wind direction can serve
as radiation predictors for the subsequent power stations. This
allows a more accurate short term dispatching of the electrical
power. For situations with upcoming larger clouds the desalination
production is reduced in favor of thermal storage to have enough
capacity for Rankine power generation. The control facility 100 to
perform such functions can be automated. Movement speed and
direction of clouds can be measured by detecting the covering
speed and direction on the different receivers for an upcoming
cloud. The measurement is performed by e.g., the quadrant detector
that is already part of the two axis trackers. Such inputs are
then fed into the control system 100 to determine the trajectory
of the cloud and determine whether and when a neighboring power
station will be affected. This monitoring can be performed
continuously. Outside of the main production zone 300 scattered
"metrology" receiver arrays 301-303 are placed that may supply
single houses or small villages but mainly serve as "early
warning" stations for the appropriate dispatching strategy of the
main power stations. These arrays have to be large enough to be
able to detect cloud speed and direction.
[0220] Next, the control system 100 can be designed to tune the
buffered energy corresponding to weather predictions. The
capability planning of the power-station is now coupled with
weather forecast. Before a predicted rainfall, desalination can be
reduced to accumulate heat for production of electricity, in order
to bridge the absence of direct solar radiation during the
rainfall period. This is easily compensated due to the lower
demand for water during rainy periods. Accumulation of heat and
expansion of thermal storage is accomplished by running the
coolant hotter through the CPVT to sacrifice electrical yield.
[0221] Specific Implementation Details
[0222] Many optional features can be contemplated, some of which
have already been evoked above. To start with, the thermal
collector 22 and PV module 21 may be embodied such as described in
section 2.2. Similarly, the receiver may further include minor
elements 74, such as depicted in FIGS. 6-7. The latter are
provided in an intermediate section 75 (FIG. 9) and preferably
thermally connected to the collector thermal storage 42, by a same
circuit 72 that connects the thermal collector 22 to the collector
thermal storage 42. The receiver may also include: a band pass
filter 76 as described in section 2.2; a concentrator (FIG. 10,
27, 27a, 27b, 271) having any of the features described in section
2.2.
[0223] Concerning operation methods: the feedback algorithm could
also be based on thermal demand, to produce water, refrigeration
or feed another thermal process, and not only on the power demand.
In addition, a Rankine engine can run forward and backward, to
help to "pump" up the stored heat. Reversible Rankine engine can
contribute to grid services, which allows for using the investment
in the Rankine engine longer and with better value.
[0224] Additional Technical Implementation Details
[0225] Finally, FIG. 20 illustrates an exemplary embodiment of a
computerized unit suitable for implementing aspects of the present
invention. It will be appreciated that the methods described
herein are largely non-interactive and automated. In exemplary
embodiments, the methods described herein can be implemented
either in an interactive, partly-interactive or non-interactive
system. The methods described above can be partly implemented in
software (e.g., firmware), hardware, or a combination thereof. In
exemplary embodiments, the methods described herein are
implemented in software, as an executable program, and is executed
by a special or general-purpose digital computer, such as a
personal computer, workstation, minicomputer, or mainframe
computer. The system 100 therefore includes general-purpose
computer 101.
[0226] In exemplary embodiments, in terms of hardware
architecture, as shown in FIG. 20, the computer 101 includes a
processor 105, memory 110 coupled to a memory controller 115, and
one or more input and/or output (I/O) devices 140, 145 (or
peripherals) that are communicatively coupled via a local
input/output controller 135. The input/output controller 135 can
be, but is not limited to, one or more buses or other wired or
wireless connections, as is known in the art. The input/output
controller 135 may have additional elements, which are omitted for
simplicity, such as controllers, buffers (caches), drivers,
repeaters, and receivers, to enable communications. Further, the
local interface may include address, control, and/or data
connections to enable appropriate communications among the
aforementioned components. As described herein the I/O devices
140, 145 can be any generalized cryptographic card or smart card
known in the art.
[0227] The processor 105 is a hardware device for executing
software, particularly that stored in memory 110. The processor
105 can be any custom made or commercially available processor, a
central processing unit (CPU), an auxiliary processor among
several processors associated with the computer 101, a
semiconductor based microprocessor (in the form of a microchip or
chip set), a macroprocessor, or generally any device for executing
software instructions.
[0228] The memory 110 can include any one or combination of
volatile memory elements (e.g., random access memory, RAM, such as
DRAM, SRAM, SDRAM, etc.) and nonvolatile memory elements (e.g.,
ROM, erasable programmable read only memory (EPROM),
electronically erasable programmable read only memory (EEPROM),
programmable read only memory (PROM), tape, compact disc read only
memory (CD-ROM), disk, diskette, cartridge, cassette or the like,
etc.). Moreover, the memory 110 may incorporate electronic,
magnetic, optical, and/or other types of storage media. Note that
the memory 110 can have a distributed architecture, where various
components are situated remote from one another, but can be
accessed by the processor 105.
[0229] The software in memory 110 may include one or more separate
programs, each of which includes an ordered listing of executable
instructions for implementing logical functions. In the example of
FIG. 20, the software in the memory 110 includes methods described
herein in accordance with exemplary embodiments and a suitable
operating system (OS) 111. The OS 111 essentially controls the
execution of other computer programs, such as the methods as
described herein, and provides scheduling, input-output control,
file and data management, memory management, and communication
control and related services.
[0230] The methods described herein may be in the form of a source
program, executable program (object code), script, or any other
entity comprising a set of instructions to be performed. When in a
source program form, then the program needs to be translated via a
compiler, assembler, interpreter, or the like, which may or may
not be included within the memory 110, so as to operate properly
in connection with the OS 111. Furthermore, the methods can be
written as an object oriented programming language, which has
classes of data and methods, or a procedure programming language,
which has routines, subroutines, and/or functions.
[0231] In exemplary embodiments, a conventional keyboard 150 and
mouse 155 can be coupled to the input/output controller 135. Other
output devices such as the I/O devices 140, 145 may include input
devices, for example but not limited to a printer, a scanner,
microphone, and the like. Finally, the I/O devices 140, 145 may
further include devices that communicate both inputs and outputs,
for instance but not limited to, a network interface card (NIC) or
modulator/demodulator (for accessing other files, devices,
systems, or a network), a radio frequency (RF) or other
transceiver, a telephonic interface, a bridge, a router, and the
like. As described herein the I/O devices 140, 145 can be any
generalized cryptographic card or smart card known in the art. The
system 100 can further include a display controller 125 coupled to
a display 130. In exemplary embodiments, the system 100 can
further include a network interface 160 for coupling to a network
165. The network 165 can be an IP-based network for communication
between the computer 101 and external servers or clients and the
like via a broadband connection. The network 165 transmits and
receives data between the computer 101 and external systems 300,
301, 302, 303. In exemplary embodiments, network 165 can be a
managed IP network administered by a service provider. The network
165 may be implemented in a wireless fashion, e.g., using wireless
protocols and technologies, such as WiFi, WiMax, etc. The network
165 can also be a packet-switched network such as a local area
network, wide area network, Internet network, or other type of
network environment. The network 165 may be a fixed wireless
network, a wireless local area network (LAN), a wireless wide area
network (WAN) a personal area network (PAN), a virtual private
network (VPN), intranet or other suitable network system and
includes equipment for receiving and transmitting signals.
[0232] If the computer 101 is a PC, workstation, intelligent
device or the like, the software in the memory 110 may further
include a basic input output system (BIOS) (omitted for
simplicity). The BIOS is stored in ROM so that the BIOS can be
executed when the computer 101 is activated.
[0233] When the computer 101 is in operation, the processor 105 is
configured to execute software stored within the memory 110, to
communicate data to and from the memory 110, and to generally
control operations of the computer 101 pursuant to the software.
The methods described herein and the OS 111, in whole or in part
are read by the processor 105, perhaps buffered within the
processor 105, and then executed.
[0234] When aspects of the systems and methods described herein
are implemented in software, as is shown in FIG. 11, the methods
can be stored on any computer readable medium, such as storage
120, for use by or in connection with any computer related system
or method.
[0235] As will be appreciated by one skilled in the art, aspects
of the present invention may be embodied as a system, method or
computer program product. Accordingly, the aspects may take the
form of an entirely hardware embodiment, an entirely software
embodiment (including firmware, resident software, micro-code,
etc.) or an embodiment combining software and hardware aspects
that may all generally be referred to herein as a "circuit,"
"module" or "system." Furthermore, aspects of the present
invention may take the form of a computer program product embodied
in one or more computer readable medium(s) having computer
readable program code embodied thereon.
[0236] Any combination of one or more computer readable medium(s)
may be utilized. The computer readable medium may be a computer
readable signal medium or a computer readable storage medium. A
computer readable storage medium may be, for example, but not
limited to, an electronic, magnetic, optical, electromagnetic,
infrared, or semiconductor system, apparatus, or device, or any
suitable combination of the foregoing. More specific examples (a
non-exhaustive list) of the computer readable storage medium would
include the following: an electrical connection having one or more
wires, a portable computer diskette, a hard disk, a random access
memory (RAM), a read-only memory (ROM), an erasable programmable
read-only memory (EPROM or Flash memory), an optical fiber, a
portable compact disc read-only memory (CD-ROM), an optical
storage device, a magnetic storage device, or any suitable
combination of the foregoing. In the context of this document, a
computer readable storage medium may be any tangible medium that
can contain, or store a program for use by or in connection with
an instruction execution system, apparatus, or device.
[0237] A computer readable signal medium may include a propagated
data signal with computer readable program code embodied therein,
for example, in baseband or as part of a carrier wave. Such a
propagated signal may take any of a variety of forms, including,
but not limited to, electro-magnetic, optical, or any suitable
combination thereof. A computer readable signal medium may be any
computer readable medium that is not a computer readable storage
medium and that can communicate, propagate, or transport a program
for use by or in connection with an instruction execution system,
apparatus, or device.
[0238] Program code embodied on a computer readable medium may be
transmitted using any appropriate medium, including but not
limited to wireless, wireline, optical fiber cable, RF, etc., or
any suitable combination of the foregoing.
[0239] Computer program code for carrying out operations for
aspects of the present invention may be written in any combination
of one or more programming languages, including an object oriented
programming language such as Java, Smalltalk, C++ or the like and
conventional procedural programming languages, such as the "C"
programming language or similar programming languages. The program
code may execute entirely on the user's computer, partly on the
user's computer, as a stand-alone software package, partly on the
user's computer and partly on a remote computer or entirely on the
remote computer or server. In the latter scenario, the remote
computer may be connected to the user's computer through any type
of network, including a local area network (LAN) or a wide area
network (WAN), or the connection may be made to an external
computer (for example, through the Internet using an Internet
Service Provider).
[0240] Aspects of the present invention are described above with
reference to flowchart illustrations and/or block diagrams of
methods, apparatus (systems) and computer program products
according to embodiments of the invention. It will be understood
that each block of the flowchart illustrations and/or block
diagrams can be implemented by computer program instructions.
These computer program instructions may be provided to a processor
of a general purpose computer, special purpose computer, or other
programmable data processing apparatus to produce a machine, such
that the instructions, which execute via the processor of the
computer or other programmable data processing apparatus,
implement the functions/acts specified in the flowchart and/or
block diagram block or blocks.
[0241] The computer program instructions may also be loaded onto a
computer, other programmable data processing apparatus, or other
devices to cause a series of operational steps to be performed on
the computer, other programmable apparatus or other devices to
produce a computer implemented process such that the instructions
which execute on the computer or other programmable apparatus
provide processes for implementing the functions/acts specified in
the flowchart and/or block diagram block or blocks.
[0242] The flowchart/block diagrams in FIGS. 11, 14 and 15
illustrate the architecture, functionality, and operation of
possible implementations of systems, involving methods and
computer program products according to embodiments. In this
regard, each block in the flowchart or block diagrams may
represent a module, segment, or portion of code, which includes
one or more executable instructions for implementing the specified
logical function(s). It should also be noted that, in some
alternative implementations, the functions noted in the blocks may
occur out of the order noted in the figures. For example, two
blocks shown in succession may, in fact, be executed substantially
concurrently, or the blocks may sometimes be executed in the
reverse order, depending upon the functionality involved. It will
also be noted that each block of the block diagrams and/or
flowchart illustration, and combinations of blocks in the block
diagrams and/or flowchart illustration, can be implemented by
special purpose hardware-based systems that perform the specified
functions or acts, or combinations of special purpose hardware and
computer instructions.
[0243] While the present invention has been described with
reference to certain embodiments, it will be understood by those
skilled in the art that various changes may be made and
equivalents may be substituted without departing from the scope of
the present invention. In addition, many modifications may be made
to adapt a particular situation to the teachings of the present
invention without departing from its scope. Therefore, it is
intended that the present invention not be limited to the
particular embodiment disclosed, but that the present invention
will include all embodiments falling within the scope of the
appended claims. For example: various other manifold layer
designs/dimensions/materials could be relied upon for the cooling
devices; various other shapes/dimensions can be contemplated for
the thermal panels of the thermal collectors;
[0244] Additional components (beyond components mentioned in the
present specification) may be inserted in the systems of FIGS. 10,
14 and 15. Many usual components have been omitted in the
description of the devices and systems of FIGS. 1-10, 12-15, and
19-20, for the sake of conciseness.
PHOTOVOLTAIC THERMAL HYBRID SOLAR RECEIVERS
US2013255752
WO2013144751
A photovoltaic thermal hybrid solar receiver includes a thermal
collector, extending in a first plane and comprising an aperture;
and a photovoltaic module, configured for electrical output power
delivery, comprising a photo-active area that extends in a second
plane at a distance from the first plane, the photo-active area
being vis-à-vis the aperture, a projection of the aperture
perpendicularly to the second plane corresponding to the
photo-active area.
BACKGROUND
[0002] The present invention generally relates to photovoltaic
thermal hybrid solar receivers and apparatuses.
[0003] Definitions of certain terms discussed herein are as
follows:
[0004] Photovoltaics (PV) generate electrical power by converting
solar radiation into direct current electricity through
semiconductors exhibiting the photovoltaic effect;
[0005] A photovoltaic cell (or PV cell, also "solar cell" or
"photoelectric cell") is a solid state device that converts energy
of light directly into electricity by virtue if the photovoltaic
effect;
[0006] A photovoltaic module (also "solar module", "solar panel"
or "photovoltaic panel") is an assembly of connected photovoltaic
cells;
[0007] A photovoltaic system typically includes an array of
photovoltaic modules, an inverter and interconnection wiring;
[0008] A thermal collector (also "solar thermal collector")
collects heat by absorbing radiations, such as sunlight;
[0009] A heat exchanger is a device/piece of equipment to
efficiently transfer heat from one medium to another;
[0010] In electronic systems, a heat sink is a component to cool a
device by dissipating heat into a surrounding medium;
[0011] Solar thermal energy (STE) concerns technologies for
harnessing solar energy for thermal energy (heat). STE differs
from and is acknowledged to be much more efficient than
photovoltaics, which converts solar energy directly into
electricity;
[0012] Concentrated solar power (also "concentrating solar power"
or CSP) systems use mirrors or lenses that concentrate a large
area of solar thermal energy onto a small area, such that
electrical power (also "power") can be produced when concentrated
light is converted to heat, which drives a heat engine (e.g., a
steam turbine) connected to a power generator. Common forms of
concentration are: parabolic trough, dish Stirlings, concentrating
linear Fresnel reflector and solar power tower.
[0013] Concentrated photovoltaic (CPV) systems use optics (e.g.,
lenses) to concentrate a large amount of sunlight onto a small
area of solar photovoltaic materials to generate electricity.
Concentration allows for production of smaller areas of solar
cells.
[0014] CPV should not to be confused with CSP: in CSP concentrated
sunlight is converted to heat, and then heat is converted to
electricity, whereas in CPV concentrated sunlight is converted
directly to electricity using the photovoltaic effect;
[0015] Photovoltaic thermal hybrid solar collectors (also "hybrid
PV/T systems" or PVT) are systems converting solar radiation into
thermal and electrical energy. Such systems combine a photovoltaic
cell, which converts photons into electricity, with a solar
thermal collector, which captures the remaining energy and removes
waste heat from the PV module. Two categories of PVT collectors
are generally known:
[0016] PV/T fluid collector (air or liquid). In liquid collectors,
a typical water-cooled design uses conductive-metal piping or
plates attached to the back of a PV module. The working fluid is
typically water or glycol. The heat from the PV cells are
conducted through the metal and absorbed by the working fluid,
which assumes that the working fluid is cooler than the operating
temperature of the cells. In closed-loop systems this heat is
either exhausted (to cool it) or transferred at a heat exchanger,
where it flows to its application. In open-loop systems, this heat
is used, or exhausted before the fluid returns to the PV cells;
[0017] PV/T concentrator (CPVT), wherein a concentrating system is
provided to reduce the amount of solar cells needed. CPVT can
reach very good solar thermal performance compared to flat PV/T
collectors. However, main obstacles to CPVT are to provide good
cooling of the solar cells and a durable tracking system.
[0018] A disadvantage of PV systems compared to other energy
sources is the unpredictable nature of the direct solar radiation.
This leads to intermittent power delivery, which has much less
value than on demand power and leads to grid instabilities.
Storage of electrical energy in e.g. batteries is prohibitively
expensive so that the cost for a storage unit for a full day
production costs much more than the solar power station.
Concentrated solar power systems (CSP) that can store the
collected heat can produce electricity on demand until the stored
heat is dissipated. Concentrated photovoltaic (CPV) power plants
have higher conversion efficiencies than PV and CSP but still
suffer from intermittent power production. Concentrated
photovoltaic thermal (CPVT) systems have a higher system
efficiency because of the improved cooling but reject the heat to
the ambient or produce low grade heat with limited utility.
SUMMARY
[0019] In one embodiment, a photovoltaic thermal hybrid solar
receiver includes a thermal collector, extending in a first plane
and comprising an aperture; and a photovoltaic module, configured
for electrical output power delivery, comprising a photo-active
area that extends in a second plane at a distance from the first
plane, the photo-active area being vis-à-vis the aperture, a
projection of the aperture perpendicularly to the second plane
corresponding to the photo-active area.
[0020] In another embodiment, an apparatus includes a photovoltaic
thermal hybrid solar receiver, the photovoltaic thermal hybrid
solar receiver comprising a thermal collector, extending in a
first plane and comprising an aperture, and a photovoltaic module,
configured for electrical output power delivery, comprising a
photo-active area that extends in a second plane at a distance
from the first plane, the photo-active area being vis-à-vis the
aperture, a projection of the aperture perpendicularly to the
second plane corresponding to the photo-active area; a
concentrator, arranged to concentrate radiation towards an optical
focus; and a positioning mechanism, wherein the receiver and/or
the concentrator are movably mounted in the apparatus via the
positioning mechanism, and wherein the positioning mechanism
allows for changing a ratio of an intensity of radiation received
at the photovoltaic module to an intensity of radiation received
at the thermal collector.
Adsorption heat exchanger devices
TW201321691
Adsorption heat exchanger devices (11, 30) are provided for solid
sorption refrigeration systems (1). Such a device includes a heat
exchanger (12) having a plurality of projections (17) arranged for
extending into an adsorbate of the system (1) in use. An
adsorption structure (13, 31) is formed on the heat exchanger (12)
for adsorption of said adsorbate. The adsorption structure (13,
31) comprises a plurality of elongate adsorption elements (20)
extending outwardly from each of said projections (17) of the heat
exchanger (12).
Electrochemically powered integrated
circuit package
CN103119713
The invention is notably directed to an integrated circuit package
(10c). Said package has a layer structure with ICs and electrodes
(17) arranged in electrical connection with a layer (16) of the
layer structure. The package further comprises one or more fluid
circuit sections (19), each meant to receive a respective
electrolyte solution (or two distinct solutions, see the dual flow
redox mode described below). Each solution involved has soluble
electroactive species. A fluid section is designed to receive and
allow an electrolyte solution to contact corresponding electrodes,
such as to supply power to the ICs, in operation. As electrodes
are integrated to the package, electrical power can be supplied
close to the ICs, thereby improving efficiency of the power
supply. Finally, as a liquid is involved in-situ, suitable heat
removal can be contemplated, it being noted that electrical power
delivery and heat removal needs are congruent.
COOLANT PUMPING SYSTEM FOR MOBILE
ELECTRONIC SYSTEMS
US2012273183
A coolant pumping system for a mobile electronic system includes a
coolant reservoir containing a coolant, a heat exchanger member
fluidly connected to the coolant reservoir, and a mass moveably
mounted to the mobile electronic system. The mass is moved along
at least one axis in response to at least one of accelerations and
orientation changes of the mobile electronic system. The coolant
system further includes a force transfer member operatively
connected between the mass and the coolant reservoir. The force
transfer member urges the coolant from the coolant reservoir
through the heat exchanger member in response to movements of the
mass. A gear member is operatively connected between the mass and
the force transfer member.
ADSORPTION HEAT EXCHANGER DEVICES
WO2013001391
Adsorption heat exchanger devices (11, 25) are provided for use in
solid sorption refrigeration systems (1) together with methods for
making such devices and adsorbent structures therefor. The methods
include applying a curable binder, in solution in a solvent, to
granular adsorbent material, and then evaporating the solvent and
curing the binder. The curable binder solution is sufficiently
dilute that, during evaporation of the solvent, the binder becomes
concentrated around contact points between granules (18) of the
adsorbent material whereby localized bonds (19) are formed around
the contact points on curing of the binder.
ADSORPTION HEAT EXCHANGER DEVICES
WO2013001390
Adsorption heat exchanger devices (11, 30) are provided for solid
sorption refrigeration systems (1). Such a device includes a heat
exchanger (12) having a plurality of projections (17) arranged for
extending into an adsorbate of the system (1) in use. An
adsorption structure (13, 31) is formed on the heat exchanger (12)
for adsorption of said adsorbate. The adsorption structure (13,
31) comprises a plurality of elongate adsorption elements (20)
extending outwardly from each of said projections (17) of the heat
exchanger (12).
LIGHT-REFLECTING GRATING STRUCTURE FOR
PHOTOVOLTAIC DEVICES
US2014060642
A photovoltaic cell includes an absorbing layer configured to
generate electron-hole pairs from incident photons of incoming
light; and a first grating layer arranged at a first surface of
the absorbing layer which is opposite to a second surface of the
absorbing layer from which light is incident, wherein the first
grating layer includes at least one grating extending along the
first surface, wherein the at least one grating has grating
structures which are dimensioned to provide a reflectivity for
light incident through the absorbing layer back into the absorbing
layer.
SOLID SORPTION REFRIGERATION
US2013340253
A method of making integrated adsorption and heat exchanger
devices for solid sorption refrigeration systems (1). An
integrated adsorption and heat exchanger device comprises a solid
material having formed therein both a porous adsorption structure,
which is pervious to an adsorbate of said system, and a heat
exchanger structure, which is impervious to said adsorbate, for
heat exchange with the porous adsorption structure in operation of
the system.
PHOTOVOLTAIC MODULE COOLING DEVICES
WO2013144750
Also published as: GB2500703 //
US2013255750
A chip module cooling device (25) is provided. The chip module
comprises two fluid circuits corresponding to an inlet fluid
circuit (i) and an outlet fluid circuit (o), respectively, wherein
each of the two fluid circuits comprises an arrangement of
orifices (Oi, Oo) and channel portions(CPi, CPo) forming a tree
structure, wherein branches of the tree structure represent the
orifices and nodes of the tree structure represent the channel
portions, a branch linking a node to one child node only, whereby
several nodes having a same parent node are sibling nodes. Each of
the two fluid circuits further extends through L levels (L1 - L3)
of said tree structure, with L>=3, and is in fluidic connection
with the other one of the two fluid circuits, via channel portions
corresponding to leaf nodes of the tree structure. For each of the
fluid circuits, channel portions corresponding to sibling nodes:
are parallel; are parallel to channel portions corresponding to a
grandparent node of said sibling nodes, if any; and are not
parallel to a channel portion corresponding to a parent node of
said sibling nodes. Finally, channel portions of one of the fluid
circuits are parallel to and interdigitated with channel portions
of the other one of the fluid circuits.