80% Efficiency conversion of IR to electricity.
Inventor: KOTTER DALE K // NOVACK STEVEN D [US]
Applicant: BATTELLE ENERGY ALLIANCE LLC [US]
EC: H01Q1/24E // H01Q21/06B
IPC: H01L31/0232
Abstract -- Energy
harvesting devices include a substrate coupled with a
photovoltaic material and a plurality of resonance elements
associated with the substrate. The resonance elements are
configured to collect energy in at least visible and infrared
light spectra. Each resonance element is capacitively coupled
with the photovoltaic material, and may be configured to
resonate at a bandgap energy of the photovoltaic material.
Systems include a photovoltaic material coupled with a
feedpoint of a resonance element. Methods for harvesting
energy include exposing a resonance element having a resonant
electromagnetic radiation having a frequency between
approximately 20 THz and approximately 1,000 THz, absorbing at
least a portion of the electromagnetic radiation with the
resonance element, and resonating the resonance element at a
bandgap energy of an underlying photovoltaic material. Methods
for forming an energy harvesting device include forming
resonance elements on a substrate and capacitively coupling
the resonance elements with a photovoltaic material.
Description
CROSS-REFERENCE TO RELATED
APPLICATIONS
[0001] This application is a continuation of U.S. patent
application Ser. No. 11/939,342, filed Nov. 13, 2007, which
will issue as
U.S. Pat. No.
8,071,931 on Dec. 6, 2011. This application is
related to U.S. patent application Ser. No. 13/179,329, filed
Jul. 8, 2011, which is a divisional of U.S. patent application
Ser. No. 11/939,342, filed Nov. 13, 2007, which will issue as
U.S. Pat. No. 8,071,931
on Dec. 6, 2011. This application is also related to U.S.
patent application Ser. No. 11/939,358 filed Nov. 13, 2007,
now
U.S. Pat. No. 7,792,644,
issued Sep. 7, 2010, entitled METHODS, COMPUTER READABLE
MEDIA, AND GRAPHICAL USER INTERFACES FOR ANALYSIS OF FREQUENCY
SELECTIVE SURFACES, and U.S. Provisional Patent Application
Ser. No. 60/987,630 filed Nov. 13, 2007, entitled ANTENNA
DEVICES COMPRISING FLEXIBLE SUBSTRATES, RELATED STRUCTURES,
AND METHOD OF MAKING AND USING THE SAME. The disclosures of
each of the above referenced applications are incorporated by
reference herein in their entireties.
GOVERNMENT RIGHTS
[0002] This invention was made with government support under
Contract No. DE-AC07-05-1D14517 awarded by the United States
Department of Energy. The government has certain rights in the
invention.
TECHNICAL FIELD
[0003] Embodiments of the present invention relate generally
to structures and methods for harvesting energy from
electromagnetic radiation and, more specifically, for
nanostructures and related methods and systems for harvesting
energy from, for example, the infrared, near-infrared and
visible spectrums and capturing millimeter and Terahertz
energy.
BACKGROUND
[0004] Conventionally, energy harvesting techniques and
systems are focused on renewable energy such as solar energy,
wind energy, and wave action energy. Solar energy is
conventionally harvested by arrays of solar cells, such as
photovoltaic cells, that convert radiant energy to DC power.
Such energy collection is limited in low-light conditions such
as at night or even during cloudy or overcast conditions.
Conventional solar technologies are also limited with respect
to the locations and orientations of installment. For example,
conventional photovoltaic cells must be installed such that
the light of the sun strikes them at specific angles such that
they are receiving relatively direct incident radiation.
[0005] Additionally, current photovoltaic cells are relatively
large and are limited in where they may be installed. As such,
while providing some utility in harvesting energy from the
electromagnetic radiation provided by the sun, current solar
technologies are not yet developed to take full advantage of
the potential electromagnetic energy available. Further, the
apparatuses and systems used in capturing and converting solar
energy are not particularly amenable to installation in
numerous locations or situations.
[0006] Moreover, photovoltaic cells are conventionally limited
to collection of energy in a very narrow band of light (e.g.,
approximately 0.8 micrometer to 0.9 micrometer ([mu]m)
wavelengths). The spectrum of potentially available
electromagnetic energy is much greater than the narrow band in
which conventional photovoltaic cells operate. For example,
electromagnetic energy provided by the sun falls within the
wavelength spectrum of approximately 0.1 [mu]m to
approximately 6 [mu]m. Additionally, energy absorbed by the
earth and reradiated (e.g., at night) falls within the
wavelength spectrum of approximately 3 [mu]m to approximately
70 [mu]m. Current energy harvesting technologies fail to take
advantage of such available energy.
[0007] Turning to another technology, frequency selective
surfaces (FSSs) are used in a wide variety of applications
including radomes, dichoric surfaces, circuit analog
absorbers, and meanderline polarizers. An FSS is a
two-dimensional periodic array of electromagnetic antenna
elements. Such antenna elements may be in the form of, for
example, conductive dipoles, loop patches, slots or other
antenna elements. An FSS structure generally includes a
metallic grid of antenna elements deposited on a dielectric
substrate. Each of the antenna elements within the grid
defines a receiving unit cell.
[0008] An electromagnetic wave incident on the FSS structure
will pass through, be reflected by, or be absorbed by the FSS
structure. This behavior of the FSS structure generally
depends on the electromagnetic characteristics of the antenna
elements, which can act as small resonance elements. As a
result, the FSS structure can be configured to perform as
low-pass, high-pass, or dichoric filters. Thus, the antenna
elements may be designed with different geometries and
different materials to generate different spectral responses.
[0009] Conventionally, FSS structures have been successfully
designed and implemented for use in radio frequency (RF) and
microwave frequency applications. As previously discussed,
there is a large amount of renewable electromagnetic radiation
available that has been largely untapped as an energy source
using currently available techniques. For instance, radiation
in the ultraviolet (UV), visible, and infrared (IR) spectra
are energy sources that show considerable potential. However,
the scaling of existing FSSs or other similar structures for
use in harvesting such potential energy sources comes at the
cost of reduced gain for given frequencies.
[0010] Additionally, scaling FSSs or other transmitting or
receptive structures for use with, for example, the IR or
near-IR spectra presents numerous challenges due to the fact
that materials do not behave in the same manner at the
so-called "nano-scale" as they do at scales that enable such
structures to operate in, for example, the radio frequency
(RF) spectra. For example, materials that behave homogenously
at scales associated with the RF spectra often behave
inhomogenously at scales associated with the IR or near-IR
spectra.
[0011] There remains a desire in the art to improve upon
existing technologies and to provide methods, structures and
systems associated with harvesting energy including
structures, methods and systems that provide access to greater
bands of the electromagnetic spectrum and, thus greater access
to available, yet-unused energy sources.
BRIEF SUMMARY OF THE
INVENTION
[0012] In one embodiment of the present invention, an energy
harvesting device is provided. The energy harvesting device
includes a substrate and at least one resonance element
associated with the substrate. The at least one resonance
element is configured to have a resonant frequency between
approximately 20 THz and approximately 1,000 THz. A layer of
conductive material substantially covers a surface of the
substrate. An optical resonance gap extends a distance between
the at least one resonance element and the layer of conductive
material of approximately one-quarter wavelength of a
wavelength of the at least one resonance element's resonant
frequency. At least one energy transfer element is associated
with the at least one resonance element.
[0013] In accordance with another embodiment of the present
invention, another energy harvesting device is provided. The
energy harvesting device includes a ground plane, a first
substrate disposed on a first side of the ground plane and a
second substrate disposed on a second, opposing side of the
ground plane. At least a first resonance element is associated
with the first substrate and located on the first side of the
ground plane. The first resonance element is sized and
configured to have a resonant frequency between approximately
20 THz and approximately 1,000 THz. At least a second
resonance element is associated with the second substrate and
located on the second, opposing side of the ground plane. The
second resonance element is sized and configured to have a
resonant frequency different from the resonant frequency of
the at least a first resonance element.
[0014] In accordance with yet another embodiment of the
present invention, a method of harvesting energy is provided.
The method includes providing at least one resonance element
formed of an electrically conductive material and having a
resonant frequency between approximately 20 THz and
approximately 1,000 THz. The at least one resonance element is
exposed to electromagnetic radiation having a frequency
substantially the same as the resonant frequency. At least a
first portion of the electromagnetic radiation is absorbed by
the at least one resonance element. At least a second portion
of the electromagnetic radiation is reflected off of a defined
surface. At least a portion of the at least a second portion
of the electromagnetic radiation is absorbed by the at least
one resonance element. Induced AC (alternating current) energy
is transferred via an energy transfer element.
[0015] In accordance with another embodiment of the present
invention, another method of harvesting energy is provided.
The method includes providing at least one resonance element
formed of an electrically conductive material and exposing the
at least one resonance element to electromagnetic radiation
radiated from the earth. Resonance is induced in the at least
one resonance element to produce AC energy. The AC induced
energy is transferred from the at least one resonance element
via at least one energy transfer element.
BRIEF DESCRIPTION OF THE
SEVERAL VIEWS OF THE DRAWINGS
[0016] FIG. 1 is a partial
plan view of a device including an array of elements used to
harvest energy from electromagnetic radiation in accordance
with an embodiment of the present invention;
[0017] FIG. 2 is a
cross-sectional view of a portion of the device as indicated
by section line 2-2 as shown in FIG. 1;
[0018] FIG. 3 is a plan view
of another element used to harvest energy from
electromagnetic radiation in accordance with an embodiment
of the present invention;
[0019] FIG. 4 is an array of
elements shown in FIG. 3;
[0020] FIG. 5 is a partial
plan view of a device used to harvest energy from
electromagnetic radiation in accordance with an embodiment
of the present invention;
[0021] FIG. 6 is a
cross-sectional view of a portion of the device as indicated
by section line 6-6 as shown in FIG. 5;
[0022] FIG. 7 is a
cross-sectional view of a portion of a device used to
harvest energy from electromagnetic radiation in accordance
with another embodiment of the present invention;
[0023] FIG. 8 is a schematic
of a system incorporating energy harvesting structures in
accordance with another embodiment of the present invention;
[0024] FIG. 9 is a
cross-sectional view of certain components of a device for
converting energy in accordance with an embodiment of the
present invention;
[0025] FIG. 10 is a
perspective view of a device for converting energy in
accordance with an embodiment of the present invention;
[0026] FIGS. 11A and 11B are
schematic views, including cross-sectional views of certain
components, of an energy transfer device in accordance with
an embodiment of the present invention;
[0027] FIG. 12 is a
perspective, partial cross-sectional view of an energy
transfer device in accordance with an embodiment of the
present invention;
[0028] FIG. 13 is a schematic
view of a device according to an embodiment of the present
invention; and
[0029] FIG. 14 is a schematic
view, including a cross-sectional view of certain
components, of an energy transfer device in accordance with
an embodiment of the present invention.
DETAILED DESCRIPTION OF THE
INVENTION
[0030] In the following detailed description, reference is
made to the accompanying drawings which form a part hereof,
and in which is shown by way of illustration specific
embodiments in which the invention may be practiced. These
embodiments are described in sufficient detail to enable those
of ordinary skill in the art to practice the invention. It
should be understood; however, that the detailed description
and the specific examples, while indicating examples of
embodiments of the invention, are given by way of illustration
only and not by way of limitation. From this disclosure,
various substitutions, modifications, additions,
rearrangements, or combinations thereof within the scope of
the present invention may be made and will become apparent to
those skilled in the art.
[0031] Embodiments of the present invention provide methods,
structures and systems for harvesting energy from
electromagnetic radiation including, for example, harvesting
energy from radiation in the infrared, near-infrared and
visible light spectra.
[0032] Nano electromagnetic concentrator (NEC) structures may
include an array or other periodic arrangement of resonant
structures (also referred to as antennas, micro-antennas, and
nano-antennas). It is noted that NEC structures may include,
but are not limited to, FSS structures. Generally, the NEC
structures may be formed by a conductive material formed in a
specific pattern on a dielectric substrate to create the
resonance elements. These NEC structures may be used for
spectral modification of reflected or transmitted incident
radiation. The resonant properties of these structures are
largely dependent on the structure's layout in terms of shape,
dimension, periodicity, the structure's material properties,
and optical parameters of the surrounding media. It has been
demonstrated that by varying the NEC geometry, material
properties, or combinations thereof, it is possible to tune
the resonance of an NEC structure to meet specific design
requirements. However, as previously noted, attempts to scale
NEC structures for use in, for example, the infrared (IR),
near-IR and visible light spectra have posed particular
problems because of the inhomogenous behavior of materials at
the scales necessary to function at such wavelengths and
frequencies.
[0033] Referring to FIG. 1, a partial plan view, or top view,
of an energy harvesting device 100 is shown that includes
various resonance structures or elements 102 (sometimes
referred to herein as nanoantennas) formed in a substrate 104.
In the embodiment described with respect to FIG. 1, the
resonance elements 102 are shown as exhibiting substantially
square loop geometries. However, as will be shown with other
embodiments described herein, the resonance elements 102 may
exhibit other geometries and the example embodiments described
herein are not to be taken as limiting with respect to such
potential geometries.
[0034] With continued reference to FIG. 1, FIG. 2 is a
cross-sectional view of the device 100 shown in FIG. 1. As
seen in FIG. 2, the resonance elements 102 may be partially
disposed within the substrate 104. In other embodiments, such
resonance elements 102 may be substantially on an exterior
surface of substrate 104. A ground surface or ground plane 106
may be formed, for example, on a surface of the substrate 104
at a desired distance from the resonance elements 102.
Cavities 108 may be formed in the substrate 104 between
resonance elements 102 and the ground plane 106. In one
embodiment, the cavities 108 may be substantially unfilled
(or, in other words, filled with air), or they may be filled
with a desired substance, including dielectric material 110,
that exhibits, for example, one or more desired optical
properties or characteristics. In one embodiment, the distance
S extending between the resonance elements 102 and the ground
plane 106 (which distance may also be the height of the
cavities 108), may be approximately equal to one-quarter
([1/4]) of a wavelength of an associated frequency at which
the resonance elements 102 are intended to resonate. This
spacing forms what may be termed an optical resonance gap or
an optical resonance stand-off layer between the resonance
elements 102 and the ground plane 106.
[0035] The resonance elements 102 may be formed of an
electrically conductive material. The conductive material may
include, for example, a metal or combination of metals such as
manganese (Mn), gold (Au), silver (Ag), copper (Cu), aluminum
(Al), platinum (Pt), nickel (Ni), iron (Fe), lead (Pb), tin
(Sn), or any other suitable electrically conductive material.
In one embodiment, the conductivity of the material used to
form the resonance elements 102 may be from approximately
1.0*10<6 >Ohms<-1>-cm<-1 >to approximately
106.0*10<6 >Ohms<-1>-cm<-1>.
[0036] Additionally, as noted above, the resonance elements
102 may exhibit a variety of geometries. As non-limiting
examples, such geometries may include circular loops,
concentric loops, square spirals, circular spirals, slots, and
crosses. Moreoever, an energy harvesting device 100 may
include numerous different geometries of resonance elements
102 formed on or in the substrate 104.
[0037] The substrate 104 of the device 100 may include a
dielectric material. As non-limiting examples, the substrate
104 may comprise a semiconductor-based material including
silicon, silicon-on-insulator (SOI) or silicon-on-sapphire
(SOS) technology, doped and undoped semiconductor materials,
epitaxial layers of silicon supported by a base semiconductor
foundation, and other semiconductor structures. In addition,
the semiconductor material need not be silicon-based, but may
be based on silicon-germanium, silicon-on-insulator,
silicon-on-sapphire, germanium, or gallium arsenide, among
others.
[0038] As other non-limiting examples, the substrate 104 may
comprise a flexible material selected to be compatible with
energy transmission of a desired wavelength, or range of
wavelengths, of light. The substrate 104 may be formed from a
variety of flexible materials such as a thermoplastic polymer
or a moldable plastic. By way of other non-limiting examples,
the substrate 104 may comprise polyethylene, polypropylene,
acrylic, fluoropolymer, polystyrene, poly methylmethacrylate
(PMMA), polyethylene terephthalate (MYLAR(R)), polyimide
(e.g., KAPTON(R)), polyolefin, or any other material suitable
for use as a substrate 104. In additional embodiments, the
substrate 104 may comprise a binder with nanoparticles
distributed therein, such as silicon nanoparticles distributed
in a polyethylene binder, or ceramic nanoparticles distributed
in an acrylic binder. Any type of substrate 104 may be used as
long as it is compatible with the transmission of a desired
wavelength within the spectrum of electromagnetic radiation.
[0039] The ground plane 106 may also be formed of an
electrically conductive material. The conductive material may
include, for example, a metal or combination of metals such as
manganese (Mn), gold (Au), silver (Ag), copper (Cu), aluminum
(Al), platinum (Pt), nickel (Ni), iron (Fe), lead (Pb), tin
(Sn), or any other material suitable for use as an
electrically conductive material. The ground plane 106 may
also exhibit surface properties that make it a good optical
reflector, with minimal diffusion and scattering of the
electromagnetic energy. In one embodiment, the conductivity of
the material used to form the resonance elements 102 may be
from approximately 40.0*10<6 >Ohms<-1>-cm<-1
>to approximately 106.0*10<6
>Ohms<-1>-cm<-1>. Additionally, the ground
plane 106 may exhibit a reflectivity of approximately 95% or
greater over the full bandwidth of intended operation of the
device 100.
[0040] As noted hereinabove, in one embodiment, the cavities
108 may simply be filled with air. The use of air may provide
desirable performance characteristics of the device 100 with
respect to optical refraction and permittivity at locations
extending immediately between the resonance elements 102 and
the ground plane 106. However in other embodiments, a
dielectric material 110 may be disposed within the cavity 108.
For example, the cavities 108 may include a material 110 such
as silicon nanoparticles dispersed in a polyethylene binder,
silicon dioxide (SiO2), alumina (Al2O3), aluminum oxynitride
(AlON), or silicon nitride (Si3N4). In additional embodiments,
material such as polymers, rubbers, silicone rubbers,
cellulose materials, ceramics, glass, or crystals may be
disposed in the cavities 108.
[0041] In some embodiments, an overcoat or protective layer
may be formed on one or more surfaces of the device 100. For
example, a protective layer 112 (shown by dashed lines in FIG.
2) may comprise a flexible material such as polyethylene,
silicon nanoparticles dispersed in a polyethylene binder,
polypropylene, MYLAR(R) polymer, or KAPTON(R) polymer. In some
embodiments, the protective layer 112 may be configured to
protect one or more components of the device 100 from
environmental damage, such as corrosion caused by moisture or
caustic chemicals. The material used to form the protective
layer 112 may be based on desired electro-optic properties so
as to enhance transmission, or at least not impede
transmission, of electromagnetic radiation to the resonance
elements 102, the ground plane 106 and the cavities 108. In
this manner, the overcoat may be used to emulate environmental
conditions that could otherwise influence the resonance
properties of the resonance elements 102.
[0042] It is noted that, in some instances, the protective
layer 112 might introduce some undesirable behavior in the
solar region, including trapped antenna grating lobes
resulting in loss of energy and a reduction in
omni-directional reception of solar energy or other
electromagnetic radiation. As such, an anti-reflective coating
may be used to compensate for these undesirable features in
accordance with one embodiment of the present invention.
[0043] In one embodiment, a coating may be applied as a final
"top coat" and may be sputtered on using, for example, a
plasma-enhanced chemical vapor deposition (PECVD) process. The
coating may be applied as a thin-film having a tailored
refractive index. Materials from which the top coat may be
formed include, for example, silicon nitride, titanium
dioxide, and amorphous silicon. The thickness of the
protective layer 112 may be selected to produce destructive
interference in undesired reflected energy and constructive
interference in the desired transmitted energy. In some
embodiments, protective layer 112 may be manufactured as a
separate layer and subsequently over-laid and adhered to the
device 100.
[0044] The energy harvesting device 100 may be manufactured
using a variety of techniques including a variety of
semiconductor fabrication techniques, nanofabrication
techniques and other processes as will be recognized by those
of ordinary skill in the art depending, in part, on the
materials used to form the device 100.
[0045] Still referring to FIGS. 1 and 2, one particular
embodiment of the invention may include a substrate 104 formed
of polyethylene, with the resonance elements 102 and the
ground plane 106 formed of gold. The cavities 108 may be
filled with air or with a material 110 including silicon
nanoparticles dispersed in a polyethylene binder. It is noted
that the use of polyethylene as a substrate 104 (or other
similar material) provides the device 100 with flexibility
such that it may be mounted and installed in a variety of
locations and adapted to a variety of uses.
[0046] The dimensions of the various components may vary
depending, for example, on the frequency at which the
resonance elements 102 are desired to resonate and the
materials used to form the various components of the device
100. For example, in one embodiment, the thickness H of the
substrate 104 may be from 3 [mu]m to approximately 15 [mu]m.
The width W of the traces or individual elements forming the
resonance elements 102 may be from approximately 100
nanometers (nm) to approximately 400 nm. In one particular
example, the width W may be from approximately 200 nm to
approximately 300 nm. The thickness T of the resonance
elements 102 may be from approximately 30 nm to approximately
150 nm. The inside length L between traces or individual
elements of a given resonance element 102 may be from
approximately 1 [mu]m to approximately 10 [mu]m. The distance
X between individual resonance elements 102 may be from
approximately 100 nm to approximately 400 nm. In one
particular example, the distance X between resonance elements
102 may be from approximately 200 nm to approximately 300 nm.
The thickness Y of the ground plane 106 may be approximately
20 nm to approximately 1 [mu]m.
[0047] Various geometries and dimensions of components of the
device 100 may be determined, for example, using appropriate
modeling techniques. For example, copending U.S. Pat. No.
7,792,644, titled "METHODS, COMPUTER READABLE MEDIA, AND
GRAPHICAL USER INTERFACES FOR ANALYSIS OF FREQUENCY SELECTIVE
SURFACES," describes a method of analyzing structures and
components that may be used as an NEC (such as the device 100
of the presently described embodiments) and determining the
response of such structures using, in one example, a Periodic
Method of Moments analysis and taking into consideration a
number of different variables such as anticipated operational
frequencies, material properties, and component dimensions.
[0048] During operation of the energy harvesting device 100,
the device 100 may be exposed to electromagnetic radiation
such as, for example, that which is provided by the sun or
that which is reradiated by the earth after having absorbed
energy from the sun. Some of the radiation will be absorbed by
the resonance elements 102 as incident radiation and as
indicated by reference numeral 120. In one embodiment, the
resonance elements 102 are configured to resonate at a
frequency that corresponds with the frequency of the radiation
to which the energy harvesting device 100 is exposed. For
example, the resonance elements 102 may be configured to
resonate at a frequency in one of the infrared, near-infrared,
or visible light spectra. In one embodiment, the resonance
elements 102 may be configured with a resonant frequency of
between approximately 20 Terahertz (THz) and approximately
1,000 THz (or at wavelengths of approximately 0.3 [mu]m to
approximately 15.0 [mu]m), which corresponds generally to the
visible to the mid-infrared spectrum.
[0049] As such, an electrical resonance takes place in the
resonance elements 102 such that electrons on the surface of
the resonance elements 102 oscillate and produce an electrical
current. Radiation that is not immediately absorbed by the
resonance elements 102 may pass through the substrate 104 and
reflect off of the ground plane 106. Some of the reflected
radiation may then be absorbed by the resonance elements 102
as indicated by reference numeral 122. Some of the radiation
that is reflected, but not immediately absorbed, may resonate
within the optical resonance gap as indicated by reference
numeral 124. The optical resonance gap or stand-off layer
helps to increase the efficiency of the energy captured or
absorbed by the resonance elements 102.
[0050] As schematically indicated in FIGS. 1 and 2, an energy
transfer element 130, as shown by dashed lines, may be
associated with the resonance elements 102 to assist in
harvesting the energy produced by the resonance elements 102
when exposed to electromagnetic radiation at the appropriate
frequency. For example, the energy transfer element 130 may
include a capacitor structure coupled with a resonance element
102 so as to develop a charge based on the current produced
within the associated resonance element 102. Such an energy
transfer element 130 may, for example, be disposed adjacent a
resonance element 102 such as adjacent or within an associated
cavity 108. As noted above, the energy transfer element 130 is
shown schematically in FIGS. 1 and 2. Additional details
regarding potential embodiments utilizing more specific
embodiments of energy transfer elements are discussed
hereinbelow.
[0051] In one embodiment, there may be an energy transfer
element 130 associated with each resonance element 102 and a
plurality of energy transfer elements 130 may be coupled
together to a common storage device, such as a battery, or to
processing equipment such as a system for converting or
conditioning the power provided by the resonance elements 102
and the plurality of energy transfer elements 130. In another
embodiment, multiple resonance elements 102 may be
electrically coupled with a common energy transfer element
130. In one such embodiment, a plurality of resonance elements
102 may have feedpoints coupled to a common energy transfer
element 130.
[0052] Turning now to FIG. 3, a resonance element 102'
according to another embodiment of the present invention is
shown. The resonance element 102' may be configured to exhibit
a geometry of what may be termed square or angular spirals.
Such spirals may include a first portion 140 that spirals
inwardly to a termination point 142 and a second portion 144
that is essentially a reversed image (both vertically and
horizontally) and spirals inwardly to a termination point 146.
The first portion 140 and the second portion 144 are
cooperatively interleaved with one another such that their
respective termination points 142 and 146 are positioned
proximate one another. The termination points 142 and 146 may
act as feedpoints for an energy transfer element 130' such as
further described hereinbelow.
[0053] As shown in FIG. 4, an array of resonance elements 102'
may be used to form an apparatus configured generally
similarly to the embodiment previously described with respect
to FIGS. 1 and 2. For example, while not specifically shown in
FIGS. 3 and 4, the resonance elements 102' may be disposed on
or in a substrate material that has a ground plane associated
therewith. Additionally, optical resonance gaps or stand-off
layers may be formed in the substrate material and associated
with the resonance elements 102'. Such resonance elements 102'
may be sized and configured to resonate at a desired frequency
(e.g., at a frequency in the visible, IR or near-IR spectra or
at frequencies or wavelengths described elsewhere herein).
Similarly, optical resonance gaps or stand-off layers may be
configured in accordance with an identified frequency of
radiation at which the apparatus is intended to be exposed. A
density of resonance elements on the array may be from
approximately fifty billion per square meter to approximately
one hundred ten billion per square meter.
[0054] Turning now to FIGS. 5 and 6, another embodiment of an
apparatus 200 is shown. The apparatus 200 may include one or
more resonance elements 102 exhibiting a first configuration
(e.g., exhibiting a desired geometry, size, material property
or combination thereof) and one or more resonance elements 202
exhibiting a second configuration. For the sake of convenience
and clarity in describing such an embodiment, only one of each
configuration of resonance elements 102 and 202 is shown.
[0055] In the embodiment shown, one resonance element 202 may
be nested within the other resonance element 102, although in
other embodiments the resonance elements 102 and 202 may be
positioned laterally adjacent to one another or in other
spatial arrangements. In one embodiment, such as shown in
FIGS. 5 and 6, each of the resonance elements 102 and 202 may
exhibit similar geometries but different dimensions. In
another embodiment, while not specifically shown, a first
resonance element may be configured to exhibit a different
geometry than that of a second resonance element. For example,
a first resonance element may be configured as a loop, while a
second resonance element may be configured as a spiral.
[0056] As previously described, a cavity 108 may be associated
with the resonance element 102 of the first configuration.
Likewise, a cavity 208 may be associated with the resonance
element 202 exhibiting the second configuration. The two
resonance elements 102 and 202, along with their associated
cavities 108 and 208, may be located on the same side of a
common ground plane 206, as shown in FIG. 6. The two different
resonant elements 102 and 202 may be spaced different
distances from the common ground plane 106 so as to
effectively define two different optical resonant gaps or
stand-off layers.
[0057] The two resonance elements 102 and 202 are configured
to resonate at different frequencies. For example, in one
embodiment, one array of resonance elements may be configured
to resonate at a frequency associated with visible light,
while another array of resonance elements may be configured to
resonate at frequencies associated with what may be referred
to as "long wavelength IR." Thus, the two resonance elements
102 and 202 may provide an ability to simultaneously harvest
energy at multiple, substantially different frequencies, or to
harvest energy at substantially different frequencies at
different times based on anticipated changing radiation
conditions.
[0058] Referring briefly to FIG. 7, a cross-sectional view of
an apparatus 300 in accordance with yet another embodiment of
the present invention is shown. The apparatus 300 includes one
or more resonance elements 102 of a first configuration (e.g.,
exhibiting a desired geometry, size, material property or
combination thereof) and one or more resonance elements 302
exhibiting a second configuration. For the sake of convenience
and clarity in describing such an embodiment, only one of each
configuration of resonance elements 102 and 302 is shown.
[0059] As previously described, a cavity 108 may be associated
with the resonance element 102 of the first configuration.
Likewise, a cavity 308 may be associated with the resonance
element 302 exhibiting the second configuration. The first
resonance element 102 and associated cavity 108 (or the
plurality of resonance elements 102 and associated cavities
108) may be associated with a first substrate 304A located on
a first side of a ground plane 306 while the second resonance
element 302 and associated cavity 308 (or plurality thereof)
may be associated with another substrate 304B located on an
opposing side of the ground plane 306.
[0060] The two resonance elements 102 and 302 are configured
to resonate at different frequencies. Being on opposite sides
of the ground plane 306, the resonance elements 102 and 302
are also oriented for exposure to different sources of
radiation. For example, the resonance element or elements 102
of the first configuration may be configured and oriented to
harvest energy based on incident radiation from the sun. On
the other hand, the resonance element or elements 302 of the
second configuration may be configured and oriented to harvest
energy that is reradiated from the earth (e.g., at nighttime).
Such an apparatus 300 would enable collection of energy from
dual sources at different frequencies and being transmitted
from different locations.
[0061] As will be appreciated by those of ordinary skill in
the art, the different embodiments described herein may be
combined or modified in a variety of ways. For example, the
embodiments described with respect to FIGS. 6 and 7 may be
combined such that multiple different configurations of
resonance elements 102, 202, 302 may be disposed in or on the
associated substrates (e.g., substrates 104, 304A and 304B).
Additionally, when multiple resonance elements are being
utilized, different geometries may be intermixed in a device.
In other words, a single device may include a variety of
combinations of geometries including those previously
described herein.
[0062] Referring now to FIG. 8, a block diagram is shown of an
illustrative energy harvesting system 400 according to an
embodiment of the present invention. The energy harvesting
system 400 includes device 100, and apparatus 200, 300 that
capture and concentrate electromagnetic radiation at desired
resonant frequencies. The system 400 may further include at
least one energy conversion element 402 (that may include
energy transfer elements 130 or 130', FIGS. 1-3), which may
convert and transfer the electromagnetic energy captured by
the device 100, and apparatus 200, 300 during the harvesting
process. The system 400 may further comprise an energy storage
device 404 such as, for example, a lithium or polymer-form
factor battery. In one example, the energy storage device 404
may be trickle-charged by voltage from the energy conversion
element 402. The system 400 may further include a power
management system 406 for controlling the flow of energy
between the energy conversion element 402 and the energy
storage device 404. The energy storage device 404 may also be
operatively coupled to an external component or system
requiring energy (not shown). In some embodiments, one or more
systems 400 may be coupled to provide higher currents or
voltages as desired.
[0063] Referring now to FIG. 9, a schematic is shown (showing
cross-sections of certain components) of an energy conversion
system 450 according to one embodiment of the invention. The
energy conversion system 450 includes antenna elements 452 (or
resonance elements) parasitically coupled to a capacitive
storage element 458. The antenna elements 452 may be
configured as a dipole planar array.
[0064] Capacitive coupling is the transfer of energy within an
electrical network by means of the capacitance between circuit
nodes. Parasitic capacitive coupling can be effected by
placing two conductors within close enough proximity such that
radiated E-fields crosstalk. Such a system is generally
analogous to a charge-coupled device (CCD). Thus, the transfer
of Terahertz current from the antenna elements 452 does not
require a direct or "physical" electrical connection (e.g., a
wire or conductive trace).
[0065] The antenna element 452 has a known resistance, such
resistance being a function of sheet resistance of, for
example, a bulk metal of which the antenna element 452 is
fabricated. Electromagnetic energy, as shown by arrows in FIG.
9, impinges on the antenna elements 452 and induces surface
currents. The currents propagate to the center feedpoint 456
of each antenna element 452. Each antenna element 452 has a
dedicated and electrically isolated capacitive plate 460 that
serves as a node for collection of charge, which is
proportional to the electromagnetic energy intensity that is
exciting the antenna element 452 to a resonance condition. An
E-field transfers energy from the center feedpoint 456 to a
capacitive plate 458. The capacitive plates 458 and 460 share
a common dielectric region 462 and a common underlying grid or
plate 464. In effect this serves as a capacitor array, and
accumulates an electric charge.
[0066] The rate of charge of the capacitor array is a function
of the RC (resistance-capacitance) time constant of the
system. This time constant is determined by the antenna
impedance and capacitance of an associated storage element.
The time constant is the time required for the charge (or
discharge) current to fall to 1/e being Euler's number or the
natural logarithm base) of its initial value. After
approximately five time constants the capacitor is 99%
charged. The capacitor will charge and discharge as the THz
alternating current fluctuates.
[0067] At some period associated with the rate of charge, a
control circuit will transfer the collected charge into an
amplifier that converts the charge into a voltage. The control
circuit may be implemented with conventional electronic
circuitry as will be appreciated by those of ordinary skill in
the art. The charge circuit, in effect, rectifies the THz
current. The power may be further filtered, conditioned and
stored for long-term use. Multiple devices may be
interconnected in series to increase wattage.
[0068] Referring to FIG. 10, a perspective view is shown of an
energy conversion system 500 according to another embodiment
of the present invention. The energy conversion system 500
includes antenna elements directly coupled to capacitive
storage elements. The antenna elements may include an array of
apertures or slots 502 configured as antenna structures. The
slots 502 may be formed, for example, by systematic removal of
material from a substantially uniform conductive sheet 506.
The electric field induced in a slot by an incident
electromagnetic wave is equivalent to magnetic current
density. A voltage distribution results that can be used for
capacitive storage of energy.
[0069] As noted above, the slots 502 may be fabricated into an
electrically conductive layer 506. This electrically
conductive layer 506 may also function as an upper capacitive
plate. The capacitive storage device is completed by placing a
dielectric material 508 between the slot layer 506 and an
electrically conductive material layer 510 (which may also
serve as a ground plane of the energy conversion system 500,
such as discussed hereinabove). In one embodiment, the
dielectric material 508 may exhibit a thickness (i.e., the
distance between the slot layer 506 and the electrically
conductive material layer 510) that is a quarter ([1/4])
wavelength of the wavelength of radiation (shown by arrows)
that is anticipated to impinge on the energy conversion system
500. This thickness provides an optical resonance gap or
stand-off layer to properly phase the electromagnetic wave for
maximum absorption in the antenna plane. Additionally, the
dielectric material 508 exhibits a desired permittivity to
enable concentration and storage of electrostatic lines of
flux.
[0070] The capacitance is proportional to the surface area of
the conductive plates (506 and 510) and the permittivity of
the dielectric material 508. Due to the resonance behavior of
the slot antennas, a charge will accumulate on the upper
capacitor plate (slot layer 506). A voltage develops across
the slot layer 506 and the electrically conductive material
layer 510. When there is a difference in electric charge
between the plates or layers 506 and 510, an electric field is
created in the region therebetween, the electric field being
proportional to the amount of charge that has been moved from
one plate to the other.
[0071] The presently described embodiment provides the ability
to directly acquire a capacitor voltage by electrical
discharge across the capacitor. The slot layer 506 is
configured as a continuous conductor, rather than as the
discrete conducting elements, such as have been described with
respect to other embodiments hereinabove. The slot layer 506
serves as the upper electrode and the electrically conductive
material layer 510, or ground plane, serves as the lower
electrode. The dielectric material 508 serves as the stand-off
layer. A control circuit will transfer the collected voltage
to a storage device (not shown). The control circuit may be
implemented with conventional electronic circuitry components
known to those of ordinary skill in the art. As with other
embodiments described herein, multiple devices may be
interconnected in series to increase wattage.
[0072] Referring to FIGS. 11A and 11B, schematics are shown of
an energy conversion system 550 according to another
embodiment of the present invention. The energy conversion
system 550 includes one or more antenna elements 552 with a
rectifier diode element 554 embedded into the antenna element
552. At optical frequencies, the skin depth of an
electromagnetic wave in metals is just a few nanometers. This
results in a high resistivity causing THz AC (alternating
current) currents to dissipate in the form of Joule heating if
the transmission line is over a few microns in length. To
reduce transmission losses the AC current is substantially
immediately rectified. Rectification may be performed using a
metal-semiconductor-metal Schottky junction. THz radiation
excites surface current waves in the antenna elements 552. The
received AC waves are rectified to DC (direct current) with
the rectifier diode element 554.
[0073] Conventional rectification devices are not suitable for
use at the frequencies at which the antenna elements 552 will
resonate. Rather, the rectification of electromagnetic waves
at the high frequency range of THz radiation is performed with
using metal-on-metal (MoM) Schottky-diodes. Such MoM devices
include a thin barrier layer and an oxide layer sandwiched
between two metal electrodes. An MoM device works when a large
enough field causes the tunneling of electrons across the
barrier layer. A difference in the work function between the
metal Schottky junctions results in high speed rectification.
Examples of MoM materials include Au-Si-Ti and InGaAs/InP.
[0074] The increased cutoff frequency (to THz) is achieved by
reducing the diode capacitance to the atto-farad range and
also by reducing contact resistance. This is achieved by
forming a gate region on the order of, for example, 30 nm in a
T-gate configuration. Due to the small junction area, it is
believed that low enough junction capacitance will be
maintained to sustain THz-rate switching times.
[0075] Components may be impedance matched to ensure maximum
power transfer between components, to minimize reflection
losses, and achieve THz switch speeds. Proper impedance
matching may be achieved by connecting the feedpoint of the
antenna structure through a co-planar strip (CPS) transmission
line 556 to the rectifier diode elements 554. The output of
the rectifier diode elements 554 may be DC coupled together.
In one embodiment, the rectifier diode elements 554 may be
interconnected in series, resulting in a summation of DC
voltage. This enables the use of a common power bus 558.
[0076] It is noted that in certain embodiments, such as the
one described with respect to FIGS. 11A and 11B, the
collection elements (i.e., the antenna or resonance elements)
may have a termination or feedpoint such as has been described
herein, and that electrical current is transferred from the
collection element (e.g., antenna element 552) to the transfer
or conversion element (e.g., rectifier diode element 554). The
current produced by the collection element is AC with a
sinusoidal frequency of between 10<12 >and 10<14
>hertz. The high-efficiency transmission of electrons along
a wire at THz frequencies is not a conventional practice.
Thus, as described with respect to FIGS. 11A and 11B, this may
be accomplished through the use of a co-planar strip
transmission line (e.g., transmission line 556) that is
specifically designed for high speed and low propagation loss.
[0077] Conventional design methods commonly used to design
strip transmission lines at microwave frequencies are not
fully valid at IR frequencies. Thus, frequency dependent
modeling may be employed to characterize transmission line
behavior such as has been indicated hereinabove with respect
to other components of various embodiments. At THz frequencies
the propagating electromagnetic field is not totally confined
to the conductor. The resulting dispersive nature of the
E-fields may result in potential losses from impacts of the
surrounding media, including stray leakage through dielectric
materials and substrate boundaries. Design of the CPS takes
into account, for example, impedance matching to reduce
standing wave ratio (SWR) and tailoring permittivity of
adjacent media to reduce refraction in order to improve power
transfer from the antenna elements to the conversion elements
and improve the efficiency of the device.
[0078] It is noted that the CPS conductor size and spacing
between the balanced transmission lines also impact
characteristic impedance. The optical properties of the strip
line metal, including index of refraction (n) and extinction
coefficient (k) may be analyzed and used to derive frequency
dependent conductivity properties. Tailoring the physical
design of the strip line helps to maximize power transfer. The
strip line may be designed to match the impedance of the
antenna to the impedance of the conversion element. In another
embodiment, to further reduce transmission line loss, the
conversion element may be physically located substantially
co-planar with the antenna.
[0079] Referring to FIG. 12, a perspective, partial
cross-sectional view is shown of an energy conversion system
600 system according to another embodiment of the present
invention. The energy conversion system 600 may include
antenna elements 602 formed on a thin film substrate 604. The
thin film substrate 604 may include a flexible material such
as, for example, polyethylene. A ground plane is not utilized
in this embodiment. The antenna elements 602 may be configured
to collect electromagnetic radiation in the visible and
infrared bands. As shown in FIG. 12, the antenna elements 602
may include spiral loop antenna elements having a central
feedpoint 606. The complementary geometry of the antenna
elements 602 generate surface currents that are additive and
focus radiant energy at the central feedpoint 606 of the
antenna elements 602. A photovoltaic (PV) material 608 may be
placed in proximity to the antenna's feedpoint 606 for
conversion of the energy collected by the antenna elements
602.
[0080] In the currently described embodiment, the thin-film
substrate 604 and associated antenna elements 602 may be
overlaid, laminated or bonded to photovoltaic (PV) material
608, which may include, for example, commercially available PV
materials. The antenna elements 602 capture and focus energy
(shown by arrows) into each associated feedpoint 606 of each
antenna element 602 analogous to the focal point of an optical
lens. The antenna elements 602 are designed for resonance at
the bandgap energy of the PV material 608. The concentrated,
radiant energy is capacitively coupled (no direct wiring
required) to the PV material 608. This induces electron-hole
transfer in the PV material 608 and initiates the solar energy
conversion process. Conventional methods used to collect and
store DC energy from the PV material 608 may then be
implemented.
[0081] The use of antenna elements (e.g., micro-antennas or
nano-antennas), with an omni-directional field-of-view, such
as provided by the antenna elements described herein, enables
modification of the angular reception characteristics of
conventional solar cells, leading to higher collection
efficiency independent of the angle of incidence of the sun.
It is further noted that a-Si, amorphous silicon (a leading
material for PV) has an intrinsic light induced degradation.
In the presently described embodiment, the antenna layer
serves as a "top coat" or protective layer for the PV material
608 providing environmental protection and reducing the
effects of degradation.
[0082] Referring to FIG. 13, a schematic is shown of an energy
conversion system 650 according to another embodiment of the
present invention. In this embodiment, an antenna element 652
may have a PV material 654 embedded in, or coupled with, the
feedpoint 656 thereof. The THz currents of the antenna element
652 are directly coupled to the PV material 654, achieving a
high efficiency electron-hole transfer in the PV material 654
and corresponding generation of DC current. Different antenna
geometries may be designed with peak resonances to match
specialized multi-band gapped engineered PV materials. By
combining the efficiency, bandwidth, and omni-directional
field-of-view of the antenna element 652 with exotic energy
capturing materials, it is possible to reduce the amount and
cost of PV material 654 required. This enables an economical
manufacturing of high power density PV devices.
[0083] The embodiments described with respect to FIGS. 12 and
13 effectively concentrate infrared and visible energy onto
photovoltaic materials to greatly improve operational
efficiency, durability, and cost effectiveness of solar
generated electricity. The use of micro-antennas and
nano-antennas make it possible to use sub-wavelength sized PV
materials such as bandgap-engineering superlattice materials.
[0084] Referring now to FIG. 14, a schematic of an energy
conversion system 700 is shown in accordance with yet another
embodiment of the present invention. The energy conversion
system 700 includes a plurality of antenna elements 702
disposed in cavities 704 formed in a substrate 706. Capacitors
708 may also be disposed in the cavities 704 between the
antenna elements 702 and the ground plane 710 to function as
energy transfer elements. For example, a dielectric material
712 may be disposed on top of the antenna elements 702 to
electrically insulate them from other components. The
sidewalls of the cavities 704 may be lined with, for example,
carbon nanotubes 714. Carbon nanostructures have excellent
nanoporosity geometries which, it is believed, will enable
high efficiency dielectric and energy storage properties. A
dielectric material 716 may be disposed in the remaining
portion of the cavity 704 to complete the capacitor structure.
The capacitors 708 may be coupled to a common power bus 718.
[0085] Embodiments of the present invention, such as have been
described above, may include apparatuses or devices that are
amenable to installation and use in a variety of locations and
conjunction with a variety of applications. For example, since
the apparatuses may be formed using flexible substrates, they
may be integrated into structures or devices having complex
and contoured surfaces. Such apparatuses may be integrated
into, for example, clothing, backpacks, automobiles (or other
transportation apparatuses), consumer electronics, and a
variety of other types of devices and structures.
[0086] Although the present invention has been described with
reference to particular embodiments, the present invention is
not limited to these described embodiments. Rather, the
present invention is limited only by the appended claims,
which include within their scope all equivalent devices or
methods that operate according to the principles of the
present invention as described.