rexresearch.com
Frank CHESTER
Chestahedron
Chestahedron : a new form, discovered in
2000; a seven-sided polyhedron with surfaces of equal area,
with potential applications and implications in many areas.
[ Related : Amplituhedron ... Gomboc ]
[ Click to Enlarge ]
https://www.youtube.com/watch?v=V7hOjLYz7g4
Frank Chester - Sacred Geometry &
Chestahedron
https://www.youtube.com/watch?v=70eDBh3zuYo
Frank Chester Explains the Transformative
Power of the Chestahedron & Sacred Geometry @EOSWorldExpo
https://www.youtube.com/watch?v=dQMpEAsNHmY
Frank Chester - The Chestahedron - The
Wonder of Seven
https://b-ok.cc/book/3582757/f001f2
A New Sacred Geometry: The Art and Science
of Frank Chester
by Seth Thomas Miller
This book is a visually compelling journey through the unique
geometric discoveries of Frank Chester, a contemporary sacred
geometer, artist, and sculptor. This art-style book with highly
polished design elements leads the reader from discovery to
discovery, complemented by original text from the author, a PhD
who has studied Frank's work from its inception, when it was just
seven sticks in a ball of mud on the banks of the American
River... From the back cover: The ancient tradition of Sacred
Geometry is still alive and well in the person of Frank Chester.
He has discovered a new geometric form that unites the five
Platonic solids and provides some startling indications about the
form and function of the human heart. This new form, called the
Chestahedron, was discovered in 2000, and is a seven-sided
polyhedron with surfaces of equal area. Frank has been exploring
the form and its significance for over a decade. His work has
potential implications across a number of areas, from physiology
to architecture, sculpture, geology, and beyond. Inspired by the
work of Rudolf Steiner, Frank sees a deep connection between form
and spirit. This book gives a brief, highly visual overview of
some of Frank's discoveries, and presents a compelling series of
indications for future research.
US8814419B1
Chesta vortex organizer
[ PDF ]
Abstract
Blade systems mix fluids and/or air to create and organize unique
vortexes. The vortexes periodically implode to provide superior
mixing. The blade structures may comprise four fold lines upon a
circular planar surface. The planar surface may be prepared by
removal of just one small portion of material, the removed portion
spanning approximately one radian of the perimeter.
BRIEF SUMMARY OF THE INVENTION
[0003] The present invention overcomes shortfalls in the related
art by presenting an unobvious and unique combination and
configuration of mixing blade geometry resulting in superior fluid
dynamics. Disclosed embodiments of the invention include efficient
patterns placed upon flat sheets of material whereby little
material is wasted and few folds are made in the construction of
mixing blades. In one embodiment, three symmetrical blades are
attached together to form a mixing blade system. The disclosed
geometry allows for secure attachment of mixing blades by joining
select surfaces of identical angles and surface areas that also
form surfaces useful for mixing, vortex organization and vortex
implosions.
[0004] In one embodiment, three of the disclosed blades are
identical and are attached in an equilateral triangle formation at
an approximate angle of 26 degrees from a vertical reference
center line projection. A disclosed blade efficiently comprises
four fold lines upon a circular planar surface and the removal is
just one a small portion of material, the removed portion spanning
approximately one radian of the perimeter.
[0005] These and other objects and advantages will be made
apparent when considering the following detailed specification
when taken in conjunction with the drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
[0006] FIG. 1 is a perspective view of a disclosed embodiment
[0007] FIG. 2 is a perspective view of a disclosed embodiment
[0008] FIG. 3 is a top view of a disclosed embodiment
[0009] FIG. 4 is an elevation view of a disclosed embodiment
[0010] FIG. 5 is a rotated view of FIG. 4
[0011] FIG. 6 is a plan view of geometry of a disclosed blade
[0012] FIG. 7 is a plan view featuring a disclosed connection flap
and removed section
[0013] FIG. 8 is a plan view of disclosed geometry of blade
attachment
[0014] FIG. 9 is perspective view of geometry disclosing blade
face orientations
[0015] FIG. 10 is a detailed plan view of a disclosed blade
[0016] FIG. 11 is a perspective view blade orientations referenced
with a center system line
[0017] FIG. 12 is a perspective view of blade orientations
[0018] FIG. 13 is a sectional view of disclosed blade orientations
[0019] FIG. 14 is a simplified presentation of the projection
lines, flap sections and geometry of a disclosed blade
[0020] FIG. 15 is a plan view of a detailed disclosure of
projection lines, flap sections and geometry of a disclosed blade
[0021] FIG. 16 is a simplified presentation of a disclosed mixing
disk or mixing blade
[0022] FIG. 17 is a plan view disclosing line names, arc names and
point names of a disclosed blade
[0023] FIG. 18 is a plan view of a disclosed blade with depictions
of various fold angles and other components
REFERENCE NUMERALS AND LETTERS IN THE DRAWINGS
100 is a mixing blade
in general
110 is a main flat base
section
115 is an outer flap
section
120 is a middle flap
section
125 is an inner flap
section
130 connection flap
300 is a mixing shaft,
connected to three connected mixing blades
301 center system line,
may be aligned with a mixing shaft
400 a mixing system
500 a first fold line
501 a second fold line
503 a third fold line
510 a base circle
520 portion of base
circle sometime removed
525 a first linear
boundary of the removed base circle portion 520
530 a second linear
boundary of the removed base circle portion 520
A′ is A prime and is a
bottom center point within the base circle
A is opposite of A′ and
is on the top of the base circle
B is a point to the
left of A′ and point B is adjacent to arc 1
C is a point between
points B and A, point C is the only point not found upon the
perimeter of the base circle
D is a point found to
the right of A′, the perimeter of the base circle between points
A′ and D define arc 2
arc 1 is found between
points A′ and B
arc 2 is found between
points A′ and D
arc 3 is found between
points D and A
line A′-B is sometimes
a fold line that is bent 12 degrees backwards
line A′-C is sometimes
a fold line that is bent 42 degrees forward
line A′-D is sometimes
a fold line that is bent 50 degrees forward
CL means center line
base circle means a
circle drawn as points of reference for construction of
embodiments of the disclosed invention
DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION
[0053] The following detailed description is directed to certain
specific embodiments of the invention. However, the invention can
be embodied in a multitude of different ways as defined and
covered by the claims and their equivalents. In this description,
reference is made to the drawings wherein like parts are
designated with like numerals throughout.
[0054] Unless otherwise noted in this specification or in the
claims, all of the terms used in the specification and the claims
will have the meanings normally ascribed to these terms by workers
in the art.
[0055] Unless the context clearly requires otherwise, throughout
the description and the claims, the words “comprise,” “comprising”
and the like are to be construed in an inclusive sense as opposed
to an exclusive or exhaustive sense; that is to say, in a sense of
“including, but not limited to.” Words using the singular or
plural number also include the plural or singular number,
respectively. Additionally, the words “herein,” “above,” “below,”
and words of similar import, when used in this application, shall
refer to this application as a whole and not to any particular
portions of this application.
[0056] The above detailed description of embodiments of the
invention is not intended to be exhaustive or to limit the
invention to the precise form disclosed above. While specific
embodiments of, and examples for, the invention are described
above for illustrative purposes, various equivalent modifications
are possible within the scope of the invention, as those skilled
in the relevant art will recognize. For example, while steps are
presented in a given order, alternative embodiments may perform
routines having steps in a different order. The teachings of the
invention provided herein can be applied to other systems, not
only the systems described herein. The various embodiments
described herein can be combined to provide further embodiments.
These and other changes can be made to the invention in light of
the detailed description.
[0057] Any and all the above references and U.S. patents and
applications are incorporated herein by reference. Aspects of the
invention can be modified, if necessary, to employ the systems,
functions and concepts of the various patents and applications
described above to provide yet further embodiments of the
invention.
[0058] These and other changes can be made to the invention in
light of the above detailed description. In general, the terms
used in the following claims, should not be construed to limit the
invention to the specific embodiments disclosed in the
specification, unless the above detailed description explicitly
defines such terms.
[0059] Referring to FIG. 1, a side perspective view of a disclosed
mixer system is shown with a mixing shaft 300 superior to the
blades. The mixing shaft 300 is sometimes aligned to the center
reference point shown or axis in FIG. 9 as “A”. Referring back to
FIG. 1, a mixing blade 100 in general may be comprised of a main
flat base section 110 , an outer flap section 115 , a middle flap
section 120 , an inner flap section 125 and a connection flap 130
.
[0060] FIG. 2 depicts a disclosed system that may comprise a
plurality of blades.
[0061] FIG. 3 presents a top plan view of a three blade embodiment
with each blade attached to a shaft 300 .
[0062] FIG. 4 depicts an elevation view of a disclosed system.
FIG. 4 further depicts a blade comprising a main flat base section
110 , an outer flap section 115 , a middle flap section 120 , an
inner flap section 125 and a connection flap 130 .
[0063] FIG. 5 depicts a rotated view of FIG. 4 and depicts a back
side of an outer flap 115 and other blade components.
[0064] FIG. 6 is a plan view of a disclosed blade 100 and
discloses construction of a blade by use of various angles,
reference lines and reference points. While certain angles are
disclosed as the best mode, other angles are contemplated.
[0065] FIG. 6 discloses projection lines, angels of construction
for fold lines and angles of fold. The terms “reward” and
“forward” are not limiting, but are used in reference to one
disclosed embodiment shown in FIG. 6 wherein the view of FIG. 6
has been arbitrarily considered to be a front view with A′ on the
bottom and A on the top. Other configurations are possible and
other orientations are contemplated.
[0066] A blade center line of A′-A is shown in dashed lines and
runs along the center and vertical diameter of a base circle 510 .
A base circle 510 is sometimes used as reference points for
various components. A small portion ( 520 of FIG. 7) of the base
circle is removed to complete the blade. The remaining perimeter
sections of the base circle are sometimes called arc 1 , arc 2 and
arc 3 and are clearly shown in FIG. 17 and FIG. 18.
[0067] FIG. 7 is a plan view featuring a disclosed connection flap
130 , a removed section 520 and a first linear boundary 525 and a
second linear boundary 530 defining outer edges of a finished
blade. In the best mode known to date, the flap section is at a 54
degree angle. In general the flap section is between 45 to 65
degrees.
[0068] The view of FIG. 7 is positioned to show the relative back
side of the marked disk connection area 130 . The disk connection
area is bent so as to facilitate the positioning of blades as
contemplated in FIG. 9. The blade section formed by joining two
disk connection areas can be instrumental in creating a moving
vertex when spinning a disclosed blade system or assembly in
fluid. While the disk connection area is perfectly symmetrical
with respect to the blade centerline configuration, the assembled
disc connection area presents an asymmetrical quality that is
highly advantageous for mixing material.
[0069] FIG. 8 discloses one construction of assembling or setting
a center blade line A′-A at an angle from a vertical axis line.
While an angle of 26 degrees is shown, other angles are
contemplated. The vertical axis line shown at a right angle in
FIG. 8 is sometimes called the absolute center line. A mixing
shaft 300 may sometimes be attached in alignment with the absolute
center line. The absolute center line may also be called the axis
line. A center line is marked at Aq on top and q Axis on the
bottom. The top of the face center line is marked Aq while the
bottom of the face center line is marked A′q or A prime q.
[0070] FIG. 9 is a continuation of FIG. 8, in that FIG. 9 shows
three centerlines for attachment of three of A′-A center lines.
The displayed center line guides at a projected bottom plane take
the shape of an equilateral triangle. Points A′ will be angled
away from the absolute center line by approximately 26 degrees.
[0071] FIG. 10 is presented to more clearly reveal the disclosed
angles and geometry of a disclosed blade 100 . FIG. 10 more
clearly shows the term CL found long line A′-A. In FIG. 10 the
term CL or centerline refers to the centerline of the drawn blade.
In final assembly, only point A will be adjacent to the absolute
center line shown in FIG. 9.
[0072] FIG. 11 is a perspective view blade orientations referenced
with a center system line 301 . An absolute center line is found
at point A and travels downwardly to the center of the drawn
equilateral triangle. Three points marked A′ are shown to be at an
angle from the absolute center line. During construction, a
temporary equilateral triangle may be used to facilitate the
desired placement and retention of three blades. A construction
triangle may be placed at or near the plane of the drawn
equilateral triangle. Point A′ and edges A are aptly named, as
blade points A′ and A are correspondingly attached.
[0073] FIG. 12 is a perspective view of blade orientations. The
axis is sometimes called the absolute center line.
[0074] FIG. 13 is sectional view of disclosed blade orientations.
A face center line is shown at an angle with respect to an axis
line. The face center line could be described as an edge A-A′
dihedral angle 26 degrees center line, from axis.
[0075] FIG. 14 is a simplified version of one embodiment of a
disclosed blade. Point A is shown at the bottom of the base circle
510 and point A′ is shown on the top of the base circle. FIG. 14
depicts a first fold line 500 , a second fold line 501 and a third
fold line 502 .
[0076] FIG. 15 depicts a plan view of a disclosed blade and
presents disclosures of angles of fold lines and reference lines.
[0077] FIG. 16 presents a disk or blade embodiment with the excess
material removed just to the left of point A. The removed section
is defined by lines 525 and 530 .
[0078] FIG. 17 is a plan view of a disclosed blade. FIG. 17
depicts is a blade or disk structure with various edges and points
named in traditional methods. For example, points A′ and C define
line A′-C.
[0079] FIG. 18 is a plan view of a disclosed blade with depictions
of various fold angles and other components and discloses various
edges, points and angle of folding.
[0080] Disclosed embodiments include, but are not limited to the
following items:
[0081] Item 1. A mixing and vortex organizing system, the system
comprising:
[0000] a plurality of mixing blades wherein each mixing blade
comprises:
[0082] a planer circular surface comprising three fold lines and a
neutral center line with a first fold line bent in a forward
direction between 45 and 55 degrees from the neutral center line,
a second fold line bent in a forward direction between 35 and 45
degrees from the neutral center line and a third fold line is bent
in a backward direction 6 to 18 degrees from the position of the
second fold line, and a disk connection section defined between
first fold line and the neutral center line,
the plurality of mixing blades fastened to each other at each
respective disk connection section; and
a mixing shaft connected to the attached plurality of mixing
blades.
[0083] The system of item 1 wherein the planer circular surface
comprises a lower center reference point and the neutral center
line starts at the lower center reference point and ends at an
upper center reference point and wherein the first fold line is
between 30 and 40 degrees from the lower center reference point
and wherein the second fold line is between 15 and 25 degrees from
the lower center reference point and wherein the third fold line
is between 15 to 25 degrees from the second fold line.
[0084] The system of item 2 wherein the planer circular surface is
reduced at two edge lines, the first edge line defined at an angle
of between 100 to 110 degrees from the upper center reference
point to the second fold line and the second edge line is defined
at an angle of between 90 to 100 degrees from the third fold line.
[0085] The system of item 3 wherein the connection section is at
an angle between 50 to 60 degrees.
[0086] The system of item 4 wherein the plurality of mixing blades
are each angled between 16 and 26 degrees from a central center
line located equidistant from the mixing blades.
US9278744B1
ChetProp air or water propeller and spinner with front and
back leg assemblies attached to spinner
[ PDF ]
Abstract
An air or watercraft propeller comprises a plurality of blade
systems wherein each blade system is composed of a front leg
attached to a back blade. The front legs pull air or water towards
spinner while the back legs use vertical suction to draw air or
water towards the spinner to complement the air or water flow
created by the front legs. The back legs are angularly attached to
the spinner at approximately 60 degrees rotated from the spinner
center line. The back legs are also tilted to an angle of
approximately 60 degrees from the surface of the spinner. The
front legs are attached to the back legs at an angle of
approximately 60 degrees. The propeller system presents several
equilateral triangles to maximize propulsion efficiency. The front
legs are rigidly attached to the spinner while the back legs may
be adjusted for pitch.
USD681502S
Thirteen-sided polyhedron form
[ PDF ]
[0001] FIG. 1 is a top view of a thirteen-sided polyhedron form
showing my new design;
[0002] FIG. 2 is a bottom view thereof;
[0003] FIG. 3 is a first side view thereof;
[0004] FIG. 4 is a second side view thereof;
[0005] FIG. 5 is a third side view thereof;
[0006] FIG. 6 is a top front perspective view thereof; and,
[0007] FIG. 7 is a top plan view of the thirteen-sided polyhedron
form in a unfolded out position.