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.