Wind power electrical generator system

A wind power electrical generator system having improved efficiency including a wind mill which activates an air compressor to generate a supply of pressurized air. An air motor activated by the supply of pressurized air drives a generator to produce electrical power. A waste air recovery mechanism, activated by the waste air from the air motor produces rotary energy assisting the wind mill in activating the air compressor.

BACKGROUND OF THE INVENTION 
1. Field of the Invention 
The invention relates to wind power electrical generator systems and in 
particular to a wind power electrical generator system in which the wind 
power is first converted to a pressurized source of air which is 
susbsequently converted to electrical power by an air motor connected to 
an electrical generator. 
2. Prior Art 
Wind power electrical generator systems in which the wind energy is 
converted to electrical energy through an intermediate storage step are 
known in the art. In particular, Harsen in U.S. Pat. No. 3,806,733, 
discloses a wind driven electrical energy conversion apparatus in which 
the wind energy is converted to a pressurized air supply which is 
susbsequently converted to rotary power by inflating air cells carried by 
an endless belt immersed in a tank filled with a fluid. The rotary output 
of the endless belt is connected to an electrical generator which produces 
the desired electrical power. Mead et al in U.S. Pat. No. 4,229,661, 
discloses a power plant for a camping trailer in which the wind energy is 
first converted to a pressurized air supply which is subsequently 
converted to a rotary output by an air driven turbine. The rotary output 
of the turbine is connected to a generator which produces the desired 
electrical power. 
These systems are inefficient and do not utilize the total energy of the 
pressurized air supply. Disclosed herein is a wind powered electrical 
generator system in which the energy wasted in the conversion of the 
pressurized air supply to electrical power is partially recovered. 
SUMMARY OF THE INVENTION 
The wind power electrical generator includes a wind mill rotatably mounted 
on the top of a tower, an air compressor connected to the rotary output of 
the wind mill, an accumulator storing the pressurized air output of the 
air compressor to generate a supply of pressurized air, a first air motor 
receiving pressurized air from the accumulator to generate a rotary 
output, an electrical generator driven by the rotary output of the first 
air motor for generating the desired electrical power, and a waste air 
recovery mechanism having a second air motor driven by the exhaust air of 
the first air motor producing a rotary output supplementing the wind 
energy driving the air compressor. 
The primary advantage of the disclosed wind power electrial generator 
system is that it makes more efficient use of the energy of the 
pressurized air supply. Another advantage of the disclosed wind power 
electrical generator system is that the pressurized air supply may be used 
to power air driven tools. Still another advantage of the disclosed wind 
power electrical generator is that solar energy may be used to supplement 
the supply of pressurized air during periods when wind energy is incapable 
of sustaining the operation of the system. 
These and other advantages of the disclosed wind power electrical generator 
system will become apparent from a reading of the detailed description of 
the invention in connection with the accompanying figures.

DESCRIPTION OF THE PREFERRED EMBODIMENT 
Referring to FIG. 1 there is shown the physical structure of the disclosed 
wind power electrical generator 10. The wind power electrical generator 
system includes an upper assembly 12 rotatably attached to the top of a 
support tower 14. The support tower 14 is rigidly mounted on a concrete 
base 16 buried in the ground. 
The upper assembly 12 includes a wind mill assembly 18 mounted to one end 
of a shaft 20. The wind mill assembly 18 includes a plurality of 
propellers 22 connected to a hub assembly 24. The shaft 20 passes through 
a waste air recovery mechanism 26 which also serves to support the shaft 
20 and the wind mill assembly 18 for rotation from a base plate 30. The 
opposite end of the shaft 20 is connected to an air compressor 28 also 
mounted on the base plate 30. The base plate 30 is rotatably attached to a 
circular plate 32 rigidly supported at the top of the tower 14. 
A vertical vane 36 is fixedly attached to the base plate 30 by means of a 
pair of support struts 38. The vertical vane 36 keeps the base plate 30 
and the wind mill assembly 18 pointed into the wind. 
An air line 42 interconnects an output port of the air compressor 28 with 
an input port to an accumulator 44 through a check valve 46. An output air 
line 48 interconnects an output port of the accumulator 44 with an input 
to a flow rate regulator 50. An air line 52 interconnects the regulated 
output of the flow rate regulator 50 with an input to a first air motor 54 
through a check valve 56. The first air motor 54 has a rotary output shaft 
58 which drives an electrical generator 60. The electrical generator 60 
generates electrical power on a pair of output leads 62 in response to the 
rotation of the shaft 58 by the first air motor 54. 
An air line 64 interconnects an exhaust port of the first air motor 54 to 
an input port of the waste air recovery mechanism 26 through a pressure 
relief valve 65. The waste air recovery mechanism 26 has an exhaust port, 
not illustrated, exhausting the expended air to the atmosphere. The waste 
air recovery mechanism 26 includes a second air motor as shall be 
explained hereinafter with reference to FIGS. 5 and 6 which assists the 
wind mill assembly 18 in rotating the shaft 20 to drive the air compressor 
28. Air lines 42 and 64 are pictorially illustrated external to the tower 
14 to simplify the drawing. The air lines 42 and 64, respectively, are 
connected to the air compressor 28 and waste air recovery mechanism 26 
respectively, through a rotary interconnect (not shown) attached to the 
base plate 30 and concentric with its axis of rotation about the circular 
plate 32 to accommodate rotation of the wind mill assembly 18 with respect 
to the tower 14. 
The operation of the wind power generator is as follows: Wind energy 
rotates the wind mill 18 actuating the air compressor 28 to generate a 
supply of pressurized air stored in the accumulator 44. The check valve 46 
prevents the pressurized air from back flowing through the air compressor 
during periods of light or low wind. A pressurized air flow from the 
accumulator 44 to the air motor 54 is regulated to a predetermined flow 
rate by the flow rate regulator 50. The regulated air flow activates the 
air motor 54 to drive the electrical generator 60 at a predetermined speed 
to produce an alternating current at its output having the desired 
frequency. For common household use this frequency would be 60 Hertz. but 
may be any other desired frequency. 
Only part of the energy of the air flow is expended in the air motor 54 to 
drive the electrical generator. The unused portion of this energy is 
exhausted from the air motor in the form of an air flow at a reduced 
pressure. The air flow exhausted from the air motor 54 is applied to the 
waste air recovery mechanism 26 which embodies a second air motor 
converting the unused energy into rotational energy of the shaft 20 
supplementing the wind mill assembly 18 in driving the air compressor 28 
thereby increasing the efficiency of the system. The pressure relief valve 
65 prohibits an excessive back pressure from being built up at the exhaust 
port of the air motor 54 when the wind power is not sufficient for the 
wind mill assembly 18 to activate the air compressor 28. 
As would be obvious to those skilled in the art, the pressurized air stored 
in the accumulator may also be used to power other devices such as an air 
wrench, a pneumatic jack, or similar mechanism. 
The details of the propeller's hub assembly 24 are shown in FIGS. 2, 3 and 
4. Referring first to FIG. 2 there is shown a plan view of the hub 
assembly 24 with the cover plate (not shown) removed. The hub assembly 24 
includes a cup shaped support member 66 having a hub 68 concentrically 
mounted thereto by means of fasteners, such as screws 70. The shaft 20 is 
secured to the hub 68 by means of a set screw 71 as shown in FIG. 3. 
Each shaft 72 of the three propellers 22 are radially supported to rotate 
with respect to the support member 66 by means of a pair of spatially 
separated bushing blocks 74. Each bushing block 74 is attached to the 
support member 66 by a pair of screws, such as screws 76. Radial 
displacement of the propellers 22 is inhibited by a pair of "C" shaped 
retainer rings 78 disposed in peripheral grooves formed in each propeller 
shaft 72 either side of the inner most bushing block 74. 
A collar 80, attached to each propeller shaft 72 intermediate the bushing 
blocks 74, supports a ball headed standard 83 which is mechanically linked 
by a link member 96 to a flyweight governors 84 and 86. The flyweight 
governor 84 includes a straight arm 82 and an angled arm 88 mounted for 
rotation about a pivot 90 attached to a mounting tab 92 extending radially 
from support member 66. A weight 94 is attached to the end of the angled 
arm 88 external to the support member 66 while the straight arm 82 
rotatably connects the internal end of the angled arm 88 with the link 
member 96 attached to one of the propeller shafts 72. The external end of 
angled arm 88 is radially biased towards the shaft 20 by a spring assembly 
98 including a spring shaft 100 having one end connected to the external 
end of the angled arm 88 and the other end passing through an aperture in 
an "L" shaped mounting bracket 102 and, through a resilient member such as 
a spring 104. A spring retainer 106 is mounted on the other end of the 
spring shaft 100 and captivates the spring 104 between itself and the "L" 
shaped mounting bracket 102. A nut 108 is threadably received at the other 
end of the spring shaft 100 and provides for the adjustment of the 
position of the spring retainer 106 and the force biasing the external 
portion of the angled arm 88 radially towards the center of the hub 
assembly 24. 
The flyweight governor 86 includes a second angled arm 110 mounted for 
rotation about a pivot 112 attached to a mounting tab 114 extending 
radially from the support member 66. A weight 116 is attached to the end 
of the angled arm 110 external to the support member 66 while a connecting 
arm 120 is pivotally connected at the other end. One end of the connecting 
arm 120 is connected to the ball headed standard 83 associated with one of 
the other two propeller shafts 72 while the other end of the connecting 
arm 120 is pivotally connected to one arm of a "V" lever 122. The "V" 
lever is rotatably supported from said support member 66 by means of a 
pivot member such as hex headed bolt 124. A connecting arm 126 pivotally 
interconnects the other arm of "V" lever 122 and the ball headed standard 
83 associated with the third propeller shaft 72. A second spring assembly 
128 similar to the spring assembly 98 resiliently biases the end of the 
angled arm 110 external to the support member 66 towards the center of the 
hub assembly 24. 
The operation of the hub assembly 24 is as follows: Under light wind 
conditions, the spring assemblies 98 and 128 bias the external end angled 
arms 88 and 110 towards the center of the hub assembly to the retracted 
positions shown in FIG. 2. In this position, the mechanical linkages 
connected between the internal ends of the angled arms 98 and 110 and the 
ball headed standards 83 associated with each propeller shaft 72, hold the 
propellers 22 at an angle predetermined to produce maximum efficiency of 
the wind mill assembly 18. When the rotational velocity of the wind mill 
assembly 18 exceeds a predetermined speed, the centrifugal force acting on 
the weights 94 and 116 produces a force on the external ends of the angled 
arms 88 and 110 exceeding the biasing forces of the spring assemblies 98 
and 128, respectively. This causes the angled 88 and 110 to rotate about 
the respective pivots to an extended position. This rotation produces a 
corresponding mechanical displacement of the external ends of the angled 
arms 88 and 110 which is transferred to the ball headed standards 83 
associated with each of the propeller shafts 72 by the mechanically 
linkages discussed above. The mechanical translation of the ball headed 
standards 82 normal to the axis of propeller shafts 72 causes them to 
rotate about their axis in the bushing blocks 74 in a direction tending to 
the "feather" the propellers 22 to a less efficient angle with respect to 
the wind. The weights 94 and 116, respectively, and the biasing forces of 
the spring assemblies 98 and 128 are selected so that the propeller blades 
22 will be feathered in unison and their rotational velocity will not 
exceed a predetermined speed under high wind conditions. 
The details of the waste air recovery mechanism 26 are shown on FIGS. 5 and 
6. The waste air recovery mechanism 26 includes an impeller housing 130 
having an internal cylindrical chamber 132 and a mounting flange 134. The 
shaft 20 passes axially through the cylindrical chamber 132 and is 
supported for rotation at the opposite ends of the cylindrical chamber 132 
by a pair of roller bearings 136 and 138. The shaft 20 has four equally 
spaced slots or grooves 140 which hold four vanes 142 radially extending 
between the shaft 20 and the internal surface of the cylindrical chamber 
132. A pair of cup shaped spacers 144 and 146 are disposed between the 
vanes 142 and the bearings 136 and 138 respectively and define a working 
chamber 148 of an air motor 150 including the shaft 20, the cylindrical 
chamber 132, and the spacers 144 and 146. Shaft seals 151 and 152, 
disposed inside the cup shaped spacers 144 and 146, respectively form an 
air tight seal about the shaft 20 at either end of the air motor's working 
chamber 148. The impeller housing 130 has a threaded air inlet port 153 
for threadably receiving a hose fitting 154 or similar threaded 
connection, and an exhaust port 156. The flange 134 has four bolt mounting 
holes, such as holes 157 for bolts securing the waste air recovery 
mechanism 26 to the base plate 30. 
As previously stated, the waste air recovery mechanism 26 includes an air 
motor 150 and supports the shaft 20 and wind mill assembly 18 for 
rotation. Waste air from the air motor 54 driving the electrical generator 
60 is received at the air inlet port 153. The waste air received at inlet 
port 153 generates a pressure differential across the vane 142 between the 
inlet port 153 and the exhaust port 156 which produces a rotational force 
on the shaft 20 assisting the wind mill assembly 18 in actuating the 
compressor 28. 
The details of the propellers 22 are shown on FIGS. 7 through 10. Referring 
to FIGS. 7 and 8 each propeller comprises a propeller shaft 72, a series 
of ribs 158 though 166 fixedly attached to the propeller shaft 72, and a 
tip section 168. The spaces between the ribs 158 through the tip section 
168 are filled with an expanded material 170 such as styrofoam or aluminum 
honeycomb for structural support and is covered with a thin layer of 
aluminum 172. Referring now to FIG. 8, the propeller shaft 72 has a 
circular section 174 at one end and a tapered blade section 176 for the 
remainder of its length. The end of the circular section 174 of the 
propeller shaft has a pair of circumferential grooves 178 and 180 for 
receiving the "C" shaped retaining rings 78 as described with reference to 
FIG. 2. 
The details of the ribs 158 through 166 are shown on FIGS. 9 and 10. The 
first rib 158 shown in FIG. 9 is in the form of an air foil having a 
circular aperture 182 adapted to be received over the circular section 174 
of the propeller shaft 72. A threaded aperture 184 receives a set screw 
(not shown) for fixedly attaching the rib 158 to the shaft 72. 
The rib 160, shown on FIG. 10, is in the form of a corresponding air foil 
and has an oblong aperture 186 adapted to be received over the tapered 
blade section 176 of the propeller shaft 72. Apertures 188 and 190 may be 
added to reduce the weight of the rib. A threaded aperture 192 is provided 
to receive a set screw (not shown) for attaching the rib 160 to the 
propeller shaft 72. The remaining ribs 162 through 166 are basically the 
same as the rib 160 but are progressively smaller as they approach 
lightweight tip of the propeller shaft 72. The oblong apertures 186 may be 
disposed at different angles with respect to the air foil to provide a 
twist to the propeller blade as is known in the art. The air foil 
configuration of the ribs 158 through 166 may be of any conventional shape 
and not limited to the air foil configuration shown. 
The tip section 168, shown in FIG. 11, has the same basic air foil 
configuration with an oblong aperture 194 adapted to be received over the 
end of the tapered blade section 176 of the propeller shaft 72 and a 
threaded aperture 196 for receiving a set screw (not shown) attaching the 
tip section 168 to the propeller shaft 72. Holes 198 and 200 may be added 
to reduce the weight of the tip section 168. The tip section 168, as well 
as ribs 158 through 166, may be made from any lightweight structural 
material such as aluminum, wood or a lightweight structural plastic. 
The wind power electrical generator may be supplemented by a solar energy 
converter as illustrated on FIG. 12. As previously described, the wind 
mill assembly 18 generates a rotary motion on the shaft 20 which passes 
through the waste air recovery mechanism 26 and activates the air 
compressor 28. The compressed air generated by the air compressor 28 
passes through a check valve 46 and is stored in an accumulator 44. The 
compressed air stored in the accumulator 44 activates an air motor 54 
which produces a rotary motion turning the electrical generator 60. The 
waste air from air motor 54 passes through a selector valve 212 back to 
the waste air recovery mechanism 26 where it assists the wind mill 
assembly 18 in activating the air compressor 28. The operation and 
function of the selector valve 212 shall be explained hereinafter. 
Additionally the system includes a solar energy to steam conversion 
apparatus such as a parabolic mirror 200 which collects solar energy which 
is transmitted to a boiler 202 which produces steam in response to the 
collected solar energy. The steam from the boiler 202 activates a vane 
motor 204 to produce a rotary motion on a shaft 205 which activates an air 
compressor 208 through a waste air recovery mechanism 206. The waste air 
recovery mechanism 206 and the air compressor 208 are functionally the 
same as waste air recovery mechanism 26 and the air compressor 28 
discussed with reference to FIG. 1 and structurally may include identical 
elements. The compressed air from the air compressor 208 passes through a 
check valve 210 to the accumulator 44 where it is stored. 
The check valves 46 and 210 isolate their respective air compressors from 
the pressure in the accumulator 44 and only permit an air flow to the 
accumulator 44 when their associated air pump is providing air at a 
pressure greater then the pressure in the accumulator 44. 
The selector valve 212 is controlled by the output pressure being generated 
by both the air compressors 28 and 208 and transmits the waste air from 
the air motor 54 back to the waste air recovery mechanism whose air 
compressor is generating air at the highest pressure thereby assisting the 
air pump which is supplying air to the accumulator 44. Thus it is seen 
that the accumulator 44 is capable of being supplied with pressurized air 
from either wind or solar energy. 
One skilled in the art will recognize that other solar to rotary energy 
converters may be substituted for the parabolic mirror 200, boiler 202, 
and vane motor 204 without departing from the spirit of the present 
invention.