This application relates to conversion of energy of a mechanical motion into electrical energy.
Energy is a valuable resource. A variety of techniques have been and are being developed to generate energy from various sources, such as the coal, oil, natural gas, hydrogen, sunlight, wind, and ocean waves. Certain energy resources are limited on earth and are not renewable. Examples of such energy sources include the fossil fuels like coal, oil, and natural gas, and nuclear fuels such as uranium. The fossil fuels, uranium and other non-renewable energy sources will eventually be depleted on earth by continuous exploration and use. The consumption and use of many non-renewable energy sources such as fossil fuels and nuclear fuels are also known for causing pollutions to the environments.
In contrast, certain other energy resources, such as the sunlight, wind, and ocean waves, are practically unlimited in their supply and may be utilized in ways that can significantly reduce or minimize adverse impacts to the environments and the earth's ecological systems. Therefore, techniques, devices and systems for obtaining energy from various sources other than fossil fuels and nuclear fuels are desirable to preserve earth's natural resources, to reduce pollution to the environments, and to expand energy supply sources in order to provide sustainable energy supply to humans.
For example, the motion of water waves in a large body of water, e.g., lakes, rivers, and oceans, may be used to generate electricity. Oceans, in particular, have an enormous potential as a source of energy in part because oceans cover over 70% of the earth's surface and are estimated to have an annual capacity of about 2000 tera watt-hour in the surface wave energy alone.
This application describes implementations of techniques and devices that use a spinning gyroscope to convert an oscillating torque caused by an oscillating motion into a continuous torque acting on an electromagnetic motor generator and thus cases a continuous rotation of the electromagnetic motor generator which generates electricity. In one implementation, for example, a method is described to use a spinning gyroscope to convert an oscillating motion into a continuous rotation motion and to cause the continuous rotation motion to activate an electromagnetic motor-generator to generate electricity.
In another implementation, an exemplary device is described to include a base reactive to an oscillating motion acting on the base; a gyroscope engaged to the base and operable to precess in response to the oscillating motion of the base when the gyroscope is spinning; an electromagnetic motor-generator to rotate and to generate electricity; and a coupling unit coupled between the gyroscope and the electromagnetic motor-generator to transfer the precession of the gyroscope to continuous rotation of the electromagnetic motor-generator, thus converting energy of the oscillating motion into electricity.
In yet another implementation, a device is described to include a floating device to float in water and a base engaged to the floating device to be substantially parallel to a water surface at a location where the base is located. This device includes a gyroscope engaged to the base and operable to precess, when the gyroscope is spinning, in response to an oscillating motion of the base when floating on the water. An electromagnetic motor-generator is engaged to the base and to rotate around a motor rotation axis that is perpendicular to the base. This device includes crank arm engaged to the electromagnetic motor-generator and operable to rotate the electromagnetic motor-generator and engaged to the gyroscope so that an axis of the spinning of the gyroscope is parallel to the crank arm. The crank arm is operable to transfer the precession of the gyroscope into continuous rotation of the electromagnetic motor-generator, thus converting energy of the oscillating motion into electricity. A control module is coupled to control spinning of the gyroscope according to a frequency of the oscillating motion.
These and other implementations are described in greater detail in the attached drawings, the detailed description and the claims.
The techniques and devices described in this application use a spinning gyroscope to convert an oscillating torque caused by an oscillating motion into a continuous torque acting on an electromagnetic motor generator and thus cases a continuous rotation of the electromagnetic motor generator. The electromagnetic motor generator generates electricity from the continuous rotation. A coupling mechanism is provided to transfer or transform the precession motion of the spinning gyroscope under the oscillating torque into the continuous rotation of the motor generator. As described in detail below, the use of the spinning gyroscope and the coupling mechanism can be implemented in simple and efficient configurations that convert the energy of an oscillating motion into electricity for a variety of applications.
The implementation of the combination of the spinning gyroscope and the coupling mechanism may be adapted different to efficiently interact with different forms of oscillating motions. For example, the oscillating motion may be caused by a natural phenomenon such as water waves in, e.g., oceans and winds. Specific examples are described here for designs that directly convert the periodic torque of oscillating surface waves in a body of water such as ocean waves into the continuous torque acting on a rotary electric generator which in turn generates electricity. The spinning gyroscope, which sometimes may be used as an inertial frame of reference such as a horizontal spinning top, is configured to continuously precess harmonically to the oscillating motion of the ocean waves, usually with varying amplitudes and periods. This precession of the spinning gyroscope is then used to drive the rotary motor generator to continuously rotate and thus generate electricity. The entirety or a portion of the generated electricity may be directly used to power an electric load or device. The entirety or a portion of the generated electricity may also be used to charge up a rechargeable battery to store the generated energy or be stored in other energy storage device. In some applications, the generated electricity may be partially used to drive an electric load or device while the remainder of the generated electricity is being stored.
In certain implementations, the spinning motion of the gyroscope may be initiated or initially powered by a power supply such as a battery. After the initial spinning of the gyroscope, the combined operation of the spinning gyroscope and the coupling mechanism generate electricity from a specific oscillating motion with which the system is designed to interact. While a portion of or the most of the generated electricity may be sent to the storage device or may be used to drive the electric load, a portion of the generated electricity from the rotary electric generator is partitioned out of the generated electricity and is used to power the spinning motion of the gyroscope. Therefore, after the initial powering by the power supply, the gyroscope may be controlled to cease receiving energy from the power supply after the partitioned portion of the electricity generated by the motor is sufficient to maintain spinning of the gyroscope. The power supply for the initial spinning of the gyroscope may be a rechargeable battery that can be recharged by the generated electricity. Therefore, under this particular design, a gyroscope-based generator may be a self-powered, autonomous system when the spinning gyroscope, the precession of the gyroscope and the oscillating motion are in phase and in resonance with one another.
In other implementations, gyroscope-based generators based on the present combined operation of the spinning gyroscope and the coupling mechanism may be configured to initiate the spinning of the gyroscope without using energy from a power supply. The oscillating motion caused by a suitable source such as the ocean waves or winds can be used to cause the coupling mechanism to rotate the rotary electromagnetic motor generator to generate the electricity. This electricity is then used to spin up the gyroscope until the spinning gyroscope, the precession of the gyroscope and the oscillating motion are in phase and in resonance with one another. After this initial spin-up of the gyroscope, a part of the generated electricity is used to sustain the spinning of the gyroscope while the remaining part of the generated electricity is used to drive an electric load or to be stored in a storage device.
The change in the component of N, (Np), oriented along the axis of precession, which is the crank arm axis in an example described below, is ∥Np∥=L sin(θ) for one quarter of a full cycle. Because Np is the change in Li that contributes to the torque turning the crank arm of the device 100, and the average torque
can be expressed as follows:
τ=4Lf sin(θ),
where f is the frequency of the oscillating object or force such as ocean waves. Thus the theoretical input power from the torque caused by the oscillating object or force is:
Pin=8πf2L sin θ.
As an example, consider an implementation of the design in
The gyro wheel 412 of the gyroscope 410 is mounted to spin around a gyro axle 414 that is substantially parallel to the crank arm 430 and to the base 480. The gyro axle 414 is engaged to and is rotated by the gyro motor 418 to cause the gyro wheel 412 to spin. A gyroscope power supply, such as a battery, may be used to supply the electrical power to the gyro motor 418 for, at the minimum, initiating the spin of the gyro wheel 412 so that the oscillating motion of the base 408 can cause the gyroscope 410 to precess. A gyro bracket 416 is structured to hold the gyro wheel 412, the gyro axle 414, and the gyro motor 418 together as the assembled gyroscope 410. A mechanical coupler or coupling element 420 may be used to engage the gyro bracket 416 to the crank arm 430. In this configuration, as the gyroscope 410 precesses in response to the external oscillating motion exerted on the generator 400, the precession motion of the gyroscope 410 causes the crank arm 430 to rotate via the coupling element 420.
The crank arm 430 in the illustrated example is engaged to a first rotational axel 440 that is substantially perpendicular to the crank arm 430 and the gyro axel 414. When the gyroscope 410 precesses, the crank arm 430 rotates around the axel 440 along with the precession of the gyroscope 410. The crank arm 430 may be configured in various geometries. For example, the crank arm 430 may be a circular plate with its center engaged to the axel 440 so that the plate spins or rotates around the axel 440. The crank arm 439 includes a crank hub 432 that is engaged to the axel 440. The gyroscope 410 may be positioned on the crank arm 430 off the first axel 440, or alternatively, near or at the axel 440. The axel 440 may be the rotary axel of the rotary motor generator 460. In the illustrated example, a pair of reduction gears 442 and 444 are used to transfer the rotation of the axel 440 to the rotation of a second, substantially parallel axel 450 which is the rotary axel of the motor generator 460. The gear 442 is engaged to rotate with the axel 440 and the gear 444 is engaged to rotate with the axel 450. The gears 442 and 444 are engaged to each other so their rotary motions are synchronized and may be sized with different diameters, e.g., the diameter of the gear 442 is greater than that of the gear 444, to rotate the motor 460 at a higher angular velocity than the axel 440. Therefore, in the illustrated example, the combination of the crank arm 430, the axel 440, the pair of reduction gears 442 and 444 forms the coupling mechanism 120 in
The gyroscope generator 400 is further shown to use a generator frame 490 on a bottom plate 482 to hold the motor 460, the reduction gears 442 and 444, and the first axel 440. Electrical connectors and circuits (e.g., rectifiers) 470 for the rotary motor generator 460 may also be placed in the generator frame 470. The bottom plate 482 may be directly engaged to the base 480.
The gyroscope generator 400 may be adapted to interact with various oscillating motions to generate electricity. For example, the base 480 or an extension connected to the base 480 may be used to interact with wind to cause the base 480 to oscillate with the wind and to generate electricity. As another example, a floating device or a buoy may be engaged to the base 408 and the entire system can float on the ocean to generate electricity from the oscillating motion of the ocean waves.
The housing 510 may be engaged to a set of elongated plates or blades, which extend vertically into the water, to provide lateral stability of the housing 510 and to ensure that the bottom 518 of the housing 510 faces downward. As illustrated in
In the designs shown in
where M1 is the projected mass of a disk with the outer radius of the ring, and M2 is the projected mass of a disk with the inner radius of the ring, and r1 and r2 are the outer and inner radii, respectively.
Consider a specific configuration for the above example as follows:
M=0.47 [kg],
r1=0.046 [m],
r2=0.03 [m],
M/m2=123.031 [kg/m2],
M1=0.817862 [kg] and
M2=0.347862 [kg],
The moment is I=0.000709 [kg·m2], the angular momentum is L=Iω=0.400794 [kg·m2ω] and the input power for spinning the gyroscope is Pin=8πf2 L sin(θ)=5.383 [W]. The gyroscope 410 in the designs shown in
The designs in
τ/L=4f sin(θ).
As long as this ratio is maintained during operation, the device can resonate at any given wave frequency and angle.
A simple prototype, Gyro-Gen, based on the designs in
In testing the prototype Gyro-Gen, a motion controlled test frame was built as a wave simulator to simulate the rocking motion of the device when floated on the ocean. The test frame includes a brushless torque motor and programmed to simulate ⅔ to 4-second period ocean waves. An 8-channel data recorder (Persistor, Inc. CF2) was mounted on the test frame to record 20 samples per second electrical output power and output of a 3-axis accelerometer (Crossbow CXL04LP3) mounted below the crank arm shaft. Data analysis software was written using Matlab.
The Gyro-Gen was tested with varying wave periods, fixing tilt, electrical load, gyro rate, and crank arm offset to obtain measures of the output power as a function of the angular velocity. The gyro spinning rate was varied by 20 r.p.s. between successive runs. Before each run, the gyro was spun up by applying a constant voltage to the gyro motor from a lab power supply (Tektronix PS280). The gyro spinning rate was determined using the back e.m.f. frequency of the gyro motor recorded with a Tektronix THS 730A digital storage oscilloscope. The load impedance was measured with the Fluke 87 DMM. The electrical generator's load impedance was set to 100 ohms. During the run wave frequencies were held constant for 30 seconds before stepping in 0.25 Hz. increments until the maximum frequency of 1.5 Hz was reached. Then the wave frequency was stepped down in 0.25 Hz increments until the minimum of 0.25 Hz. was reached marking the end of the run. Each run was performed 3 times.
Measurements of the generated power as a function of the electrical load were also obtained by decreasing the load impedance from the initial value of 100 ohms to 50 ohms and 33 ohms and gyro angular velocities set to 65 and 90 r.p.s.
A Maximum Load Test was conducted (at the previous range of wave frequencies and gyro rates) in which the load was increased using a 100 watt Ohmite rheostat until the crank arm stopped rotating synchronously, then decreased just enough to restore synchronous rotation. Under this condition, the voltage generated and the final load impedance were recorded using an averaging D.M.M. Then the power was calculated to determine the maximum power the system could generate at a specific gyro rate and a specific wave frequency.
Another bench test, Self-Powered Gyro Test, was conducted with the Gyro-Gen operating autonomously by using the generated power to spin the gyroscope. The gyro was initially spun by the bench power supply at 80 r.p.s. The gyro motor was then switched to the electric generator, which was also loaded with 100 ohms and driven by the test frame at 1.5 Hz wave frequencies until the gyro rate was stabilized. The wave frequency was decreased to 1.25 Hz and the gyro's angular velocity was again allowed to stabilize.
The efficiency of the system can be estimated by dividing the net power (maximum power generated minus the gyro motor power) by the total power at maximum output and adding all measurable system losses. For example, at 90 r.p.s. and 1.25 Hz, the power output of gyro motor plus load was 2.98 watts. The gyro motor power was 2.16 watts, so that the net output power was 0.817 watts. Adding the total losses, the diode bridge loss was 1.13 watts and the generator's internal resistance loss was 1.042 watts. The total measured power dissipation equals 5.122 watts. This compares well with the theoretical total power input of 6.17 watts. The corresponding efficiency is 0.817 watts/5.12 watts, or 16%. Using the theoretical power input instead of the measured power output the efficiency is 13%. Noting losses in the diode bridges, the rectifiers were replaced with Schottky diodes and efficiency increased to 18.4%.
The above Gyro-Gen as mounted in a watertight (60.6 liter Rubbermaid Roughneck) utility tub to form a prototype based on the design in
Ocean testing included seven test runs shown in
The above test results demonstrate that power generation based on gyroscopic precession is a viable technology for an autonomous wave-powered generator. The prototype Gyro-Gen successfully generated sufficient power to run both the gyroscope and an auxiliary load. Hence, the gyroscope can be used to efficiently transfer power from periodic angular motion into electricity. The test results further show that the crank arm could generate little power without the gyro's precessional torque. As the angular momentum of the gyroscope increases, the amount of the potential torque to the generator and the electrical power output increase accordingly. Notably, the load can be controlled in order to achieve the maximum power output. Both experimental and theoretical results indicate that the electrical load and the angular momentum of the gyro are interrelated, i.e., if the angular momentum on the gyro is increased, it only helps to a certain point before the load must be increased. For instance, as indicated in
Sea tests of the prototype Gyro-Gen show that a rotating gyro increased the power output significantly. The buoy design in
The present gyroscope-based generator may be implemented in a large scale to increase the power output. As an example, assume a gyroscope with a moment of inertia of about 30 [kg·m2] is used. This is approximately equivalent to the moment of inertia of a 250 [kg] disk with a radius of 0.5 [m]) spinning at 200 [r.p.s]. The angular momentum of this large gyroscope is approximately 3600 [kg·m2·ω]. Thus a Gyro-Gen buoy containing a single gyroscope mechanism with the above large gyroscope can generate approximately 2340 Watts in little more than one cubic meter of space excluding the buoy hull assuming the buoy pitches at ±15 degrees on a 10 second period wave. Therefore, depending on the power requirements, gyroscope-based generators may be sized to provide sufficient power outputs for different applications.
The system controller 1130 processes the measurements from the sensors 1120 and 1140 and the load information from the power regulator 1150 and dynamically controls the angular velocity of the gyroscope 110 by producing a gyro motor velocity control signal. A gyro motor velocity control unit 1110 is provided to respond to the control signal and to control the gyro motor 418 accordingly. The gyro motor 418, in turn, drives the gyroscope 110 at a desired gyro angular velocity. Hence, this control feedback is dynamic in the sense that the gyro angular velocity is adjusted with changes in the external periodic torque and the load. The power regulator 1150 splits the power from the generator 130 into a first portion as the output for distribution, e.g., driving an electronic device or an electrical appliance, and a second portion to a storage battery 1160. The storage battery may be used as the power supply for the gyro motor 418.
In the above examples, only a single gyroscope is used in a gyroscope-based generator. In other implementations, two or more gyroscopes may be used in a generator to achieve certain operating advantages.
In summary, only a few implementations are disclosed. However, it is understood that variations and enhancements may be made.
This application claims the benefit of U.S. Provisional Application No. 60/627,349 entitled “GYROSCOPE-BASED ELECTRICITY GENERATOR” and filed Nov. 12, 2004, which is incorporated herein by reference in its entirety as part of the specification of this application.
Number | Name | Date | Kind |
---|---|---|---|
1992457 | Anderson, Jr. | Feb 1935 | A |
2410831 | Maybarduk et al. | Nov 1946 | A |
2412961 | Braddon | Dec 1946 | A |
2415429 | Kellogg et al. | Feb 1947 | A |
2427130 | Ford | Sep 1947 | A |
2501885 | Barnes et al. | Mar 1950 | A |
2592643 | Barnes | Apr 1952 | A |
2684007 | Newell | Jul 1954 | A |
2734278 | Hammond, Jr. | Feb 1956 | A |
2968956 | Agins | Jan 1961 | A |
3203644 | Kellogg, Jr. | Aug 1965 | A |
3558936 | Horan | Jan 1971 | A |
3589019 | Culver | Jun 1971 | A |
4088352 | Kling | May 1978 | A |
4161889 | Hinds | Jul 1979 | A |
4262209 | Berner | Apr 1981 | A |
4266434 | Burns | May 1981 | A |
4288986 | Watson | Sep 1981 | A |
4295381 | Hinds | Oct 1981 | A |
4352023 | Sachs et al. | Sep 1982 | A |
4365437 | Jameson | Dec 1982 | A |
4423334 | Jacobi et al. | Dec 1983 | A |
4484083 | Jefferies | Nov 1984 | A |
4642988 | Benson | Feb 1987 | A |
4720640 | Anderson et al. | Jan 1988 | A |
5014564 | Culkin | May 1991 | A |
5123292 | Woltering | Jun 1992 | A |
5129600 | Polites | Jul 1992 | A |
5158493 | Morgrey | Oct 1992 | A |
5172599 | Woltering | Dec 1992 | A |
5313850 | Finvold et al. | May 1994 | A |
5396815 | Polites et al. | Mar 1995 | A |
5631514 | Garcia et al. | May 1997 | A |
5818115 | Nagao | Oct 1998 | A |
5955801 | Romero et al. | Sep 1999 | A |
5959375 | Garcia | Sep 1999 | A |
5994801 | Garcia | Nov 1999 | A |
6640659 | Jegatheeson | Nov 2003 | B1 |
6860166 | Hintz | Mar 2005 | B2 |
6876095 | Williams | Apr 2005 | B2 |
6926595 | Pollak et al. | Aug 2005 | B2 |
6956299 | Serrano Molina et al. | Oct 2005 | B2 |
7003947 | Kanki | Feb 2006 | B2 |
7105939 | Bednyak | Sep 2006 | B2 |
7124656 | Miller | Oct 2006 | B2 |
7239038 | Zimmerman et al. | Jul 2007 | B1 |
20030052564 | Wilsdorf | Mar 2003 | A1 |
20030067245 | Pelrine et al. | Apr 2003 | A1 |
20030220058 | Pollak et al. | Nov 2003 | A1 |
20040217671 | Rosenthal et al. | Nov 2004 | A1 |
20040222637 | Bednyak | Nov 2004 | A1 |
20040222638 | Bednyak | Nov 2004 | A1 |
20060178829 | Gaiffe | Aug 2006 | A1 |
20070050139 | Sidman | Mar 2007 | A1 |
20070075545 | Wilson et al. | Apr 2007 | A1 |
20070138793 | Zimmerman et al. | Jun 2007 | A1 |
20070228736 | Smushkovich | Oct 2007 | A1 |
Number | Date | Country | |
---|---|---|---|
60627349 | Nov 2004 | US |