US2549464A - Electric power source - Google Patents

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US2549464A
US2549464A US782703A US78270347A US2549464A US 2549464 A US2549464 A US 2549464A US 782703 A US782703 A US 782703A US 78270347 A US78270347 A US 78270347A US 2549464 A US2549464 A US 2549464A
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tube
heat
energy
gas
oscillations
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US782703A
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Ralph V L Hartley
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AT&T Corp
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Bell Telephone Laboratories Inc
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03GSPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G7/00Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
    • F03G7/002Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for using the energy of vibration of fluid columns
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02NELECTRIC MACHINES NOT OTHERWISE PROVIDED FOR
    • H02N11/00Generators or motors not provided for elsewhere; Alleged perpetua mobilia obtained by electric or magnetic means
    • H02N11/002Generators
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S116/00Signals and indicators
    • Y10S116/22Heated air

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Apparatuses For Generation Of Mechanical Vibrations (AREA)

Description

April 1 I R. v. HARTLEY 2,549,464
ELECTRIC POWER SOURCE Filed Oct. 29, 1947 uvvavron R. M L. HARTLEY ATTORNEY Patented Apr. 17, 1951 ELECTRIC POWER SOURCE Ralph V. L. Hartley, Summit, N. J., assignor to Bell Telephone Laboratories, Incorporated, New York, N. Y., a corporation of New York Application October 29, 1947, Serial No. 782,703
1 Claim. 1
This invention relates to electric power sources.
A general object of the invention is to derive electrical energy from heat energy in a novel manner. A subsidiary object is to derive electrical energy from the energy of vibration of a fluid column. A related object is to improve the emciency of thermo-acoustic vibrating systems.
It is known that compression waves of considerable amplitude may be set up in a column of air, gas, vapor or other elastic fluid confined in a pipe or tube, by the application of heat at a suitable point. In a simple form of the apparatus a cylindrical tube or pipe, open at both ends, is provided internally with a heatingelement, such as a screen of wire gauze, disposed approximately one-quarter of the distance from the lower end of the tube, to the upper end. Upon application of heat, as by a torch, to the screen, the fluid column, which in this case is a mixture of air and gases, breaks into violent oscillations, emitting a loud roaring sound. In a modified arrangement, the upper end of the tube is terminated in a resonant bulb or chamber. In still another modification, the heat may be applied directly, as by a flame, to the enclosed fluid column. If preferred, the heat of the flame may be applied externally to the walls of the tube. The oscillatory pressure pattern remains fixed with respect to the tube despite the steady convective flow of the fluid through the tube and away from the heat source. Thus the wave pattern advances with respect to the medium with a velocity equal to that of the medium with respect to the tube. These devices have in the past served as educational exhibits for illustrating ecoustical sional vibrations of the column are thus translated into electric currents which may then be supplied to a desired load. In addition, a part of the desired electrical energy may be fed back to control the timing of the application of heat, thus assisting in the maintenance of the oscillations.
In a modification, the tube is reentrant upon 2 itself, thus providing a closed path for a circuital fluid flow, and so conserving heat energy and increasing efiiciency.
The invention will be fully apprehended from the following detailed description of preferred embodiments thereof, taken in conjunction with the appended drawings, in which:
Fig. l is a schematic diagram of apparatus in accordance with the invention in one of its simplest forms;
Fig. 2 is a cross-section of the apparatus of Fig. 1 taken at the section 2-2;
Fig. 3 is a schematic diagram of a modification of Fig. 1;
Fig. 4 is a schematic diagram of another modification of the apparatus of Fig. 1;
Figs. 5 and 6 are two alternative forms of a further modification of the apparatus of Fig. 1; and
Fig. 7 is a diagrammatic representation of a screen structure alternative to that of Fig. 1.
Referring now to Fig. 1, there is provided a tube or pipe I, open at both ends and communicating with a second tube 2 at a point substantially midway between the two open ends of the first tube. Each tube may be of any suitable pressure resisting material, such as sheet metal or glass. The tube is preferably from 10 to 30 times its diameter. Ihus, for example, it may be about 5 feet in length and 4 inches in diameter.
At a point intermediate the lower end of the tube 1 and its mid-point, for example, about onefifth of the tube length from the lower end, there is provided a heating element which may comprise a screen of wire gauze, or a plurality of such screens 3 placed close to each other. This screen or screens may be shaped to flt the inside of the tube in any suitable manner and fixed in place in a plane approximately normal to the axis of the tube I either permanently or removably, as desired.
As is well known, upon the application of heat to the wire screen 3 by the flame 4 of a gas jet '5 or the like, the air or gas within the tube breaks into violent oscillations, standing compression waves are established and the tube emits a loud roaring sound. The wavelength of the fundamental component of the oscillations is approximately equal to twice the length of the tube. The mechanism by which this phenomenon takes place and whereby the steady heat energy applied to the screen 3 is converted into acoustical osciliatory energy has been many times described in the literature. In particular'it is described in The Theory of sound by Lord Rayleigh, volume 2, pages 226-235.
While the oscillations are in progress, the oscillating velocity of the particles of air or gas is greatest at the two ends of the tube while the oscillating pressures are greatest at the mid-point of the tube. This condition is indicated by the broken lines 6 which show, approximately, the instantaneous velocities of the air particles at various points along the length of the tube at two successive half cycles of the oscillations, one half cycle apart.
In accordance with the invention, the pressure energy, which is greatest in the central region of the tube I, is in part withdrawn to actuate a mechanical-electrical transducer. Thus a second tube 2 communicates with the vibrating air or gas column at the central point of the first tube I. The second tube 2 is terminated in a vibratile diaphragm which may be of conventional construction and which, when actuated by pressures within the tube, vibrates in the field of a permanent magnet 8, causing a current to flow in magnet winding 9 to which a load I0 may be connected.
Mechanical-electrical transducer elements of conventional form, including the telephone receiver schematically illustrated in Fig. 1, are characterised by impedances which, in the main, are high in comparison with the characteristic impedance of the vibrating air or gas column. Therefore, to withdraw substantial amounts of the energy of the vibrating column, some impedance matching device is desirable. A quarter wave impedance transformer is adequate for the purpose and accordingly the branch pipe 2 should be approximately one quarter wavelength from end to end, or, if preferred, an odd multiple of a quarter wavelength. The theory and operation of quarter wavelength transformers, both electrical and acoustical are well known per se and are described, for example, in Electromechanical Transducers and Wave Filters by W. P. Mason (Van Nostrand 1942). The quarter wavelength transformer or other impedance matching device is considered advantageous but is by no means essential, particularly because too perfect an impedance match between the vibrating air or gas column and the telephone receiver would result in too great a transfer of energy. If energy is withdrawn from the vibrating air column too rapidly the oscillations cannot be sustained.
It is to be understood that the pick-up device as shown in Fig. 1 may be replaced by any other suitable mechanical-electrical transducer, for example a piezoelectric element as in Fig. 6 or a magnetostrictive element as in Fig. 3.
The strength and the stability of the oscillations of the air or gas column are increased by the withdrawal of heat from a point intermediate the upper open end and the mid-point of this tube. To this end a cooling means II may be provided, for example, a screen of tubular members I2 as shown in Fig. 2, through the hollow meshes of which there flows a liquid such as water which may be circulated through a cooling radiator I3 external to the tube as by a pump M.
Fig. 3 shows a modification of the invention in which the upper end of the tube is closed by a bulb or resonator 2 I. Heat may be applied to a suitable point of the tube 20 by way of a heating element, such as wire gauze screens 3 as described in connection with Fig. 1. With this arrangement, high alternating pressures exist internally of the resonator 2| and the resonator wall therefore offers a suitable location for the electromechanical transducer. Thus a vibratile diaphragm 22 may be mounted in an aperture in the resonator wall and a magnetostrictive member 23 provided with a winding 24 which may be connected to a load 25, may be mounted externally to the resonator so that when the diaphragm is actuated by pressures within the radiator, the member 23 is vibrated within the winding 24 and so modifies the current of a battery 25 flowing through the winding 24 to establish a varying current in a load 25.
Fig. 4 shows a further modification of the apparatus in which the wire gauze screens 3 and burners 4 of Figs. 1 and 3 are replaced by the flame 30 of a gas jet 3I. This arrangement has the advantage that the heat may be applied intermittently and in synchronism with the oscillations of the air column in the tube I, by alternately increasing and reducing the strength of the flame 30. Various means may be resorted to for this purpose and two are indicated in the figure. Thus the length of the gas pipe 32, measured from a reservoir 33 to the jet 3| may be altered as by adjustment of a U-tube 34 until this gas pipe is itself a resonant gas column having the same resonant frequency as the main tube. When this relation has been attained, and with suitable adjustment of the gas pressure in the gas main 35, then the alternate rise and fall of the pressure within the main tube I reacts on the jet 3| to cause alternate increase and reduction of the gas flow and therefore of the height and strength of the flame 30. Again, a valve 36 may be inserted in the gas pipe 32 which valve is alternately opened and partially closed in synchronism with the oscillations in the main tube I. For example, the valve 36 may be operated by a relay 3'! which is energized as shown. Electric current is supplied from the magnet winding 9, by way of an adjustable phase controlling device 38 to the relay 31. With this arrangement the strength of the oscillations in the main tube I and therefore the oscillatory energy which is available for withdrawal to the load circuit In is increased as compared with its value when the application of heat is steady.
With the open ended tubes of Figs. 1 and 4, some heat energy inevitably escapes to the atmosphere without contributing to the energy supplied to the load ID. To reduce these losses, the tube may be turned back on itself and made reentrant to provide a return path as indicated in Figs. 5 and 6. Thus in Fig. 5 there are two heating elements 4| and two cooling elements 42, so arranged around the endless tube 40 that the gas or air in its travel meets first an element of one type and then an element of the other. These elements are indicated schematically and each heater may be a wire screen or screens to which heat may be applied by external means, as by a battery 43. The cooling elements 42 may be of any desired type, for example, screens of tubular material as indicated in Figs. 1 and 2. They may be cooled by units 44 which may comprise pump, radiator and fan as in Fig. 1. The full length of the closed tube 40, measured along its axis around the circuit and back to the same point, is a full wavelength of the enclosed air or gas column or an integral number of full wavelengths. In operation, there is a small steady flow in one direction superposed on the rapid air or gas particle movement of oscillation. The direction of this movement depends on the arrangement and supply of the heating and cooling elements. Thus, if a large amount of heat is applied to the heater 4| at the lower portion of the left-hand branch of Fig. 5 and a smaller amount at the upper end of the right-hand branch, there will be a net convective flow of the air or gas in the tube in a clockwise direction and oscillations will be sustained. If the heating elements are placed at the lower part of the right hand branch and at the upper part of the lefthand branch with the cooling elements between them, and the heat supplied to the former element exceeds that supplied to the latter, the convective flow will be in a counterclockwise direction and operation will be otherwise the same.
Energy of vibration may be withdrawn from suitable high pressure points of the system, for example from the mid-points of both tube branches. To this end a branch pipe 45 which may be one-quarter wavelength long communicates with one vertical leg of the closed tube 40 substantially at its mid-point, and a similar branch pipe 45' communicates with the other vertical leg at its mid-point. Each branch pipe 45, 45' may be terminated in a mechanicalelectrical transducer which may be of the electromagnetic type described above and including a diaphragm 1, a magnet 8 and windings 9, or of any other suitable type. The outputs of these two transducers may be together fed to a desired load 47 and they may be connected in parallel, although it is preferred to interpose an adjustable phase adjusting device 48 between them to compensate for any phase displacement which may exist between the oscillating pressures of the two branch pipes.
Fig. 6 shows a variant of Fig. 5 in which a single mechanical-electrical transducer, here shown by way of example as a piezoelectric element 50, is coupled to both branch pipes 5|, 5| of the reentrant tube 4|]. In other respects the apparatus of Fig. 6 may be the same as that of Fig. 5, and its operation is similar. case of Fig. 5, the heat supplied to the upward flowing branch should exceed that supplied to the downward flowing branch by an amount suflicient to sustain the steady convective flow in one particular direction and overcome the retarding effect of friction against the tube walls.
The closed reentrant tube arrangements of Fig. 5 and 6 lend themselves to use with the vapor of a high boiling point liquid such as mercury. This serves to facilitate the interchange of heat energy from the vibrating fluid column to the heater screens M and increases the efficiency of energy transfer to a high impedance mechanical-electrical transducer such as the piezoelectric element 50.
Wherever a wire gauze screen is employed, improved results may be obtained by the use of As in the several such screens placed close together with their openings staggered so that as much as w possible of the fluid passing through the screen comes into immediate contact with one or other wire of the mesh, thus facilitating transfer of heat from the wire screen to the fluid. This con struction is shown in Fig. 7. 1
What is claimed is:
A source of oscillatory energy comprising a tubular resonator, an elastic fluid within said resonator and capable of supporting standing compression waves of wavelength and fre-- quency determined by the dimensions of said resonator, means for periodically applying heat at a selected point of said resonator to said fluid. whereby standing compression waves are developed in said fluid, means, including a mechanical-electrical transducer coupled to said fluid, for withdrawing a portion of the oscillatory energy of said compression waves, and means for feeding back a portion of the output of said transducer to control the timing of said periodic application of heat.
RALPH V. L. HARTLEY.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 782,146 Laudet Feb. 7, 1905 1,213,611 Fessenden Jan. 23, 1917 1,481,270 Purcell Jan. 22, 1924 1,493,340 Hahnemann et a1. May 6, 1924 1,510,476 Hammond Oct. '7, 1924 1,544,010 Jordan June 30, 1925 1,795,647 Flanders W Mar. 10, 1931 1,954,516 Bourne Apr. 10, 1934 1,969,037 Rieber Aug. 7, 1934 2,017,744 Bourne Oct. 15, 1935 2,075,263 Bourne Mar. 30, 1937 2,094,621 Savage Oct. 5, 1937 2,111,036 Wippel Mar. 15, 1938 2,198,521 Whitelegg Apr. 23, 1940 2,215,895 Wippel Sept. 24, 1940 2,259,858 Reid Oct. 21, 1941 2,278,668 Piety Apr. '7, 1942 2,362,151 Ostenberg Nov. 7, 1944 2,389,067 Lieberman 1- Nov. 13, 1945 FOREIGN PATENTS Number Country Date 188,642 Great Britain Nov. 29, 1923 424,955 Great Britain May 31, 1933 OTHER REFERENCES The Theory of Sound, by Lord Rayleigh, volume 2, pages 226-235.
Electromechanical Transducers and Wave Filters, by W. P. Mason (Van Nostrand, 1942).
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Cited By (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2767783A (en) * 1952-09-09 1956-10-23 Scully Signal Co Sonic control for burners
US2836033A (en) * 1953-07-15 1958-05-27 Bell Telephone Labor Inc Heat-controlled acoustic wave system
US3066482A (en) * 1959-02-02 1962-12-04 Acoustica Associates Inc Combustion control system
US3131671A (en) * 1960-04-22 1964-05-05 Richard W Fetter Acoustic generator
US3133591A (en) * 1954-05-20 1964-05-19 Orpha B Brandon Method and apparatus for forming and/or augmenting an energy wave
US3141099A (en) * 1959-08-03 1964-07-14 Orpha B Brandon Method and apparatus for forming and/or augmenting an energy wave
US3247901A (en) * 1954-05-20 1966-04-26 Harvey B Jacobson Method and apparatus for forming and/or augmenting an energy wave
US3339635A (en) * 1965-10-22 1967-09-05 Clarence W Brandon Method and apparatus for forming and/or augmenting an energy wave
US3438352A (en) * 1954-06-03 1969-04-15 Orpha B Brandon Method for forming and/or augmenting an energy wave
US3503446A (en) * 1968-05-13 1970-03-31 Clarence W Brandon Method and apparatus for forming and/or augmenting an energy wave
US3503366A (en) * 1962-06-29 1970-03-31 Clarence W Brandon Apparatus for forming and/or augmenting an energy wave
US3548589A (en) * 1968-01-19 1970-12-22 Atomic Energy Authority Uk Heat engines
US3693604A (en) * 1970-12-01 1972-09-26 John J Horan Resonant energy-conversion systems with fluid-energy inputs
US3799205A (en) * 1966-07-18 1974-03-26 Us Army Fluid oscillators
US4215426A (en) * 1978-05-01 1980-07-29 Frederick Klatt Telemetry and power transmission for enclosed fluid systems
US4355517A (en) * 1980-11-04 1982-10-26 Ceperley Peter H Resonant travelling wave heat engine
FR2511427A1 (en) * 1981-08-14 1983-02-18 Us Energy ACOUSTIC THERMAL MOTOR WITH STATIONARY SEALING DEVICES
US4468568A (en) * 1982-07-02 1984-08-28 Carr Jr Walter J Generating power from the ocean utilizing the thermal properties of magnetic material
EP0130143A1 (en) * 1983-06-20 1985-01-02 GebràœDer Sulzer Aktiengesellschaft Refrigeration machine or heat pump
WO1990011447A1 (en) * 1989-03-17 1990-10-04 Cornelis Maria De Blok Device for utilizing heat via conversion into mechanical energy, in particular a cooling device
EP0511422A1 (en) * 1991-04-30 1992-11-04 International Business Machines Corporation Low temperature generation process and expansion engine
US5357757A (en) * 1988-10-11 1994-10-25 Macrosonix Corp. Compression-evaporation cooling system having standing wave compressor
US6375454B1 (en) 1999-11-12 2002-04-23 Sarcos, L.C. Controllable combustion device
EP1201906A3 (en) * 2000-10-16 2003-04-16 Honda Giken Kogyo Kabushiki Kaisha Exhaust heat energy recovery system for internal combustion engine
US20030108830A1 (en) * 1999-11-12 2003-06-12 Sarcos,Lc; Controllable combustion method and device
US20030192324A1 (en) * 2002-04-10 2003-10-16 Smith Robert W. M. Thermoacoustic device
US20030192322A1 (en) * 2002-04-10 2003-10-16 Garrett Steven L. Cylindrical spring with integral dynamic gas seal
US20030192323A1 (en) * 2002-04-10 2003-10-16 Poese Mathew E. Compliant enclosure for thermoacoustic device
US6876094B2 (en) 1999-11-12 2005-04-05 Sarcos, Lc Resonant electrical generation system
US20060156727A1 (en) * 1999-11-12 2006-07-20 Jacobsen Stephen C Method and apparatus for phase change driven actuator
WO2009038500A1 (en) * 2007-09-17 2009-03-26 Picoterm Ab An arrangement adapted for energy transformation

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US1213611A (en) * 1913-05-31 1917-01-23 Submarine Signal Co Dynamo-electric machinery.
GB188642A (en) * 1921-11-07 1923-11-29 Georges Celestin Alexandre Lau Device for the application of periodic explosions of gaseous explosive mixtures or of the periodical stoppage of gaseous fluids under pressure to the operation of turbines and other energy recovering apparatus
US1481270A (en) * 1920-12-18 1924-01-22 Hydromotor Company Inc Process and device for obtaining a reciprocating movement
US1493340A (en) * 1923-04-06 1924-05-06 Eleonore Du Bois Rey Mond Device for converting a continuous flow of energy into a wavelike flow of energy
US1510476A (en) * 1922-07-08 1924-10-07 Walter W Slack Tone-amplifying apparatus for musical instruments
US1544010A (en) * 1923-04-24 1925-06-30 L Air Liquide Soc Generator of electric current
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US1954516A (en) * 1931-10-19 1934-04-10 Maxim Silencer Co Sound attenuating device
US1969037A (en) * 1934-08-07 High frequency wave signaling
GB424955A (en) * 1933-05-31 1935-03-04 Jean Edouard Andreau Apparatus for producing a compressed gaseous medium by combustion
US2017744A (en) * 1934-04-30 1935-10-15 Maxim Silencer Co Sound attenuating device
US2075263A (en) * 1931-10-19 1937-03-30 Maxim Silencer Co Sound attenuating device
US2094621A (en) * 1935-06-06 1937-10-05 Edward S Savage Motor
US2111036A (en) * 1936-03-16 1938-03-15 Julius F Wippel Fluid velocity vibratory motor
US2198521A (en) * 1939-03-07 1940-04-23 Richard O Whitelegg Method and apparatus for electrically reproducing sound vibrations
US2215895A (en) * 1938-04-04 1940-09-24 Julius F Wippel Fluid velocity motor operated generator
US2259858A (en) * 1938-11-25 1941-10-21 Reid Ebenezer Emmet Musical instrument
US2278668A (en) * 1939-01-12 1942-04-07 Rca Corp Demodulation of frequency modulated oscillations
US2362151A (en) * 1943-08-18 1944-11-07 Ostenberg Pontus Electric generator
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US1969037A (en) * 1934-08-07 High frequency wave signaling
US782146A (en) * 1903-12-01 1905-02-07 Georges Laudet Apparatus for the reproduction and amplification of sound.
US1213611A (en) * 1913-05-31 1917-01-23 Submarine Signal Co Dynamo-electric machinery.
US1481270A (en) * 1920-12-18 1924-01-22 Hydromotor Company Inc Process and device for obtaining a reciprocating movement
GB188642A (en) * 1921-11-07 1923-11-29 Georges Celestin Alexandre Lau Device for the application of periodic explosions of gaseous explosive mixtures or of the periodical stoppage of gaseous fluids under pressure to the operation of turbines and other energy recovering apparatus
US1510476A (en) * 1922-07-08 1924-10-07 Walter W Slack Tone-amplifying apparatus for musical instruments
US1493340A (en) * 1923-04-06 1924-05-06 Eleonore Du Bois Rey Mond Device for converting a continuous flow of energy into a wavelike flow of energy
US1544010A (en) * 1923-04-24 1925-06-30 L Air Liquide Soc Generator of electric current
US1795647A (en) * 1929-02-19 1931-03-10 Bell Telephone Labor Inc Method and apparatus for measuring acoustical impedances
US2075263A (en) * 1931-10-19 1937-03-30 Maxim Silencer Co Sound attenuating device
US1954516A (en) * 1931-10-19 1934-04-10 Maxim Silencer Co Sound attenuating device
GB424955A (en) * 1933-05-31 1935-03-04 Jean Edouard Andreau Apparatus for producing a compressed gaseous medium by combustion
US2017744A (en) * 1934-04-30 1935-10-15 Maxim Silencer Co Sound attenuating device
US2094621A (en) * 1935-06-06 1937-10-05 Edward S Savage Motor
US2111036A (en) * 1936-03-16 1938-03-15 Julius F Wippel Fluid velocity vibratory motor
US2215895A (en) * 1938-04-04 1940-09-24 Julius F Wippel Fluid velocity motor operated generator
US2259858A (en) * 1938-11-25 1941-10-21 Reid Ebenezer Emmet Musical instrument
US2278668A (en) * 1939-01-12 1942-04-07 Rca Corp Demodulation of frequency modulated oscillations
US2198521A (en) * 1939-03-07 1940-04-23 Richard O Whitelegg Method and apparatus for electrically reproducing sound vibrations
US2362151A (en) * 1943-08-18 1944-11-07 Ostenberg Pontus Electric generator
US2389067A (en) * 1943-11-13 1945-11-13 Edgar M Lieberman Thermal pump

Cited By (46)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2767783A (en) * 1952-09-09 1956-10-23 Scully Signal Co Sonic control for burners
US2836033A (en) * 1953-07-15 1958-05-27 Bell Telephone Labor Inc Heat-controlled acoustic wave system
US3133591A (en) * 1954-05-20 1964-05-19 Orpha B Brandon Method and apparatus for forming and/or augmenting an energy wave
US3247901A (en) * 1954-05-20 1966-04-26 Harvey B Jacobson Method and apparatus for forming and/or augmenting an energy wave
US3438352A (en) * 1954-06-03 1969-04-15 Orpha B Brandon Method for forming and/or augmenting an energy wave
US3066482A (en) * 1959-02-02 1962-12-04 Acoustica Associates Inc Combustion control system
US3141099A (en) * 1959-08-03 1964-07-14 Orpha B Brandon Method and apparatus for forming and/or augmenting an energy wave
US3131671A (en) * 1960-04-22 1964-05-05 Richard W Fetter Acoustic generator
US3503366A (en) * 1962-06-29 1970-03-31 Clarence W Brandon Apparatus for forming and/or augmenting an energy wave
US3339635A (en) * 1965-10-22 1967-09-05 Clarence W Brandon Method and apparatus for forming and/or augmenting an energy wave
US3799205A (en) * 1966-07-18 1974-03-26 Us Army Fluid oscillators
US3548589A (en) * 1968-01-19 1970-12-22 Atomic Energy Authority Uk Heat engines
US3503446A (en) * 1968-05-13 1970-03-31 Clarence W Brandon Method and apparatus for forming and/or augmenting an energy wave
US3693604A (en) * 1970-12-01 1972-09-26 John J Horan Resonant energy-conversion systems with fluid-energy inputs
US4215426A (en) * 1978-05-01 1980-07-29 Frederick Klatt Telemetry and power transmission for enclosed fluid systems
US4355517A (en) * 1980-11-04 1982-10-26 Ceperley Peter H Resonant travelling wave heat engine
FR2511427A1 (en) * 1981-08-14 1983-02-18 Us Energy ACOUSTIC THERMAL MOTOR WITH STATIONARY SEALING DEVICES
US4468568A (en) * 1982-07-02 1984-08-28 Carr Jr Walter J Generating power from the ocean utilizing the thermal properties of magnetic material
EP0130143A1 (en) * 1983-06-20 1985-01-02 GebràœDer Sulzer Aktiengesellschaft Refrigeration machine or heat pump
US5357757A (en) * 1988-10-11 1994-10-25 Macrosonix Corp. Compression-evaporation cooling system having standing wave compressor
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