GB424955A - Apparatus for producing a compressed gaseous medium by combustion - Google Patents

Apparatus for producing a compressed gaseous medium by combustion

Info

Publication number
GB424955A
GB424955A GB1575033A GB1575033A GB424955A GB 424955 A GB424955 A GB 424955A GB 1575033 A GB1575033 A GB 1575033A GB 1575033 A GB1575033 A GB 1575033A GB 424955 A GB424955 A GB 424955A
Authority
GB
United Kingdom
Prior art keywords
chamber
valve
air
explosion
pressure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB1575033A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB1575033A priority Critical patent/GB424955A/en
Publication of GB424955A publication Critical patent/GB424955A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C15/00—Apparatus in which combustion takes place in pulses influenced by acoustic resonance in a gas mass
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
    • F02K7/04—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet with resonant combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/14—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being elastic fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24—HEATING; RANGES; VENTILATING
    • F24C—DOMESTIC STOVES OR RANGES ; DETAILS OF DOMESTIC STOVES OR RANGES, OF GENERAL APPLICATION
    • F24C1/00—Stoves or ranges in which the fuel or energy supply is not restricted to solid fuel or to a type covered by a single one of the following groups F24C3/00 - F24C9/00; Stoves or ranges in which the type of fuel or energy supply is not specified

Abstract

424,955. Gas turbines. ANDREAU, J. E., 73, Boulevard Montparnasse, Paris. May 31, 1933, No. 15750. Void [Abridged as open to inspection under Sect. 91 of the Acts, Dec. 1, 1933]. [Class 110 (iii)] In apparatus for producing products of combustion for use in a turbine &c., of the type in which an oscillating wave is set up in the explosion chamber, the rhythm of the ignition is maintained in resonance with the fundamental frequency of the wave. In Fig. 1 the explosion chamber 1 is fitted with a flexible admission valve 2 and a similar discharge valve 4 leading to a receiving chamber 3 and a delivery nozzle 5. The spark at 6, derived from a transformer 7, is controlled by a continuously vibrating blade 9. The periodicity of vibration may be altered by moving a weight 101 automatically along the blade in accordance with variations in mean pressure in the explosion chamber 1. In Fig. 9, carburetted air is drawn into the chamber 1 past a valve 15, and pure air through a surrounding shield 30 and past valves 2. This latter air serves to cool the sparking plugs 6, of which there may be a number firing in definite sequence, and also the intermediate passage 13. Starting may be effected by admitting compressed air intermittently by a valve controlled by a vibrating blade. In Fig. 9 a hand-actuated pump 26 is used to supply carburetted air on starting. Communication with the delivery nozzle 5 is prevented by a valve 31 until pressure has been established in the chamber 3. In the modification shown in Fig. 6, the charge of carburetted air drawn past the valve 15 by the explosion wave is precompressed by a differential piston 16, the chamber 17 at one end of which is open to the pressure at one point in the explosion chamber. This piston may also control the ignition, and the injection of fuel oil when such is used. The ignition distributer may be driven by an electric motor the speed of which depends upon the pressure in the chamber 1.
GB1575033A 1933-05-31 1933-05-31 Apparatus for producing a compressed gaseous medium by combustion Expired GB424955A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1575033A GB424955A (en) 1933-05-31 1933-05-31 Apparatus for producing a compressed gaseous medium by combustion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1575033A GB424955A (en) 1933-05-31 1933-05-31 Apparatus for producing a compressed gaseous medium by combustion

Publications (1)

Publication Number Publication Date
GB424955A true GB424955A (en) 1935-03-04

Family

ID=10064813

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1575033A Expired GB424955A (en) 1933-05-31 1933-05-31 Apparatus for producing a compressed gaseous medium by combustion

Country Status (1)

Country Link
GB (1) GB424955A (en)

Cited By (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2480626A (en) * 1947-11-03 1949-08-30 Jr Albert G Bodine Resonant wave pulse engine and process
US2523378A (en) * 1945-11-28 1950-09-26 Kollsman Paul Wing-mounted jet reaction engine for aircraft
US2532096A (en) * 1946-03-16 1950-11-28 Bell Telephone Labor Inc Power source
US2546965A (en) * 1947-06-11 1951-04-03 Jr Albert G Bodine Pulse jet standing wave engine with movable wave reflecting means
US2549464A (en) * 1947-10-29 1951-04-17 Bell Telephone Labor Inc Electric power source
US2550515A (en) * 1947-11-19 1951-04-24 Ingersoll Rand Co Gas compressor
US2581669A (en) * 1945-04-13 1952-01-08 Nina K Guercken Gas turbine power plant with tank supplied by long conduit having volume over six times that of the intermittent combustion gas generator
US2601471A (en) * 1947-05-22 1952-06-24 Vang Alfred Jet propulsion means having vibrator therein
US2613496A (en) * 1945-08-20 1952-10-14 Kollsman Paul Intermittent duct engine
US2617254A (en) * 1948-01-29 1952-11-11 Ingersoll Rand Co Explosion gas turbine plant
DE767657C (en) * 1938-07-28 1953-03-16 Paul Dipl-Ing Schmidt Method for generating recoil forces by means of fuel-air mixtures
DE767584C (en) * 1940-03-07 1953-07-06 Paul Dipl-Ing Schmidt Recoil drive with direct acceleration of air
US2644512A (en) * 1949-06-13 1953-07-07 Heizmotoren Ges Uberlingen Am Burner device having heat exchange and gas flow control means for maintaining pyrophoric ignition therein
US2650472A (en) * 1944-07-17 1953-09-01 Whitworth & Co Resonating combustion power gas generator
US2653654A (en) * 1950-02-16 1953-09-29 Wunibald I E Kamm Gas starter for resonant pulse jet burners
DE898102C (en) * 1942-08-28 1953-11-26 Karl Dr-Ing Leist Method and device for operating combustion chambers controlled by the pressure of the combustion gases, in particular for recoil engines or turbines
US2695053A (en) * 1949-06-13 1954-11-23 Swingfire Bahamas Ltd Intermittent combustion device provided with means for controlling the combustion gas flow therein
DE768063C (en) * 1942-05-17 1955-06-02 Messerschmitt Boelkow Blohm Device for the ignition of combustion chambers for hot jet engines
US2709891A (en) * 1945-06-13 1955-06-07 James Y Dunbar Valveless resonating jet motor
US2731795A (en) * 1956-01-24 bodine
US2767783A (en) * 1952-09-09 1956-10-23 Scully Signal Co Sonic control for burners
DE951829C (en) * 1950-02-11 1956-11-08 Kaercher Fa Alfred Burner with free-swinging gas column
DE963549C (en) * 1952-05-31 1957-05-09 Erik Torvald Linderoth Thermodynamic fan
DE966676C (en) * 1954-11-05 1957-08-29 Maschf Augsburg Nuernberg Ag Plant for the generation of hot compressed gases
US2872780A (en) * 1952-04-12 1959-02-10 Schmidt Paul Pulse jet engine with acceleration chamber
US2919547A (en) * 1953-07-13 1960-01-05 John A Melenric Vibrator starter for pulse jet engines
US2930196A (en) * 1951-03-30 1960-03-29 Cornell Aeronautical Labor Inc Valved intermittent combustion reaction engine
US2960314A (en) * 1959-07-06 1960-11-15 Jr Albert G Bodine Method and apparatus for generating and transmitting sonic vibrations
US3034299A (en) * 1960-05-02 1962-05-15 Robert B Hammett Apparatus and method for effecting a wave intermediary thermodynamic cycle
US3756763A (en) * 1969-10-27 1973-09-04 Pulsepower Systems Pulsed high pressure liquid propellant combustion powered gas generators
US4260361A (en) * 1978-10-10 1981-04-07 Ludwig Huber Resonant or pulsating combustion heating apparatus
CN108870439A (en) * 2018-07-27 2018-11-23 中国东方电气集团有限公司 A kind of combustion oscillation control structure for combustion apparatus

Cited By (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2731795A (en) * 1956-01-24 bodine
DE767657C (en) * 1938-07-28 1953-03-16 Paul Dipl-Ing Schmidt Method for generating recoil forces by means of fuel-air mixtures
DE767584C (en) * 1940-03-07 1953-07-06 Paul Dipl-Ing Schmidt Recoil drive with direct acceleration of air
DE768063C (en) * 1942-05-17 1955-06-02 Messerschmitt Boelkow Blohm Device for the ignition of combustion chambers for hot jet engines
DE898102C (en) * 1942-08-28 1953-11-26 Karl Dr-Ing Leist Method and device for operating combustion chambers controlled by the pressure of the combustion gases, in particular for recoil engines or turbines
US2650472A (en) * 1944-07-17 1953-09-01 Whitworth & Co Resonating combustion power gas generator
US2581669A (en) * 1945-04-13 1952-01-08 Nina K Guercken Gas turbine power plant with tank supplied by long conduit having volume over six times that of the intermittent combustion gas generator
US2709891A (en) * 1945-06-13 1955-06-07 James Y Dunbar Valveless resonating jet motor
US2613496A (en) * 1945-08-20 1952-10-14 Kollsman Paul Intermittent duct engine
US2523378A (en) * 1945-11-28 1950-09-26 Kollsman Paul Wing-mounted jet reaction engine for aircraft
US2532096A (en) * 1946-03-16 1950-11-28 Bell Telephone Labor Inc Power source
US2601471A (en) * 1947-05-22 1952-06-24 Vang Alfred Jet propulsion means having vibrator therein
US2546965A (en) * 1947-06-11 1951-04-03 Jr Albert G Bodine Pulse jet standing wave engine with movable wave reflecting means
US2549464A (en) * 1947-10-29 1951-04-17 Bell Telephone Labor Inc Electric power source
US2480626A (en) * 1947-11-03 1949-08-30 Jr Albert G Bodine Resonant wave pulse engine and process
US2550515A (en) * 1947-11-19 1951-04-24 Ingersoll Rand Co Gas compressor
US2617254A (en) * 1948-01-29 1952-11-11 Ingersoll Rand Co Explosion gas turbine plant
US2695053A (en) * 1949-06-13 1954-11-23 Swingfire Bahamas Ltd Intermittent combustion device provided with means for controlling the combustion gas flow therein
US2644512A (en) * 1949-06-13 1953-07-07 Heizmotoren Ges Uberlingen Am Burner device having heat exchange and gas flow control means for maintaining pyrophoric ignition therein
DE951829C (en) * 1950-02-11 1956-11-08 Kaercher Fa Alfred Burner with free-swinging gas column
US2653654A (en) * 1950-02-16 1953-09-29 Wunibald I E Kamm Gas starter for resonant pulse jet burners
US2930196A (en) * 1951-03-30 1960-03-29 Cornell Aeronautical Labor Inc Valved intermittent combustion reaction engine
US2872780A (en) * 1952-04-12 1959-02-10 Schmidt Paul Pulse jet engine with acceleration chamber
DE963549C (en) * 1952-05-31 1957-05-09 Erik Torvald Linderoth Thermodynamic fan
US2767783A (en) * 1952-09-09 1956-10-23 Scully Signal Co Sonic control for burners
US2919547A (en) * 1953-07-13 1960-01-05 John A Melenric Vibrator starter for pulse jet engines
DE966676C (en) * 1954-11-05 1957-08-29 Maschf Augsburg Nuernberg Ag Plant for the generation of hot compressed gases
US2960314A (en) * 1959-07-06 1960-11-15 Jr Albert G Bodine Method and apparatus for generating and transmitting sonic vibrations
US3034299A (en) * 1960-05-02 1962-05-15 Robert B Hammett Apparatus and method for effecting a wave intermediary thermodynamic cycle
US3756763A (en) * 1969-10-27 1973-09-04 Pulsepower Systems Pulsed high pressure liquid propellant combustion powered gas generators
US4260361A (en) * 1978-10-10 1981-04-07 Ludwig Huber Resonant or pulsating combustion heating apparatus
CN108870439A (en) * 2018-07-27 2018-11-23 中国东方电气集团有限公司 A kind of combustion oscillation control structure for combustion apparatus

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