GB188642A - 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 - Google Patents

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

Info

Publication number
GB188642A
GB188642A GB27857/22A GB2785722A GB188642A GB 188642 A GB188642 A GB 188642A GB 27857/22 A GB27857/22 A GB 27857/22A GB 2785722 A GB2785722 A GB 2785722A GB 188642 A GB188642 A GB 188642A
Authority
GB
United Kingdom
Prior art keywords
pipe
gaseous
turbines
nodes
application
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
GB27857/22A
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.)
GEORGES CELESTIN ALEXANDRE LAU
Original Assignee
GEORGES CELESTIN ALEXANDRE LAU
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 GEORGES CELESTIN ALEXANDRE LAU filed Critical GEORGES CELESTIN ALEXANDRE LAU
Publication of GB188642A publication Critical patent/GB188642A/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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B06—GENERATING OR TRANSMITTING MECHANICAL VIBRATIONS IN GENERAL
    • B06B—METHODS OR APPARATUS FOR GENERATING OR TRANSMITTING MECHANICAL VIBRATIONS OF INFRASONIC, SONIC, OR ULTRASONIC FREQUENCY, e.g. FOR PERFORMING MECHANICAL WORK IN GENERAL
    • B06B1/00—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency
    • B06B1/02—Methods or apparatus for generating mechanical vibrations of infrasonic, sonic, or ultrasonic frequency making use of electrical energy
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N5/00—Exhaust or silencing apparatus combined or associated with devices profiting by exhaust energy
    • F01N5/04—Exhaust or silencing apparatus combined or associated with devices profiting by exhaust energy the devices using kinetic energy
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/10—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect
    • 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
    • F04F5/02—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being liquid
    • F04F5/04—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being liquid displacing elastic fluids
    • F04F5/06—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being liquid displacing elastic fluids of rotary type
    • 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
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Measuring Fluid Pressure (AREA)

Abstract

188,642. Laudet, G. C. A. Nov. 7, 1921. [Convention date]. Percussive tools.-Resonating chambers containing fluid, in which nodes and antinodes are produced in a manner similar to the sounding of an organ pipe, are used as elements in prime-movers. In the example shown in Fig. 7, a V-shaped pipe 21, 22 is sounded by the passage of the products of explosions through the throat 20 and an impulse turbine wheel 25 placed at an antinode in the pipe is rotated by means of the axial oscillations of the fluid in the pipe at that place. In Fig. 4, a pipe is shown which is excited by the periodic admission of a pressure fluid by way of a single inlet valve I or a valve at each end, the valves being operated in the proper phase relation. The action can also be assisted by the timed opening of valves at the nodes which communicate with suction apparatus. Gases introduced into the pipes do not travel beyond the first node and may be allowed to escape by an opening at the first anti-node. Cutting-tools and connecting-rod or ratchet mechanisms may be operated by the alternations of pressure obtaining at the nodes. Several examples of the application to turbines are given.
GB27857/22A 1921-11-07 1922-10-13 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 Expired GB188642A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR188642X 1921-11-07

Publications (1)

Publication Number Publication Date
GB188642A true GB188642A (en) 1923-11-29

Family

ID=8878832

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27857/22A Expired GB188642A (en) 1921-11-07 1922-10-13 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

Country Status (1)

Country Link
GB (1) GB188642A (en)

Cited By (17)

* 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
US2532096A (en) * 1946-03-16 1950-11-28 Bell Telephone Labor Inc Power source
US2543758A (en) * 1947-06-13 1951-03-06 Jr Albert G Bodine Standing wave heat engine with means for supplying auxiliary air
US2549464A (en) * 1947-10-29 1951-04-17 Bell Telephone Labor Inc Electric power source
US2573697A (en) * 1945-07-30 1951-11-06 James Y Dunbar Multitube mosaic reso-jet motor
US2602291A (en) * 1947-12-16 1952-07-08 Ingersoll Rand Co Resonant explosion power unit with dilution air
US2614387A (en) * 1946-09-17 1952-10-21 Ingersoll Rand Co Intermittent explosion unit for gas turbine plants
US2627163A (en) * 1947-12-16 1953-02-03 Ingersoll Rand Co One-half wave length resonant explosion gas unit
US2629983A (en) * 1948-01-14 1953-03-03 Ingersoll Rand Co Resonant explosion gas turbine plant with a mixing chamber
US2635420A (en) * 1947-05-14 1953-04-21 Shell Dev Jet propulsion engine with auxiliary pulse jet engine
US2731795A (en) * 1956-01-24 bodine
DE947124C (en) * 1943-04-14 1956-08-09 Eberspaecher J Heat exchanger for utilizing the heat from combustion gases
US2796735A (en) * 1956-08-20 1957-06-25 Jr Albert G Bodine Acoustic jet engine with flow deflection fluid pumping characteristics
DE970736C (en) * 1950-04-07 1958-10-23 Kaercher Fa Alfred Device for mixture preparation in burners with a vibrating gas column
DE1075098B (en) * 1960-02-11 Dipl.-Ing. Helmuth Ehlermann und Heinrich Richter, Bad Lippspringe Method and device for treating gases
US3330378A (en) * 1964-09-30 1967-07-11 Chicago Pneumatic Tool Co Pneumatic grinder with integral exhaust silencer
WO2010056520A1 (en) * 2008-11-14 2010-05-20 General Electric Company Multi-tube, can-annular pulse detonation combustor based engine

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1075098B (en) * 1960-02-11 Dipl.-Ing. Helmuth Ehlermann und Heinrich Richter, Bad Lippspringe Method and device for treating gases
US2731795A (en) * 1956-01-24 bodine
DE947124C (en) * 1943-04-14 1956-08-09 Eberspaecher J Heat exchanger for utilizing the heat from combustion gases
US2573697A (en) * 1945-07-30 1951-11-06 James Y Dunbar Multitube mosaic reso-jet motor
US2532096A (en) * 1946-03-16 1950-11-28 Bell Telephone Labor Inc Power source
US2614387A (en) * 1946-09-17 1952-10-21 Ingersoll Rand Co Intermittent explosion unit for gas turbine plants
US2635420A (en) * 1947-05-14 1953-04-21 Shell Dev Jet propulsion engine with auxiliary pulse jet engine
US2543758A (en) * 1947-06-13 1951-03-06 Jr Albert G Bodine Standing wave heat engine with means for supplying auxiliary air
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
US2602291A (en) * 1947-12-16 1952-07-08 Ingersoll Rand Co Resonant explosion power unit with dilution air
US2627163A (en) * 1947-12-16 1953-02-03 Ingersoll Rand Co One-half wave length resonant explosion gas unit
US2629983A (en) * 1948-01-14 1953-03-03 Ingersoll Rand Co Resonant explosion gas turbine plant with a mixing chamber
DE970736C (en) * 1950-04-07 1958-10-23 Kaercher Fa Alfred Device for mixture preparation in burners with a vibrating gas column
US2796735A (en) * 1956-08-20 1957-06-25 Jr Albert G Bodine Acoustic jet engine with flow deflection fluid pumping characteristics
US3330378A (en) * 1964-09-30 1967-07-11 Chicago Pneumatic Tool Co Pneumatic grinder with integral exhaust silencer
WO2010056520A1 (en) * 2008-11-14 2010-05-20 General Electric Company Multi-tube, can-annular pulse detonation combustor based engine

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