BE508930A - - Google Patents

Info

Publication number
BE508930A
BE508930A BE508930DA BE508930A BE 508930 A BE508930 A BE 508930A BE 508930D A BE508930D A BE 508930DA BE 508930 A BE508930 A BE 508930A
Authority
BE
Belgium
Application number
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.)
Publication of BE508930A publication Critical patent/BE508930A/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/224—Heating fuel before feeding to the burner

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
BE508930D 1951-02-10 BE508930A (pm)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US210347A US2704438A (en) 1951-02-10 1951-02-10 Starting fuel system for jet and rocket motors

Publications (1)

Publication Number Publication Date
BE508930A true BE508930A (pm)

Family

ID=22782546

Family Applications (1)

Application Number Title Priority Date Filing Date
BE508930D BE508930A (pm) 1951-02-10

Country Status (3)

Country Link
US (1) US2704438A (pm)
BE (1) BE508930A (pm)
GB (1) GB704622A (pm)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2323884A1 (fr) * 1975-09-12 1977-04-08 Rolls Royce Circuit de carburant pour turbomachines
FR2728627A1 (fr) * 1994-12-27 1996-06-28 Europ Propulsion Autopressurisation de reservoir

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2958189A (en) * 1955-05-31 1960-11-01 Phillips Petroleum Co Method and apparatus for providing improved combustion in jet engines
US2953898A (en) * 1956-10-22 1960-09-27 Holley Carburetor Co Afterburner apparatus
US3077073A (en) * 1957-10-29 1963-02-12 United Aircraft Corp Rocket engine having fuel driven propellant pumps
US3073119A (en) * 1958-12-08 1963-01-15 United Aircraft Corp Rocket propellant system
US3094838A (en) * 1959-06-17 1963-06-25 United Aircraft Corp Thrust control system
US3078659A (en) * 1959-06-30 1963-02-26 United Aircraft Corp Liquid rocket engine system
US3162009A (en) * 1959-06-30 1964-12-22 United Aircraft Corp Rocket motor control system
US3049870A (en) * 1960-04-14 1962-08-21 United Aircraft Corp Rocket propellant cycle
US3135088A (en) * 1961-03-02 1964-06-02 United Aircraft Corp Sequencing system
US3410092A (en) * 1961-07-17 1968-11-12 Marquardt Corp Reliquefaction cycle for liquid air cycle engine
US3200583A (en) * 1962-10-15 1965-08-17 Gen Motors Corp Rocket propulsion apparatus
DE1751962C2 (de) * 1968-08-24 1974-07-04 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Raketenbrennkammer für flüssige, mittels Strahlpumpen geförderte Treibstoffe, insbesondere für hypergole Treibstoffe
DE1776010A1 (de) * 1968-09-03 1971-09-16 Messerschmitt Boelkow Blohm Verfahren zum Foerdern von fluessigen Treibstoffen fuer Gaserzeuger bzw.Raketenbrennkammern,und Foerdersystem zur Durchfuehrung des Verfahrens
US3707074A (en) * 1970-09-30 1972-12-26 Westinghouse Electric Corp Spontaneous ignition of fuel in a combustion chamber
US3861141A (en) * 1971-08-17 1975-01-21 Brown Engineering Company Inc Fuel pressurization for momentum compression ramjet engine
GB2191821B (en) * 1978-12-07 1988-05-25 Rolls Royce Fuel preheater for an integrated rocket/ramjet engine
GB2119447A (en) * 1982-05-01 1983-11-16 Kershaw H A Vapourising systems in jet propulsion or gas turbine engines
US5551230A (en) * 1994-03-14 1996-09-03 Rockwell International Corporation Heat induced high pressure lox pump rocket engine cycle
FR2921979B1 (fr) * 2007-10-08 2014-06-13 Astrium Sas Dispositif et procede de motorisation de pompe pour moteur fusee par moteur a combustion interne
US8844293B2 (en) * 2011-03-22 2014-09-30 Pratt & Whitney Canada Corp. Fuel system for gas turbine engine
US20170356304A1 (en) * 2016-06-13 2017-12-14 General Electric Company Systems and methods for reducing fluid viscosity in a gas turbine engine
US10718294B1 (en) * 2017-10-27 2020-07-21 United Launch Alliance, L.L.C. Integrated vehicle fluids
US12428166B2 (en) * 2022-12-23 2025-09-30 Hamilton Sundstrand Corporation Cooling architecture using cryogenic fuels

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB191003407A (en) * 1910-02-11 1910-10-27 James Alexander Main Improvements in the Generation of Gases and Products of Combustion under Pressure for Operating Motive Power Engines.
US2395403A (en) * 1939-03-06 1946-02-26 Daniel And Florence Guggenheim Rotatable combustion apparatus for aircraft
US2558483A (en) * 1944-05-20 1951-06-26 Daniel And Florence Guggenheim Feeding apparatus, including injectors adapted to supply combustion liquids under pressure to a combustion chamber
US2612752A (en) * 1944-05-20 1952-10-07 Daniel And Florence Guggenheim Feeding apparatus, including injectors adapted to supply combustion liquids under pressure to a combustion chamber
US2505798A (en) * 1946-06-20 1950-05-02 Leslie A Skinner Liquid fuel jet propulsion system

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2323884A1 (fr) * 1975-09-12 1977-04-08 Rolls Royce Circuit de carburant pour turbomachines
FR2728627A1 (fr) * 1994-12-27 1996-06-28 Europ Propulsion Autopressurisation de reservoir
EP0719935A1 (fr) * 1994-12-27 1996-07-03 Societe Europeenne De Propulsion Autopressurisation de réservoir
US5697212A (en) * 1994-12-27 1997-12-16 Societe Europeenne De Propulsion Rocket propellant tank self-pressurization

Also Published As

Publication number Publication date
US2704438A (en) 1955-03-22
GB704622A (en) 1954-02-24

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