SG11201505502QA - Starter device for rocket motor turbopump - Google Patents

Starter device for rocket motor turbopump

Info

Publication number
SG11201505502QA
SG11201505502QA SG11201505502QA SG11201505502QA SG11201505502QA SG 11201505502Q A SG11201505502Q A SG 11201505502QA SG 11201505502Q A SG11201505502Q A SG 11201505502QA SG 11201505502Q A SG11201505502Q A SG 11201505502QA SG 11201505502Q A SG11201505502Q A SG 11201505502QA
Authority
SG
Singapore
Prior art keywords
turbopump
rocket motor
starter device
starter
rocket
Prior art date
Application number
SG11201505502QA
Other languages
English (en)
Inventor
Jean-Philippe Dutheil
Pierre Vinet
Original Assignee
Airbus Defence & Space Sas
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 Airbus Defence & Space Sas filed Critical Airbus Defence & Space Sas
Publication of SG11201505502QA publication Critical patent/SG11201505502QA/en

Links

Classifications

    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F02K9/46—Feeding propellants using pumps
    • 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
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/78—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with an air-breathing jet-propulsion plant
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • 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
    • F02C7/26—Starting; Ignition
    • 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
    • F02K9/46—Feeding propellants using pumps
    • F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
SG11201505502QA 2013-01-18 2014-01-16 Starter device for rocket motor turbopump SG11201505502QA (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1350456A FR3001260B1 (fr) 2013-01-18 2013-01-18 Dispositif de demarrage d'une turbopompe de moteur fusee
PCT/EP2014/050838 WO2014111485A1 (fr) 2013-01-18 2014-01-16 Dispositif de démarrage d'une turbopompe de moteur fusée

Publications (1)

Publication Number Publication Date
SG11201505502QA true SG11201505502QA (en) 2015-08-28

Family

ID=48289294

Family Applications (1)

Application Number Title Priority Date Filing Date
SG11201505502QA SG11201505502QA (en) 2013-01-18 2014-01-16 Starter device for rocket motor turbopump

Country Status (9)

Country Link
US (1) US20150354452A1 (fr)
EP (1) EP2946104B1 (fr)
JP (1) JP6280139B2 (fr)
CN (1) CN104919166B (fr)
BR (1) BR112015017150A2 (fr)
FR (1) FR3001260B1 (fr)
RU (1) RU2648480C2 (fr)
SG (1) SG11201505502QA (fr)
WO (1) WO2014111485A1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108590888A (zh) * 2018-03-27 2018-09-28 北京零壹空间科技有限公司 低温推进系统
CN108590887A (zh) * 2018-03-27 2018-09-28 北京零壹空间科技有限公司 基于蒸汽冷却屏的低温推进系统
US10479525B2 (en) 2018-04-03 2019-11-19 Kidde Technologies, Inc. Utilization of engine bleed air to provide extended duration emergency aircraft power
CN108839807B (zh) * 2018-05-14 2020-12-11 哈尔滨工业大学 一种新型的火星飞行器组合推进系统
CN109372655A (zh) * 2018-12-13 2019-02-22 西安航天动力研究所 高空低入口压力起动的气液并联驱动预增压系统及方法
CN109736953B (zh) * 2018-12-13 2020-02-28 西安航天动力研究所 气体驱动预压涡轮的多次起动液氧煤油发动机及起动方法
RU2742515C1 (ru) * 2019-12-29 2021-02-08 Андрей Владимирович Иванов Комбинированная силовая установка многоразовой первой ступени ракеты-носителя

Family Cites Families (21)

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Publication number Priority date Publication date Assignee Title
US2531761A (en) * 1944-12-02 1950-11-28 Aerojet Engineering Corp Thermal jet and rocket motor propulsion system
US2706888A (en) * 1949-03-10 1955-04-26 Rolls Royce Pump arrangements for gas-turbine engine fuel systems
US2745247A (en) * 1952-01-23 1956-05-15 Bell Aircraft Corp Rocket assisted composite engine arrangement
US2840986A (en) * 1952-04-29 1958-07-01 Rolls Royce After-burner fuel supply system for gas-turbine engines
FR1075034A (fr) * 1953-02-25 1954-10-12 Snecma Moteur à réaction combiné avec une fusée
US3269117A (en) * 1965-06-28 1966-08-30 John H Tweet Air driven turbopump
US4245462A (en) * 1978-11-29 1981-01-20 The Bendix Corporation Starting system for a turbine engine
US4404793A (en) * 1980-03-20 1983-09-20 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus for improving the fuel efficiency of a gas turbine engine
GB2240815B (en) * 1983-12-23 1991-12-18 Alan Bond Improvements in aerospace propulsion
DE3617757C1 (fr) * 1986-05-30 1987-07-02 Erno Raumfahrttechnik Gmbh, 2800 Bremen, De
GB2245029B (en) * 1988-03-23 1992-09-23 Rolls Royce Plc Improvements in or relating to aerospace propulsors
US5191761A (en) * 1988-09-16 1993-03-09 Janeke Charl E Aerospace plane and engine
FR2637017B1 (fr) * 1988-09-28 1990-11-30 Snecma Structure de tuyere pour propulseur combine turbo-stato-fusee
DE3909050C1 (fr) * 1989-03-18 1990-08-16 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
FR2656382B1 (fr) * 1989-12-21 1994-07-08 Europ Propulsion Moteur a propulsion combinee a haute adaptabilite pour aeronef ou avion spatial.
RU2106511C1 (ru) * 1992-12-30 1998-03-10 Ермишин Александр Викторович Ракетно-турбинный двигатель комбинированного типа
US6182435B1 (en) * 1997-06-05 2001-02-06 Hamilton Sundstrand Corporation Thermal and energy management method and apparatus for an aircraft
US6227486B1 (en) * 1999-05-28 2001-05-08 Mse Technology Applications, Inc. Propulsion system for earth to orbit vehicle
US7721524B2 (en) * 2006-02-15 2010-05-25 United Technologies Corporation Integrated airbreathing and non-airbreathing engine system
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
RU114343U1 (ru) * 2011-06-16 2012-03-20 Федеральное государственное военное образовательное учреждение высшего профессионального образования "Военная академия ракетных войск стратегического назначения имени Петра Великого" Министерства обороны Российской Федерации Комбинированный воздушно-ракетный двигатель с прямоточной камерой пульсирующего горения, форкамерой и системой воздушного запуска

Also Published As

Publication number Publication date
BR112015017150A2 (pt) 2017-07-11
WO2014111485A1 (fr) 2014-07-24
CN104919166A (zh) 2015-09-16
EP2946104B1 (fr) 2019-12-04
FR3001260A1 (fr) 2014-07-25
JP2016505106A (ja) 2016-02-18
FR3001260B1 (fr) 2017-04-21
CN104919166B (zh) 2017-07-04
RU2648480C2 (ru) 2018-03-26
EP2946104A1 (fr) 2015-11-25
RU2015134544A (ru) 2017-02-22
US20150354452A1 (en) 2015-12-10
JP6280139B2 (ja) 2018-02-14

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