FR3101676B1 - Ensemble propulsif pour fusée - Google Patents

Ensemble propulsif pour fusée Download PDF

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Publication number
FR3101676B1
FR3101676B1 FR1911131A FR1911131A FR3101676B1 FR 3101676 B1 FR3101676 B1 FR 3101676B1 FR 1911131 A FR1911131 A FR 1911131A FR 1911131 A FR1911131 A FR 1911131A FR 3101676 B1 FR3101676 B1 FR 3101676B1
Authority
FR
France
Prior art keywords
combustion chamber
propellant
fuel tank
rocket
rocket propulsion
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.)
Active
Application number
FR1911131A
Other languages
English (en)
Other versions
FR3101676A1 (fr
Inventor
Nathalie Girard
Emilie Labarthe
Christophe Bonnal
Frédéric Masson
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.)
Centre National dEtudes Spatiales CNES
Original Assignee
Centre National dEtudes Spatiales CNES
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 Centre National dEtudes Spatiales CNES filed Critical Centre National dEtudes Spatiales CNES
Priority to FR1911131A priority Critical patent/FR3101676B1/fr
Priority to EP20793749.1A priority patent/EP4042009A1/fr
Priority to PCT/FR2020/051713 priority patent/WO2021069814A1/fr
Priority to CN202080071109.8A priority patent/CN114514371A/zh
Publication of FR3101676A1 publication Critical patent/FR3101676A1/fr
Application granted granted Critical
Publication of FR3101676B1 publication Critical patent/FR3101676B1/fr
Priority to US17/715,416 priority patent/US20220228542A1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • F02K9/42—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
    • 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
    • F02K9/50—Feeding propellants using pressurised fluid to pressurise the propellants
    • 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
    • F02K9/56—Control
    • 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
    • F02K9/56—Control
    • F02K9/566—Control elements and safety devices, e.g. pressure relief valves
    • 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
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/605—Reservoirs
    • 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
    • F02K9/97—Rocket nozzles
    • F02K9/972—Fluid cooling arrangements for nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/213—Heat transfer, e.g. cooling by the provision of a heat exchanger within the cooling circuit
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/301—Pressure

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Testing Of Engines (AREA)
  • Exhaust-Gas Circulating Devices (AREA)

Abstract

Ensemble propulsif pour fusée Contenu de l’abrégé. L’invention se rapporte à un ensemble propulsif (1) pour fusée comprenant un réservoir (2) conçu pour contenir un ergol, un moteur comprenant une chambre de combustion (3) configurée pour faire subir à l’ergol une combustion générant des gaz d’échappement, un circuit d’alimentation (4) disposé entre le réservoir (2) d’ergol et la chambre de combustion (3) configuré pour alimenter la chambre de combustion (3) en ergol et un circuit de gaz d’échappement (8) disposée entre la chambre de combustion (3) et le réservoir (2) d’ergol configuré pour acheminer au moins une partie des gaz d’échappement depuis la chambre de combustion (3) vers le réservoir (2) d’ergol en vue d’en assurer sa pressurisation. Figure pour l’abrégé : Fig. 1.
FR1911131A 2019-10-08 2019-10-08 Ensemble propulsif pour fusée Active FR3101676B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1911131A FR3101676B1 (fr) 2019-10-08 2019-10-08 Ensemble propulsif pour fusée
EP20793749.1A EP4042009A1 (fr) 2019-10-08 2020-09-30 Ensemble propulsif pour fusee
PCT/FR2020/051713 WO2021069814A1 (fr) 2019-10-08 2020-09-30 Ensemble propulsif pour fusee
CN202080071109.8A CN114514371A (zh) 2019-10-08 2020-09-30 用于火箭的推进组件
US17/715,416 US20220228542A1 (en) 2019-10-08 2022-04-07 Propulsion assembly for a rocket

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1911131A FR3101676B1 (fr) 2019-10-08 2019-10-08 Ensemble propulsif pour fusée
FR1911131 2019-10-08

Publications (2)

Publication Number Publication Date
FR3101676A1 FR3101676A1 (fr) 2021-04-09
FR3101676B1 true FR3101676B1 (fr) 2021-10-15

Family

ID=69104738

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1911131A Active FR3101676B1 (fr) 2019-10-08 2019-10-08 Ensemble propulsif pour fusée

Country Status (5)

Country Link
US (1) US20220228542A1 (fr)
EP (1) EP4042009A1 (fr)
CN (1) CN114514371A (fr)
FR (1) FR3101676B1 (fr)
WO (1) WO2021069814A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115898699B (zh) * 2022-10-21 2023-10-27 北京航天试验技术研究所 一种低温推进剂回温抽空装置

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2408111A (en) * 1943-08-30 1946-09-24 Robert C Truax Two-stage rocket system
US2683963A (en) * 1947-08-05 1954-07-20 Edward F Chandler Reaction engine with automatic pressure regulation
GB2025532B (en) * 1978-07-13 1983-06-15 Sperry Rand Ltd Fuelsystems for gas generators
US5901557A (en) * 1996-10-04 1999-05-11 Mcdonnell Douglas Corporation Passive low gravity cryogenic storage vessel
US6047541A (en) * 1998-08-26 2000-04-11 The United States Of America As Represented By The Secretary Of The Air Force HAN TEAN (xm-46) mixing gas generator propellant tank pressurizer for launch vehicles and spacecraft
US20090288390A1 (en) * 2008-05-23 2009-11-26 Thomas Clayton Pavia Simplified thrust chamber recirculating cooling system
FR2975441B1 (fr) * 2011-05-16 2016-02-12 Snecma Dispositif et procede de re-pressurisation
US9816897B2 (en) * 2012-06-06 2017-11-14 Harris Corporation Wireless engine monitoring system and associated engine wireless sensor network
FR2998926B1 (fr) * 2012-11-30 2014-12-26 Snecma Ensemble propulsif pour fusee
FR3009587B1 (fr) * 2013-08-06 2015-08-28 Snecma Dispositif de pressurisation de reservoirs d'ergol d'un moteur de fusee
FR3009585A1 (fr) * 2013-08-06 2015-02-13 Snecma Dispositif de pressurisation d'un reservoir d'ergol d'un moteur de fusee
US9777698B2 (en) * 2013-11-12 2017-10-03 Daniel Keith Schlak Multiple motor gas turbine engine system with auxiliary gas utilization
US9656756B2 (en) * 2014-03-10 2017-05-23 The Boeing Company Turbo-compressor system and method for extracting energy from an aircraft engine
US9989014B2 (en) * 2014-03-28 2018-06-05 The Boeing Company Premixed liquid propellant propulsion system and method with anti-flashback quenching liquid injector
US10100748B2 (en) * 2014-09-15 2018-10-16 The Boeing Company Dual fuel gas turbine thrust and power control
US9650996B2 (en) * 2015-03-13 2017-05-16 The Boeing Company Valve controller for pressure stabilization

Also Published As

Publication number Publication date
EP4042009A1 (fr) 2022-08-17
WO2021069814A1 (fr) 2021-04-15
FR3101676A1 (fr) 2021-04-09
US20220228542A1 (en) 2022-07-21
CN114514371A (zh) 2022-05-17

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