PL3597897T3 - Konstrukcja komory spalania, szczególnie dla silników rakietowych - Google Patents

Konstrukcja komory spalania, szczególnie dla silników rakietowych

Info

Publication number
PL3597897T3
PL3597897T3 PL18183912.7T PL18183912T PL3597897T3 PL 3597897 T3 PL3597897 T3 PL 3597897T3 PL 18183912 T PL18183912 T PL 18183912T PL 3597897 T3 PL3597897 T3 PL 3597897T3
Authority
PL
Poland
Prior art keywords
combustion chamber
rocket engine
chamber structure
rocket
engine
Prior art date
Application number
PL18183912.7T
Other languages
English (en)
Inventor
Andreas GÖTZ
Marc Geyer
Torben Birck
Olivier De Bonn
Original Assignee
Arianegroup Gmbh
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 Arianegroup Gmbh filed Critical Arianegroup Gmbh
Publication of PL3597897T3 publication Critical patent/PL3597897T3/pl

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
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements
    • 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
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
    • F05D2250/311—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being in line
    • 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
    • F05D2260/205—Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
PL18183912.7T 2018-07-17 2018-07-17 Konstrukcja komory spalania, szczególnie dla silników rakietowych PL3597897T3 (pl)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP18183912.7A EP3597897B1 (en) 2018-07-17 2018-07-17 Combustion chamber structure, particularly for a rocket engine

Publications (1)

Publication Number Publication Date
PL3597897T3 true PL3597897T3 (pl) 2024-06-24

Family

ID=62981071

Family Applications (1)

Application Number Title Priority Date Filing Date
PL18183912.7T PL3597897T3 (pl) 2018-07-17 2018-07-17 Konstrukcja komory spalania, szczególnie dla silników rakietowych

Country Status (5)

Country Link
US (1) US11525420B2 (pl)
EP (1) EP3597897B1 (pl)
JP (1) JP7383410B2 (pl)
ES (1) ES2972151T3 (pl)
PL (1) PL3597897T3 (pl)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021171988A1 (ja) * 2020-02-28 2021-09-02 株式会社Ihi ロケットエンジン用燃焼装置
KR102427107B1 (ko) * 2020-10-16 2022-07-29 한국항공우주연구원 극저온 연료와 액체 산소를 이용하는 로켓 엔진의 점화 장치 일체형 연소기 및 이를 포함하는 로켓
KR102434970B1 (ko) * 2020-10-20 2022-08-22 한국항공우주연구원 산화제 및 연료를 이용하는 로켓 엔진 연소기의 재생 냉각 추력실 및 이를 포함하는 로켓
KR102468746B1 (ko) 2020-11-18 2022-11-18 한국항공우주연구원 열교환 구조를 포함하는 연소기 및 이를 포함하는 로켓
KR102469946B1 (ko) * 2020-12-31 2022-11-23 한국항공우주연구원 연소기 헤드-터보펌프 일체형 로켓엔진
WO2024017865A1 (en) 2022-07-19 2024-01-25 Heliuspace B.V. Aerospace vehicle having a spike engine, and methods of operating and simulating thereof
CN115653789B (zh) * 2022-10-31 2024-08-13 上海空间推进研究所 液体火箭发动机再生冷却身部结构、制造方法及发动机
US12480460B1 (en) * 2024-05-21 2025-11-25 General Electric Company Composite tubular structure

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2540665A (en) * 1946-02-01 1951-02-06 Daniel And Florence Guggenheim Mechanism for coaxial feeding of two combustion liquids to a combustion chamber
US2526222A (en) * 1948-01-02 1950-10-17 Daniel And Florence Guggenheim Cooling and feeding means for rocket type combustion chambers
US2991617A (en) * 1950-12-01 1961-07-11 Gen Electric Jet motor combustion chamber
DE1118539B (de) * 1959-05-25 1961-11-30 United Aircraft Corp Raketenbrennkammer
US3170286A (en) * 1962-03-26 1965-02-23 Stein Samuel Injector-valve device
GB1089055A (en) * 1965-07-20 1967-11-01 Bristol Siddeley Engines Ltd Combined combustion chamber and propulsive unit for a rocket engine
US3460759A (en) * 1967-03-07 1969-08-12 Nasa Combustion chamber
JPH0713500B2 (ja) * 1984-08-29 1995-02-15 三菱重工業株式会社 ロケツトエンジン燃焼室製造方法
FR2669966B1 (fr) * 1990-11-30 1993-03-26 Europ Propulsion Procede de fabrication de paroi de chambre de combustion, notamment pour moteur-fusee, et chambre de combustion obtenue par ce procede.
DE19901422C2 (de) 1999-01-18 2000-11-16 Daimler Chrysler Ag Brennkammer-Kühlstruktur für ein Raketentriebwerk
DE10237381B4 (de) 2002-08-12 2005-06-23 Eads Space Transportation Gmbh Brennkammerstruktur und Verfahren zu deren Herstellung
US6802179B2 (en) * 2002-12-02 2004-10-12 Aerojet-General Corporation Nozzle with spiral internal cooling channels
US7997510B2 (en) * 2006-07-24 2011-08-16 Thomas Clayton Pavia Systems, methods and apparatus for propulsion
US20090293448A1 (en) * 2007-05-15 2009-12-03 James Robert Grote Simplified thrust chamber recirculating cooling system
JP5481978B2 (ja) * 2009-07-10 2014-04-23 株式会社Ｉｈｉ ロケットエンジン
EP3507558A4 (en) 2016-09-01 2020-04-22 Additive Rocket Corporation STRUCTURAL HEAT EXCHANGER

Also Published As

Publication number Publication date
NZ755150A (en) 2021-09-24
US20200088138A1 (en) 2020-03-19
US11525420B2 (en) 2022-12-13
EP3597897A1 (en) 2020-01-22
ES2972151T3 (es) 2024-06-11
JP2020033994A (ja) 2020-03-05
JP7383410B2 (ja) 2023-11-20
EP3597897B1 (en) 2024-01-31

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