DE3860224D1 - Raketenbrennkammer. - Google Patents

Raketenbrennkammer.

Info

Publication number: DE3860224D1
Authority: DE; Germany
Prior art keywords: combustion chamber; rocket combustion; rocket; chamber; combustion
Prior art date: 1987-03-26
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 - Lifetime

Application number

DE8888302661T

Other languages

English (en)

Inventor

Ryo Horiuchi

Satoshi Saito

Koichi Suzuki

Kazuyuki Higashino

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.)

INST SPASE ASTRONAUTIC SCIENCE

IHI Corp

Original Assignee

Ishikawajima Harima Heavy Industries Co Ltd

INST SPASE ASTRONAUTIC SCIENCE

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.)

1987-03-26

Filing date

1988-03-25

Publication date

1990-07-19

1988-03-25 Application filed by Ishikawajima Harima Heavy Industries Co Ltd, INST SPASE ASTRONAUTIC SCIENCE filed Critical Ishikawajima Harima Heavy Industries Co Ltd

1990-07-19 Application granted granted Critical

1990-07-19 Publication of DE3860224D1 publication Critical patent/DE3860224D1/de

2008-03-26 Anticipated expiration legal-status Critical

Status Expired - Lifetime legal-status Critical Current

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
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49346—Rocket or jet device making

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Pressure Welding/Diffusion-Bonding (AREA)

DE8888302661T 1987-03-26 1988-03-25 Raketenbrennkammer. Expired - Lifetime DE3860224D1 (de)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
JP62070230A JPH0659502B2 (ja)	1987-03-26	1987-03-26	ロケット用高圧燃焼器の燃焼室及びその製造方法

Publications (1)

Publication Number	Publication Date
DE3860224D1 true DE3860224D1 (de)	1990-07-19

Family

ID=13425551

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
DE8888302661T Expired - Lifetime DE3860224D1 (de)	1987-03-26	1988-03-25	Raketenbrennkammer.

Country Status (4)

Country	Link
US (2)	US4856163A (de)
EP (1)	EP0284410B1 (de)
JP (1)	JPH0659502B2 (de)
DE (1)	DE3860224D1 (de)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US5048289A (en) *	1989-06-15	1991-09-17	Rockwell International Corporation	Extendible nozzle
US4942653A (en) *	1989-08-25	1990-07-24	Rockwell International Corporation	Production method for a channeled wall thrust nozzle
US5102296A (en) *	1989-09-07	1992-04-07	Ingersoll-Rand Company	Turbine nozzle, and a method of varying the power of same
DE4015204C1 (de) *	1990-05-11	1991-10-17	Mtu Muenchen Gmbh
US5075966A (en) *	1990-09-04	1991-12-31	General Electric Company	Method for fabricating a hollow component for a rocket engine
DE4115403A1 (de) *	1991-05-10	1992-11-12	Mtu Muenchen Gmbh	Duesenwand
KR950007640B1 (ko) *	1992-06-20	1995-07-13	국방과학연구소	로켓트 추진기관의 조립방법
US5249357A (en) *	1993-01-27	1993-10-05	The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration	Method of fabricating a rocket engine combustion chamber
US5363654A (en) *	1993-05-10	1994-11-15	General Electric Company	Recuperative impingement cooling of jet engine components
DE4321393C2 (de) *	1993-06-26	1996-08-22	Daimler Benz Aerospace Ag	Wandstruktur, insbesondere für ein Staustrahltriebwerk
US5444912A (en) *	1993-10-29	1995-08-29	Folmer; Carroll W.	Method for forming aircraft engine nacelle exhaust mixers and similar products
JPH08270950A (ja) *	1995-02-01	1996-10-18	Mitsubishi Heavy Ind Ltd	ガスタービン燃焼器
FR2733581B1 (fr) *	1995-04-27	1997-07-18	Europ Propulsion	Enceinte de combustion avec refroidissement par transpiration
US5680767A (en) *	1995-09-11	1997-10-28	General Electric Company	Regenerative combustor cooling in a gas turbine engine
US7234294B1 (en)	2001-01-11	2007-06-26	Volvo Aero Corporation	Outlet nozzle and a method for manufacturing an outlet nozzle
WO2002055860A1 (en) *	2001-01-11	2002-07-18	Volvo Aero Corporation	An outlet nozzle and a method for manufacturing an outlet nozzle
US7188417B2 (en) *	2002-06-28	2007-03-13	United Technologies Corporation	Advanced L-channel welded nozzle design
FR2850741B1 (fr) *	2003-01-30	2005-09-23	Snecma Propulsion Solide	Procede de fabrication d'un panneau de refroidissement actif en materiau composite thermostructural
KR100717376B1 (ko)	2004-12-29	2007-05-10	한국항공우주연구원	고압액체로켓엔진용 재생냉각 연소실
RU2526998C2 (ru) *	2012-11-30	2014-08-27	Открытое акционерное общество "Конструкторское бюро химавтоматики"	Способ установки геометрической оси камеры жрд и компенсирующее замыкающее устройство для его реализации
KR101931023B1 (ko) *	2017-09-04	2019-03-11	주식회사 한화	가압형 라이너 주입장치 및 방법
CN112253334B (zh) *	2020-09-29	2021-10-19	西安航天动力研究所	一种集成冷却通道的燃气管路

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE1019865B (de) *	1940-03-09	1957-11-21	Bayerische Motoren Werke Ag	Kuehleinrichtung fuer Raketenmotoren
US2968918A (en) *	1949-08-22	1961-01-24	California Inst Res Found	Rocket motor shell construction
GB759901A (en) *	1951-12-06	1956-10-24	Armstrong Siddeley Motors Ltd	Combustion chambers
US2900168A (en) *	1955-03-24	1959-08-18	Meredith M Nyborg	Reaction motor with liquid cooling means
US3057148A (en) *	1956-10-01	1962-10-09	Aerojet General Co	Means to improve adherence of lining materials to the inner surface of combustion chambers of rocket motors
US3154914A (en) *	1959-12-12	1964-11-03	Bolkow Entwicklungen Kg	Rocket engine construction
US3249989A (en) *	1962-03-13	1966-05-10	Thiokol Chemical Corp	Method of making a sheet metal thrust chamber
US3224678A (en) *	1962-10-04	1965-12-21	Marquardt Corp	Modular thrust chamber
US3605412A (en) *	1968-07-09	1971-09-20	Bolkow Gmbh	Fluid cooled thrust nozzle for a rocket
FR2012723A1 (de) *	1968-07-11	1970-03-20	Messerschmitt Boelkow Blohm
US3630449A (en) *	1970-05-11	1971-12-28	Us Air Force	Nozzle for rocket engine
JPS58214652A (ja) *	1982-06-08	1983-12-13	Natl Aerospace Lab	複合冷却ロケツト燃焼器
JPS6082602A (ja) *	1983-10-07	1985-05-10	Natl Aerospace Lab	ロケツト燃焼器外筒製作法

1987
- 1987-03-26 JP JP62070230A patent/JPH0659502B2/ja not_active Expired - Lifetime
1988
- 1988-03-22 US US07/171,856 patent/US4856163A/en not_active Expired - Lifetime
- 1988-03-25 DE DE8888302661T patent/DE3860224D1/de not_active Expired - Lifetime
- 1988-03-25 EP EP88302661A patent/EP0284410B1/de not_active Expired - Lifetime
1989
- 1989-04-13 US US07/337,551 patent/US4909032A/en not_active Expired - Lifetime

Also Published As

Publication number	Publication date
EP0284410A1 (de)	1988-09-28
US4856163A (en)	1989-08-15
JPS63238923A (ja)	1988-10-05
US4909032A (en)	1990-03-20
EP0284410B1 (de)	1990-06-13
JPH0659502B2 (ja)	1994-08-10

Publication	Publication Date	Title
DE3672389D1 (de)	1990-08-09	Brennkammerwandstruktur.
DE59000422D1 (de)	1992-12-10	Brennkammeranordnung.
DE3860224D1 (de)	1990-07-19	Raketenbrennkammer.
DE68900218D1 (de)	1991-09-26	Teilverbrennungsbrenner.
DE3854174D1 (de)	1995-08-24	Kraftstoffeinspritzventil.
DE3866137D1 (de)	1991-12-19	Sonnenbetriebener stirling-motor.
IT8820431A0 (it)	1988-05-03	Camera di combustione.
DE3761916D1 (de)	1990-04-19	Raketentriebwerke.
DE68900273D1 (de)	1991-10-24	Zweistoffraketenmotor.
DE68903944D1 (de)	1993-01-28	Raketenwerfer.
DE3868887D1 (de)	1992-04-09	Isolierte brennkraftmaschine.
DK161479C (da)	1991-12-16	Forbraendingskammer
DE3866977D1 (de)	1992-01-30	Mehrstufenfeststoffrakete.
DE3860912D1 (de)	1990-12-06	Einspritzbrennkraftmaschine.
DE69002215D1 (de)	1993-08-19	Raketenbrennkammer.
ES2023489B3 (es)	1992-01-16	Bomba de combustible.
DE3868100D1 (de)	1992-03-12	Brennstoffanordnung.
DE3886126D1 (de)	1994-01-20	Brennstoffeinspritzventil.
DE3881383D1 (de)	1993-07-01	Waermekraftmaschine.
DE3667729D1 (de)	1990-01-25	Geschosszuender.
NO158898C (no)	1988-11-09	Prosjektil.
NO881083D0 (no)	1988-03-11	Prosjektil med sprengladning.
DE3873184D1 (de)	1992-09-03	Waermeisolierter brennkraftmaschinenaufbau.
DE3861291D1 (de)	1991-01-31	Gasbeheiztes verbrennungsgeraet.
DE59101352D1 (de)	1994-05-19	Raketenmotor.

Legal Events

Date	Code	Title	Description
1991-07-11	8364	No opposition during term of opposition