DE3768156D1 - Fluessigtreibstoffraketenmotor. - Google Patents

Fluessigtreibstoffraketenmotor.

Info

Publication number: DE3768156D1
Authority: DE; Germany
Prior art keywords: liquid fuel; rocket engine; fuel rocket; engine; liquid
Prior art date: 1986-05-07
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

DE8787106661T

Other languages

English (en)

Inventor

Yukio C O Nat Space Dev Koyari

Eiji C O Nat Space Deve Sogame

Kenji C O Nagoya Air Kishimoto

Yojiro C O Nagoya Aircr Kakuma

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.)

National Space Development Agency of Japan

Mitsubishi Heavy Industries Ltd

Original Assignee

NATIONAL SPACE DEVELOPMENT TOKIO/TOKYO JP

NAT SPACE DEV

Mitsubishi Heavy Industries Ltd

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.)

1986-05-07

Filing date

1987-05-07

Publication date

1991-04-04

Family has litigation

First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=14381752&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE3768156(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.

1987-05-07 Application filed by NATIONAL SPACE DEVELOPMENT TOKIO/TOKYO JP, NAT SPACE DEV, Mitsubishi Heavy Industries Ltd filed Critical NATIONAL SPACE DEVELOPMENT TOKIO/TOKYO JP

1991-04-04 Application granted granted Critical

1991-04-04 Publication of DE3768156D1 publication Critical patent/DE3768156D1/de

2007-05-08 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
- F02K9/44—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
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
- F02K9/64—Combustion or thrust chambers having cooling arrangements

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Engine Equipment That Uses Special Cycles (AREA)
Jet Pumps And Other Pumps (AREA)

DE8787106661T 1986-05-07 1987-05-07 Fluessigtreibstoffraketenmotor. Expired - Lifetime DE3768156D1 (de)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
JP61104481A JPS62261652A (ja)	1986-05-07	1986-05-07	液体ロケツトエンジン

Publications (1)

Publication Number	Publication Date
DE3768156D1 true DE3768156D1 (de)	1991-04-04

Family

ID=14381752

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
DE8787106661T Expired - Lifetime DE3768156D1 (de)	1986-05-07	1987-05-07	Fluessigtreibstoffraketenmotor.

Country Status (5)

Country	Link
US (1)	US4879874A (de)
EP (1)	EP0252238B1 (de)
JP (1)	JPS62261652A (de)
CN (1)	CN87103346A (de)
DE (1)	DE3768156D1 (de)

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US5873241A (en) *	1991-05-23	1999-02-23	United Technologies Corporation	Rocket engine auxiliary power system
US5267437A (en) *	1991-05-23	1993-12-07	United Technologies Corporation	Dual mode rocket engine
US5207399A (en) *	1992-03-20	1993-05-04	General Dynamics Corporation, Space Systems Division	Vapor pressurization system for outer space
US5444973A (en) *	1993-12-13	1995-08-29	United Technologies Corporation	Pressure-fed rocket booster system
DE19505357C1 (de) *	1995-02-17	1996-05-23	Daimler Benz Aerospace Ag	Verfahren zur Kühlung von Triebwerkswänden und Wandstruktur zur Durchführung desselben
ATE386203T1 (de)	1999-03-10	2008-03-15	Williams Int Co Llc	Raketenmotor
SE516046C2 (sv) *	2000-03-17	2001-11-12	Volvo Aero Corp	Anordning för styrning av värmeöverföringen till munstycksväggen hos raketmotorer av expandertyp
US6832471B2 (en) *	2003-03-12	2004-12-21	Aerojet-General Corporation	Expander cycle rocket engine with staged combustion and heat exchange
RU2333869C2 (ru) *	2003-03-28	2008-09-20	Моуджейв Аэроспейс Венчерз, Ллс	Унифицированная комбинированная ракетная система
US6918243B2 (en) *	2003-05-19	2005-07-19	The Boeing Company	Bi-propellant injector with flame-holding zone igniter
US7389636B2 (en) *	2005-07-06	2008-06-24	United Technologies Corporation	Booster rocket engine using gaseous hydrocarbon in catalytically enhanced gas generator cycle
US8122703B2 (en)	2006-04-28	2012-02-28	United Technologies Corporation	Coaxial ignition assembly
KR100674118B1 (ko) *	2006-07-07	2007-01-24	(주)씨앤스페이스	로켓 추진용 메탄엔진
US20100326043A1 (en) *	2007-01-31	2010-12-30	Florida Turbine Technologies, Inc.	Expander cycle rocket engine nozzle
WO2008100186A1 (en) *	2007-02-13	2008-08-21	Volvo Aero Corporation	A component configured for being subjected to high thermal load during operation
US20080264035A1 (en) *	2007-04-25	2008-10-30	Ricciardo Mark J	Coolant flow swirler for a rocket engine
FR2937092B1 (fr) *	2008-10-15	2010-12-10	Snecma	Procede et dispositif de calcul d'une sequence de demarrage ou d'arret d'un moteur.
WO2010068636A2 (en) *	2008-12-08	2010-06-17	Firestar Engineering, Llc	Regeneratively cooled porous media jacket
US20110005195A1 (en)	2009-07-07	2011-01-13	Firestar Engineering, Llc	Aluminum porous media
RU2481489C1 (ru) *	2012-03-05	2013-05-10	Николай Борисович Болотин	Турбонасосный агрегат ракетного двигателя
RU2495273C1 (ru) *	2012-05-04	2013-10-10	Николай Борисович Болотин	Жидкостный ракетный двигатель
RU2506444C1 (ru) *	2012-05-22	2014-02-10	Александр Фролович Ефимочкин	Жидкостный ракетный двигатель
FR2991392B1 (fr) *	2012-06-01	2016-01-15	Snecma	Turbopompe
FR2992364B1 (fr) *	2012-06-25	2014-07-25	Snecma	Turbopompe
RU2514466C1 (ru) *	2013-01-22	2014-04-27	Открытое акционерное общество "Конструкторское бюро химавтоматики"	Жидкостный ракетный двигатель
JP6000159B2 (ja) *	2013-02-19	2016-09-28	三菱重工業株式会社	ロケットエンジン
WO2014144369A1 (en) *	2013-03-15	2014-09-18	Orbital Sciences Corporation	Hybrid-cycle liquid propellant rocket engine
RU2514582C1 (ru) *	2013-06-18	2014-04-27	Николай Борисович Болотин	Жидкостный ракетный двигатель
RU2531831C1 (ru) *	2013-06-18	2014-10-27	Николай Борисович Болотин	Жидкостный ракетный двигатель
RU2531835C1 (ru) *	2013-07-02	2014-10-27	Николай Борисович Болотин	Жидкостный ракетный двигатель
JP2015039925A (ja) *	2013-08-21	2015-03-02	株式会社Ｉｈｉエアロスペース	スラスタ用熱エネルギ回収装置
CN103629013B (zh) *	2013-11-27	2016-01-13	中国科学院力学研究所	一种亚声速燃烧冲压发动机燃烧室及其再生冷却方法
RU2544684C1 (ru) *	2014-01-09	2015-03-20	Открытое акционерное общество "Конструкторское бюро химавтоматики"	Жидкостный ракетный двигатель
RU2562315C1 (ru) *	2014-08-05	2015-09-10	Николай Борисович Болотин	Трехкомпонентный жидкостный ракетный двигатель
US10072612B2 (en) *	2015-10-05	2018-09-11	Vector Launch Inc.	Enhanced liquid oxygen-propylene rocket engine
RU2612512C1 (ru) *	2016-03-29	2017-03-09	Владислав Юрьевич Климов	Жидкостный ракетный двигатель
CN106640424A (zh) *	2016-10-26	2017-05-10	湖北航天技术研究院总体设计所	一种液体火箭发动机燃烧室
CN106555707A (zh) *	2016-11-30	2017-04-05	西北工业大学	电驱推进剂供给系统液体火箭发动机
CN108412637B (zh) *	2018-03-16	2020-04-10	北京航天动力研究所	一种新型氢氧火箭发动机系统
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
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
CN108825380B (zh) *	2018-05-28	2020-05-19	华中科技大学	一种涡轴发动机
CN109322765B (zh) *	2018-07-31	2019-09-20	李鹏	基于改进膨胀偏转喷管的大推力闭式膨胀循环火箭发动机
CN109184956B (zh) *	2018-09-21	2024-04-09	同济大学	一种高压气态氢氧喷气式发动机装置
CN111794878A (zh) *	2020-08-06	2020-10-20	北京环境特性研究所	一种火箭发动机冷却与隐身设计装置
CN112594093B (zh) *	2020-12-04	2022-05-27	北京航空航天大学	用于固液火箭发动机的往复式容积泵的控制系统
CN112746912B (zh) *	2021-01-18	2022-05-13	天津大学	可液气分离的液体火箭发动机多层主动冷却装置
CN113404621B (zh) *	2021-06-19	2022-08-16	西北工业大学	火星上升飞行器用固液混合发动机及方法
US11598290B2 (en) *	2021-07-02	2023-03-07	Korea Aerospace Research Institute	Combustor of liquid rocket engine
KR102686396B1 (ko) *	2021-07-02	2024-07-19	한국항공우주연구원	액체로켓엔진의 연소기
US12180914B1 (en) *	2023-08-28	2024-12-31	Pivotal Space, Inc.	Boost injection turbine exhaust cycle (BITEC)

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* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3077073A (en) *	1957-10-29	1963-02-12	United Aircraft Corp	Rocket engine having fuel driven propellant pumps
US3024606A (en) *	1958-07-10	1962-03-13	Curtiss Wright Corp	Liquid cooling system for jet engines
US3613375A (en) *	1961-06-05	1971-10-19	United Aircraft Corp	Rocket engine propellant feeding and control system
US3168807A (en) *	1961-08-08	1965-02-09	United Aircraft Corp	Nuclear rocket flow control
US3516254A (en) *	1967-09-11	1970-06-23	United Aircraft Corp	Closed-loop rocket propellant cycle
US3605412A (en) *	1968-07-09	1971-09-20	Bolkow Gmbh	Fluid cooled thrust nozzle for a rocket
DE1950407B2 (de) *	1969-10-07	1972-03-30	Maschinenfabnk Augsburg Nürnberg AG, 8000 München	Treibstoffversorgungssystem fuer ein raketentriebwerk
US3713293A (en) *	1970-10-08	1973-01-30	Maschf Augsburg Nuernberg Ag	Combustion chamber and nozzle arrangement for a rocket engine
US4107919A (en) *	1975-03-19	1978-08-22	The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration	Heat exchanger
DE2743983C2 (de) *	1977-09-30	1982-11-11	Messerschmitt-Bölkow-Blohm GmbH, 8000 München	Flüssigkeitsraketentriebwerk in Nebenstrombauart für den Betrieb im luftleeren Raum
DE3228162A1 (de) *	1982-07-28	1984-02-09	Messerschmitt-Bölkow-Blohm GmbH, 8000 München	Fluessigkeitsraketentriebwerk in nebenstrombauart fuer den betrieb im luftleeren raum

1986
- 1986-05-07 JP JP61104481A patent/JPS62261652A/ja active Granted
1987
- 1987-05-07 CN CN198787103346A patent/CN87103346A/zh not_active Withdrawn
- 1987-05-07 DE DE8787106661T patent/DE3768156D1/de not_active Expired - Lifetime
- 1987-05-07 EP EP87106661A patent/EP0252238B1/de not_active Expired
1988
- 1988-04-18 US US07/182,938 patent/US4879874A/en not_active Expired - Lifetime

Also Published As

Publication number	Publication date
JPH0532579B2 (de)	1993-05-17
CN87103346A (zh)	1987-11-25
EP0252238A1 (de)	1988-01-13
US4879874A (en)	1989-11-14
EP0252238B1 (de)	1991-02-27
JPS62261652A (ja)	1987-11-13

Publication	Publication Date	Title
DE3768156D1 (de)	1991-04-04	Fluessigtreibstoffraketenmotor.
DE3786416D1 (de)	1993-08-12	Kraftstoffeinspritzsystem.
DE3763745D1 (de)	1990-08-23	Brennstoffpumpe.
IT8720527A0 (it)	1987-05-14	Riscaldatore per carburante diesel.
DE3761916D1 (de)	1990-04-19	Raketentriebwerke.
DE68900273D1 (de)	1991-10-24	Zweistoffraketenmotor.
DE3762877D1 (de)	1990-06-28	Kraftstoffgemisch.
FI834504L (fi)	1984-06-10	Dieselbraenslen.
IT8720553A0 (it)	1987-05-15	Iniettori di combustibile.
DE3774170D1 (de)	1991-12-05	Brennstoffleitung.
DE3765038D1 (de)	1990-10-25	Tankeinrichtung.
DE3788585D1 (de)	1994-02-10	Flüssige Brennstoffzusammensetzungen.
DE3863624D1 (de)	1991-08-14	Dickstoff-pumpe.
DE3782773D1 (de)	1993-01-07	Fluessige brennstoffzusammensetzungen.
DE3761841D1 (de)	1990-04-12	Kraftstoffverbindung.
DE3863801D1 (de)	1991-08-29	Kraftstoffpumpe.
ATE46743T1 (de)	1989-10-15	Brennkraftmaschine.
DE3669559D1 (de)	1990-04-19	Viertakt-brennkraftmaschine.
DE3772284D1 (de)	1991-09-26	Kraftstoffeinspritzpumpe.
DE3777454D1 (de)	1992-04-23	Brennstoff-einspritzvorrichtung.
IT8720551A0 (it)	1987-05-15	Iniettori di combustibile.
DE3580791D1 (de)	1991-01-17	Motor-kraftstoffe.
DE3765002D1 (de)	1990-10-25	Brennkammer fuer fluessigbrennstoff.
IT8720173A0 (it)	1987-04-17	Iniettore di combustibile per carburatore.
NL193286B (nl)	1999-01-04	Verbrandingsmotor.

Legal Events

Date	Code	Title	Description
1992-03-05	8363	Opposition against the patent
1993-11-11	8365	Fully valid after opposition proceedings
2003-04-30	8327	Change in the person/name/address of the patent owner	Owner name: MITSUBISHI JUKOGYO K.K., TOKIO/TOKYO, JP Owner name: NATIONAL SPACE DEVELOPMENT AGENCY, TSUKUBA, IBARAK

Date

Code

Title

Description

1992-03-05

8363

Opposition against the patent

1993-11-11

8365

Fully valid after opposition proceedings

2003-04-30

8327

Change in the person/name/address of the patent owner

Owner name: MITSUBISHI JUKOGYO K.K., TOKIO/TOKYO, JP

Owner name: NATIONAL SPACE DEVELOPMENT AGENCY, TSUKUBA, IBARAK