DE1009927T1 - Staustrahltriebwerk mit ejektor - Google Patents

Staustrahltriebwerk mit ejektor

Info

Publication number
DE1009927T1
DE1009927T1 DE1009927T DE98938440T DE1009927T1 DE 1009927 T1 DE1009927 T1 DE 1009927T1 DE 1009927 T DE1009927 T DE 1009927T DE 98938440 T DE98938440 T DE 98938440T DE 1009927 T1 DE1009927 T1 DE 1009927T1
Authority
DE
Germany
Prior art keywords
ejector
jet engine
straight jet
straight
engine
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.)
Pending
Application number
DE1009927T
Other languages
English (en)
Inventor
J Boehnlein
G Bendot
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.)
Space Access LLC
Original Assignee
Space Access LLC
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 Space Access LLC filed Critical Space Access LLC
Publication of DE1009927T1 publication Critical patent/DE1009927T1/de
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
DE1009927T 1997-08-12 1998-08-07 Staustrahltriebwerk mit ejektor Pending DE1009927T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/909,509 US5946904A (en) 1997-08-12 1997-08-12 Ejector ramjet engine
PCT/US1998/016431 WO1999007988A1 (en) 1997-08-12 1998-08-07 Ejector ramjet engine

Publications (1)

Publication Number Publication Date
DE1009927T1 true DE1009927T1 (de) 2000-09-14

Family

ID=25427346

Family Applications (2)

Application Number Title Priority Date Filing Date
DE1009927T Pending DE1009927T1 (de) 1997-08-12 1998-08-07 Staustrahltriebwerk mit ejektor
DE69829385T Expired - Fee Related DE69829385T2 (de) 1997-08-12 1998-08-07 Staustrahltriebwerk mit ejektor

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE69829385T Expired - Fee Related DE69829385T2 (de) 1997-08-12 1998-08-07 Staustrahltriebwerk mit ejektor

Country Status (8)

Country Link
US (1) US5946904A (de)
EP (1) EP1009927B1 (de)
CN (1) CN1123687C (de)
AU (1) AU8696798A (de)
DE (2) DE1009927T1 (de)
RU (1) RU2195565C2 (de)
UA (1) UA57103C2 (de)
WO (1) WO1999007988A1 (de)

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US6457305B1 (en) * 2001-02-07 2002-10-01 James R. Schierbaum Turbo shaft engine with acoustical compression flow amplifying ramjet
US6564555B2 (en) 2001-05-24 2003-05-20 Allison Advanced Development Company Apparatus for forming a combustion mixture in a gas turbine engine
US6786040B2 (en) 2002-02-20 2004-09-07 Space Access, Llc Ejector based engines
US6948306B1 (en) * 2002-12-24 2005-09-27 The United States Of America As Represented By The Secretary Of The Navy Apparatus and method of using supersonic combustion heater for hypersonic materials and propulsion testing
US7320285B1 (en) * 2005-03-31 2008-01-22 The United States Of America As Represented By The Secretary Of The Navy Safe and arm device and method of using the same
US6857261B2 (en) * 2003-01-07 2005-02-22 Board Of Regents, The University Of Texas System Multi-mode pulsed detonation propulsion system
GB2404952B (en) * 2003-08-12 2006-08-30 Rolls Royce Plc Air breathing reaction propulsion engines
US20060213179A1 (en) * 2004-06-25 2006-09-28 Sanders Bobby W Subsonic diffuser
US7886516B2 (en) * 2006-12-18 2011-02-15 Aerojet-General Corporation Combined cycle integrated combustor and nozzle system
FR2924763B1 (fr) * 2007-12-06 2014-04-25 Snecma Systeme de tuyeres de moteur-fusee
US8381528B2 (en) 2007-12-21 2013-02-26 Grossi Aerospace, Inc. Ramjet superheater
CA2736412C (en) * 2008-09-09 2015-11-24 Dresser-Rand Company Supersonic ejector package
RU2519014C2 (ru) * 2010-03-02 2014-06-10 Дженерал Электрик Компани Диффузор для камеры сгорания турбины (варианты) и камера сгорания турбины
US8863525B2 (en) 2011-01-03 2014-10-21 General Electric Company Combustor with fuel staggering for flame holding mitigation
EP2644997A1 (de) * 2012-03-26 2013-10-02 Alstom Technology Ltd Mischanordnung zum Mischen von Kraftstoff mit einem Strom aus sauerstoffhaltigem Gas
CN102606564B (zh) * 2012-04-13 2013-10-02 中国人民解放军国防科学技术大学 超声速流道的实现方法和装置
CN102720587B (zh) * 2012-05-21 2014-06-04 中国科学院力学研究所 局部收缩比一致的变截面高超声速内转式进气道
CN102979623B (zh) * 2012-12-31 2015-03-04 中国人民解放军国防科学技术大学 超声速进气道及其壁面确定方法
CN103143461B (zh) * 2013-02-05 2015-09-16 中国人民解放军国防科学技术大学 滑块式变马赫数喷管及其壁面确定方法
CN105089851B (zh) * 2014-05-06 2016-11-16 中国航天科技集团公司第六研究院第十一研究所 可重复拆装推力室及该推力室推力向量精度的调节方法
CN104110326B (zh) * 2014-07-02 2016-06-29 北京航空航天大学 一种新概念高速飞行器推进系统布局方法
US10087884B2 (en) 2014-12-15 2018-10-02 United Technologies Corporation Stepped fairing modulated exhaust cooling
CN104595058A (zh) * 2015-01-05 2015-05-06 杜善骥 冲压火箭的工作方法
CN104727978A (zh) * 2015-01-06 2015-06-24 杜善骥 叠加冲压火箭工作方法
CN104963788B (zh) * 2015-07-03 2017-02-22 湖南华园科技有限公司 一种航空、航天、航海于一体的混合发动机
CN105156229A (zh) * 2015-09-29 2015-12-16 清华大学 一种液体喷射辅助式涡轮冲压组合循环发动机
CN105604735A (zh) * 2016-01-27 2016-05-25 吴畏 高超音速飞行器
CN106438108B (zh) * 2016-08-26 2018-10-12 南京理工大学 大调节比型固体火箭冲压发动机燃气流量调节装置
CN106801891B (zh) * 2017-01-20 2019-11-12 南京航空航天大学 一种用于高超能源系统的富燃和冲压组合燃气发生器
CN107725190B (zh) * 2017-09-26 2019-10-15 南京航空航天大学 一种可调边界燃烧的变几何超紧凑燃烧室
CN107762664A (zh) * 2017-11-20 2018-03-06 北京航天动力研究所 一种具有支撑和导流作用的喷嘴结构
CN109057993B (zh) * 2018-07-25 2019-12-31 湖南云顶智能科技有限公司 一种带电极冷却功能的等离子体喷雾燃烧装置
CN109252978A (zh) * 2018-08-31 2019-01-22 西安航天动力技术研究所 一种控制棒式变推力固体发动机
CN109915282B (zh) * 2019-04-04 2020-03-20 中国人民解放军国防科技大学 应用于火箭基组合循环发动机的自适应火箭喷管
DE102021000530A1 (de) 2021-02-03 2022-08-04 Mathias Hermann Antriebskonzept zum Start und Betrieb luftatmender Triebwerkssysteme (z.B. bei Ramjets) durch zusätzlich-variable Einbringung eines Oxidators
CN112945509B (zh) * 2021-04-22 2022-04-15 中国空气动力研究与发展中心超高速空气动力研究所 一种高超声速风洞扩压器收缩段的开口封堵装置
CN116537975B (zh) * 2023-07-06 2023-10-20 北京凌空天行科技有限责任公司 一种可回收飞行器喷流控制装置

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US2663142A (en) * 1951-12-20 1953-12-22 Wilson Walter Hobart Thermojet engine
US2995893A (en) * 1957-07-03 1961-08-15 Napier & Son Ltd Compound ramjet-turborocket engine
GB942044A (en) * 1961-04-28 1963-11-20 British Siddeley Engines Ltd Ramjet engine
US3367350A (en) * 1963-05-03 1968-02-06 Cadillac Gage Co Fluid ejector
US3143856A (en) * 1963-07-30 1964-08-11 United Aircraft Corp Directional control means for rockets or the like
US3323304A (en) * 1965-03-01 1967-06-06 Ljobet Andres Fraucisco Apparatus for producing high temperature gaseous stream
US3690102A (en) * 1970-10-29 1972-09-12 Anthony A Du Pont Ejector ram jet engine
US3812672A (en) * 1972-02-10 1974-05-28 Cci Aerospace Corp Supercharged ejector ramjet aircraft engine
US4030289A (en) * 1973-10-29 1977-06-21 Chandler Evans Inc. Thrust augmentation technique and apparatus
US3998050A (en) * 1974-01-07 1976-12-21 The United States Of America As Represented By The Secretary Of The Air Force Reverse flow aft inlet ramjet system
US4202172A (en) * 1976-03-01 1980-05-13 The Boeing Company Boost survivable ramjet elements
US4077572A (en) * 1976-03-25 1978-03-07 Chandler Evans Inc. Reduced size altitude insensitive thrust vector control nozzle
IL52613A (en) * 1977-07-28 1980-11-30 Univ Ramot Method and apparatus for controlling the mixing of two fluids
FR2629136B1 (fr) * 1985-09-17 1990-11-09 Aerospatiale Statoreacteur pourvu d'une pluralite de manches d'alimentation en air carbure et missile pourvu d'un tel statoreacteur
US4845941A (en) * 1986-11-07 1989-07-11 Paul Marius A Gas turbine engine operating process
US4807831A (en) * 1987-08-12 1989-02-28 The United States Of America As Represented By The Secretary Of The Air Force Combination boundary layer control system for high altitude aircraft
US4986495A (en) * 1988-06-15 1991-01-22 Rockwell International Corporation Cooling structure
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US5135184A (en) * 1990-08-22 1992-08-04 The Johns Hopkins University Propellant utilization system
US5205119A (en) * 1991-06-14 1993-04-27 Aerojet-General Corporation Ejector ramjet

Also Published As

Publication number Publication date
AU8696798A (en) 1999-03-01
EP1009927B1 (de) 2005-03-16
US5946904A (en) 1999-09-07
CN1283253A (zh) 2001-02-07
RU2195565C2 (ru) 2002-12-27
UA57103C2 (uk) 2003-06-16
WO1999007988A1 (en) 1999-02-18
EP1009927A1 (de) 2000-06-21
DE69829385T2 (de) 2006-04-13
DE69829385D1 (de) 2005-04-21
CN1123687C (zh) 2003-10-08
EP1009927A4 (de) 2003-06-11

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