DE3811614C1 - - Google Patents

Info

Publication number
DE3811614C1
DE3811614C1 DE3811614A DE3811614A DE3811614C1 DE 3811614 C1 DE3811614 C1 DE 3811614C1 DE 3811614 A DE3811614 A DE 3811614A DE 3811614 A DE3811614 A DE 3811614A DE 3811614 C1 DE3811614 C1 DE 3811614C1
Authority
DE
Germany
Prior art keywords
engine
turbo
engines
ramjet
fuselage
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.)
Expired
Application number
DE3811614A
Other languages
German (de)
English (en)
Inventor
Helmut Dr. 8000 Muenchen De John
Otfrid Dipl.-Ing. 8201 Hohenthann De Herrmann
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Priority to DE3811614A priority Critical patent/DE3811614C1/de
Priority to GB8903981A priority patent/GB2216855B/en
Priority to FR8902577A priority patent/FR2629873B1/fr
Priority to US07/335,053 priority patent/US4919364A/en
Application granted granted Critical
Publication of DE3811614C1 publication Critical patent/DE3811614C1/de
Expired 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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1207—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0253—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft
    • B64D2033/026—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft for supersonic or hypersonic aircraft
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Jet Pumps And Other Pumps (AREA)
DE3811614A 1988-04-07 1988-04-07 Expired DE3811614C1 (enExample)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE3811614A DE3811614C1 (enExample) 1988-04-07 1988-04-07
GB8903981A GB2216855B (en) 1988-04-07 1989-02-22 Propulsive unit arrangement for hypersonic flight vehicles
FR8902577A FR2629873B1 (fr) 1988-04-07 1989-02-28 Agencement de propulseurs pour appareils volants hypersoniques
US07/335,053 US4919364A (en) 1988-04-07 1989-04-07 Propulsion system for hypersonic flight

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3811614A DE3811614C1 (enExample) 1988-04-07 1988-04-07

Publications (1)

Publication Number Publication Date
DE3811614C1 true DE3811614C1 (enExample) 1989-05-18

Family

ID=6351526

Family Applications (1)

Application Number Title Priority Date Filing Date
DE3811614A Expired DE3811614C1 (enExample) 1988-04-07 1988-04-07

Country Status (4)

Country Link
US (1) US4919364A (enExample)
DE (1) DE3811614C1 (enExample)
FR (1) FR2629873B1 (enExample)
GB (1) GB2216855B (enExample)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0392526A1 (de) * 1989-04-14 1990-10-17 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Schubdüse
DE3922018A1 (de) * 1989-07-05 1991-01-17 Messerschmitt Boelkow Blohm Hyperschallkombinationsantrieb
DE4004416A1 (de) * 1990-02-13 1991-08-14 Mtu Muenchen Gmbh Gasturbinen-staustrahltriebwerk
DE4008951A1 (de) * 1990-03-20 1991-09-26 Messerschmitt Boelkow Blohm Einlauframpe fuer ueber- oder hyperschallflugzeuge
DE4008956A1 (de) * 1990-03-20 1991-09-26 Messerschmitt Boelkow Blohm Einlaufsystem fuer ueber- oder hyperschallflugzeuge
DE4111396A1 (de) * 1990-04-14 1991-10-02 Kastens Karl Turbotriebwerk fuer hyperschallfluggeraete
DE4117933A1 (de) * 1990-04-14 1991-11-21 Kastens Karl Turbotriebwerk fuer hyperschallfluggeraete
DE4113976A1 (de) * 1990-04-14 1992-02-27 Kastens Karl Turbotriebwerk fuer hyperschallfluggeraete
DE19536181A1 (de) * 1995-09-28 1997-04-03 Gerhard Ittner Luftstrahltriebwerk für hyperschallschnelle Flugzeuge
RU2116223C1 (ru) * 1994-10-04 1998-07-27 ОЛЕЙНОВ Геннадий Александрович Устройство для улучшения аэрогидродинамических качеств конструкций
WO2008115273A3 (en) * 2006-10-26 2009-03-12 Boeing Co Tandem air inlet apparatus and method for an airborne mobile platform

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DE3901487A1 (de) * 1989-01-19 1990-07-26 Mtu Muenchen Gmbh Schubduese
US5105615A (en) * 1989-02-03 1992-04-21 Mtu Motoren- Und Turbinen-Union Munchen Gmbh Turbojet engine with at least one axially movable arranged sliding valve
US5081831A (en) * 1989-03-23 1992-01-21 General Electric Company Scramjet combustor
US5109670A (en) * 1989-03-23 1992-05-05 General Electric Company Scramjet combustor
US5072582A (en) * 1989-03-23 1991-12-17 General Electric Company Scramjet combustor
US5103633A (en) * 1989-03-23 1992-04-14 General Electric Company Scramjet combustor
US5097663A (en) * 1989-03-23 1992-03-24 General Electric Company Scramjet combustor
US5072581A (en) * 1989-03-23 1991-12-17 General Electric Company Scramjet combustor
US5694768A (en) * 1990-02-23 1997-12-09 General Electric Company Variable cycle turbofan-ramjet engine
US5123240A (en) * 1990-03-19 1992-06-23 General Electric Co. Method and apparatus for ejecting foreign matter from the primary flow path of a gas turbine engine
US5154052A (en) * 1990-05-07 1992-10-13 General Electric Company Exhaust assembly for a high speed civil transport aircraft engine
US5236152A (en) * 1992-01-30 1993-08-17 Rockwell International Corporation Cooling/fuel system for hypersonic flight
FR2692938B1 (fr) * 1992-06-24 1994-09-02 Snecma Réacteur combiné et muni de moyens de commutation entre deux états de fonctionnement.
FR2692939B1 (fr) * 1992-06-24 1994-09-02 Snecma Réacteur combiné en statoréacteur et turboréacteur.
DE4222947C2 (de) * 1992-07-11 1995-02-02 Deutsche Aerospace Strahltriebwerk
US5697394A (en) * 1993-03-02 1997-12-16 United Technologies Corporation Low observable engine air inlet system
FR2710607B1 (fr) * 1993-10-01 1995-12-01 Onera (Off Nat Aerospatiale) Entrée d'air supersonique et hypersonique bidimensionnelle, à trois rampes mobiles, pour l'air de combustion d'un moteur d'aéronef .
GB2289504B (en) * 1994-05-11 1998-01-14 British Aerospace Gas turbine propulsion unit
US5897078A (en) * 1995-12-15 1999-04-27 The Boeing Company Multi-service common airframe-based aircraft
US5831155A (en) * 1996-12-02 1998-11-03 Atlantic Research Corporation Apparatus and method for simulating rocket-to-ramjet transition in a propulsion system
WO1998037323A1 (fr) * 1997-02-25 1998-08-27 Anatoly Grigorievich Korolev Moteur magneto-gazo-dynamique combine a statoreacteur
US6119985A (en) * 1997-03-07 2000-09-19 Pioneer Rocketplane Corporation Reusable rocket-propelled high altitude airplane and method and apparatus for mid-air oxidizer transfer to said airplane
RU2130407C1 (ru) * 1998-04-14 1999-05-20 Анакин Анатолий Тимофеевич Летательный аппарат с комбинированной двигательной установкой
US6178741B1 (en) 1998-10-16 2001-01-30 Trw Inc. Mems synthesized divert propulsion system
US6793175B1 (en) * 1999-08-25 2004-09-21 The Boeing Company Supersonic external-compression diffuser and method for designing same
US6527224B2 (en) * 2001-03-23 2003-03-04 The Boeing Company Separate boundary layer engine inlet
US6968695B2 (en) * 2002-09-13 2005-11-29 The Boeing Company Compact lightweight ramjet engines incorporating swirl augmented combustion with improved performance
US6895756B2 (en) * 2002-09-13 2005-05-24 The Boeing Company Compact swirl augmented afterburners for gas turbine engines
US6907724B2 (en) * 2002-09-13 2005-06-21 The Boeing Company Combined cycle engines incorporating swirl augmented combustion for reduced volume and weight and improved performance
US7216474B2 (en) * 2004-02-19 2007-05-15 Aerojet-General Corporation Integrated air inlet system for multi-propulsion aircraft engines
RU2276272C2 (ru) * 2004-05-05 2006-05-10 Казанский государственный технический университет им. А.Н. Туполева (КГТУ им. А.Н. Туполева) Воздушная турбина привода лебедки для роспуска и подбора антенны
US7828243B2 (en) * 2005-08-03 2010-11-09 Northrop Grumman Systems Corporation SCRAMjet arrangement for hypersonic aircraft
US7837142B2 (en) * 2006-10-12 2010-11-23 Aerion Corporation Supersonic aircraft jet engine
US7762077B2 (en) * 2006-12-05 2010-07-27 Pratt & Whitney Rocketdyne, Inc. Single-stage hypersonic vehicle featuring advanced swirl combustion
US20080128547A1 (en) * 2006-12-05 2008-06-05 Pratt & Whitney Rocketdyne, Inc. Two-stage hypersonic vehicle featuring advanced swirl combustion
US7762058B2 (en) * 2007-04-17 2010-07-27 Pratt & Whitney Rocketdyne, Inc. Ultra-compact, high performance aerovortical rocket thruster
US7690192B2 (en) * 2007-04-17 2010-04-06 Pratt & Whitney Rocketdyne, Inc. Compact, high performance swirl combustion rocket engine
US8794902B1 (en) 2010-01-26 2014-08-05 II Daniel K. Van Ness System and method to improve the exhaust pressure across a RAM air turbine through secondary flow mixing
US20120070271A1 (en) 2010-09-21 2012-03-22 Urban Justin R Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion events
US9109539B2 (en) 2010-12-27 2015-08-18 Rolls-Royce North American Technologies, Inc. Turbine based combined cycle engine
GB201108951D0 (en) * 2011-05-24 2011-10-05 Bae Systems Plc Air vehicles
US9884688B2 (en) * 2013-02-14 2018-02-06 Gulfstream Aerospace Corporation Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system
US9856824B2 (en) * 2013-03-07 2018-01-02 Rolls-Royce North American Technologies Inc. Aircraft nozzle system
US9656760B2 (en) * 2013-11-07 2017-05-23 Sikorsky Aircraft Corporation Variable geometry helicopter engine inlet
CN105221266B (zh) * 2015-10-29 2017-08-29 西北工业大学 一种火箭基组合循环发动机变吸除控制进气道
US10252791B2 (en) * 2016-08-23 2019-04-09 General Electric Company Deployable assembly for a propulsor
EP3412563B1 (en) * 2017-06-08 2022-11-23 Airbus Defence and Space GmbH Variable and adaptable diverterless bump inlet
CN107620653B (zh) * 2017-09-27 2018-11-02 西北工业大学 一种用于固体火箭燃气超燃冲压发动机的扰流装置
EP3668791B1 (en) 2017-11-10 2022-06-15 Donaldson Company, Inc. Airflow control system and methods thereof
US10927708B2 (en) * 2018-10-29 2021-02-23 Rolls-Royce North American Technologies Inc. Isolated turbine engine cooling
US11261791B2 (en) 2019-02-25 2022-03-01 Rolls-Royce Corporation Hybrid propulsion cooling system
US11339744B1 (en) * 2020-02-07 2022-05-24 Rolls-Royce North American Technologies Inc. Pressure equalization in a dual flow path exhaust of a hypersonic propulsion system
CN112228243A (zh) * 2020-10-16 2021-01-15 中国航发四川燃气涡轮研究院 一种用于组合喷管变状态调节的液压推动式凸轮机构
CN114151196B (zh) * 2022-02-09 2022-05-24 南京航空航天大学 一种并联式组合动力进气道的调节机构及设计方法
CN114658563B (zh) * 2022-04-15 2024-06-14 中国航空发动机研究院 一种涡轮基组合循环发动机、飞行器及控制方法
US12246816B2 (en) * 2022-05-02 2025-03-11 Jean-Paul MERRIEN Mobile units
CN119429129B (zh) * 2024-10-15 2025-07-08 中国航空发动机研究院 进气预冷换热器与分流板一体化结构及航空发动机

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Title
US-NASA-Report CR 158926-1 "Hypersonic Cruise Aircraft Propulsion Integration Study" von R.E. Morris u. G.D. Brewer *

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0392526A1 (de) * 1989-04-14 1990-10-17 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Schubdüse
DE3922018A1 (de) * 1989-07-05 1991-01-17 Messerschmitt Boelkow Blohm Hyperschallkombinationsantrieb
DE4004416A1 (de) * 1990-02-13 1991-08-14 Mtu Muenchen Gmbh Gasturbinen-staustrahltriebwerk
DE4008951A1 (de) * 1990-03-20 1991-09-26 Messerschmitt Boelkow Blohm Einlauframpe fuer ueber- oder hyperschallflugzeuge
DE4008956A1 (de) * 1990-03-20 1991-09-26 Messerschmitt Boelkow Blohm Einlaufsystem fuer ueber- oder hyperschallflugzeuge
DE4117933A1 (de) * 1990-04-14 1991-11-21 Kastens Karl Turbotriebwerk fuer hyperschallfluggeraete
DE4111396A1 (de) * 1990-04-14 1991-10-02 Kastens Karl Turbotriebwerk fuer hyperschallfluggeraete
DE4113976A1 (de) * 1990-04-14 1992-02-27 Kastens Karl Turbotriebwerk fuer hyperschallfluggeraete
RU2116223C1 (ru) * 1994-10-04 1998-07-27 ОЛЕЙНОВ Геннадий Александрович Устройство для улучшения аэрогидродинамических качеств конструкций
DE19536181A1 (de) * 1995-09-28 1997-04-03 Gerhard Ittner Luftstrahltriebwerk für hyperschallschnelle Flugzeuge
WO2008115273A3 (en) * 2006-10-26 2009-03-12 Boeing Co Tandem air inlet apparatus and method for an airborne mobile platform
GB2456465A (en) * 2006-10-26 2009-07-22 Boeing Co Tandem air inlet apparatus and method for an airborne mobile platform
GB2456465B (en) * 2006-10-26 2011-03-16 Boeing Co Tandem air inlet apparatus and method for an airborne mobile platform

Also Published As

Publication number Publication date
FR2629873A1 (fr) 1989-10-13
GB2216855B (en) 1992-02-12
GB2216855A (en) 1989-10-18
GB8903981D0 (en) 1989-04-05
US4919364A (en) 1990-04-24
FR2629873B1 (fr) 1994-04-29

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Legal Events

Date Code Title Description
8100 Publication of the examined application without publication of unexamined application
D1 Grant (no unexamined application published) patent law 81
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: DEUTSCHE AEROSPACE AG, 8000 MUENCHEN, DE

8327 Change in the person/name/address of the patent owner

Owner name: DAIMLER-BENZ AEROSPACE AKTIENGESELLSCHAFT, 80804 M

8339 Ceased/non-payment of the annual fee