DE68900677D1 - Zweidimensionaler und asymmetrischer ueberschall-lufteinlauf fuer die verbrennungsluft eines flugzeugmotors. - Google Patents

Zweidimensionaler und asymmetrischer ueberschall-lufteinlauf fuer die verbrennungsluft eines flugzeugmotors.

Info

Publication number
DE68900677D1
DE68900677D1 DE8989402144T DE68900677T DE68900677D1 DE 68900677 D1 DE68900677 D1 DE 68900677D1 DE 8989402144 T DE8989402144 T DE 8989402144T DE 68900677 T DE68900677 T DE 68900677T DE 68900677 D1 DE68900677 D1 DE 68900677D1
Authority
DE
Germany
Prior art keywords
asymmetric
dimensional
supervisor
air inlet
plane 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.)
Expired - Lifetime
Application number
DE8989402144T
Other languages
English (en)
Inventor
Francois Falempin
Claude Sans
Patrick Champigny
Gerard Laruelle
Jean-Marie Garrel
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.)
Office National dEtudes et de Recherches Aerospatiales ONERA
Original Assignee
Office National dEtudes et de Recherches Aerospatiales ONERA
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 Office National dEtudes et de Recherches Aerospatiales ONERA filed Critical Office National dEtudes et de Recherches Aerospatiales ONERA
Application granted granted Critical
Publication of DE68900677D1 publication Critical patent/DE68900677D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • 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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0253—Arrangements 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—Arrangements 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]

Landscapes

  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Characterised By The Charging Evacuation (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Toys (AREA)
DE8989402144T 1988-08-04 1989-07-28 Zweidimensionaler und asymmetrischer ueberschall-lufteinlauf fuer die verbrennungsluft eines flugzeugmotors. Expired - Lifetime DE68900677D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8810557A FR2635075B1 (fr) 1988-08-04 1988-08-04 Entree d'air supersonique bidimensionnelle et asymetrique pour l'air de combustion d'un moteur d'aeronef

Publications (1)

Publication Number Publication Date
DE68900677D1 true DE68900677D1 (de) 1992-02-20

Family

ID=9369121

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8989402144T Expired - Lifetime DE68900677D1 (de) 1988-08-04 1989-07-28 Zweidimensionaler und asymmetrischer ueberschall-lufteinlauf fuer die verbrennungsluft eines flugzeugmotors.

Country Status (5)

Country Link
US (1) US5005782A (de)
EP (1) EP0354103B1 (de)
JP (1) JP2686149B2 (de)
DE (1) DE68900677D1 (de)
FR (1) FR2635075B1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113247277A (zh) * 2021-06-30 2021-08-13 中国人民解放军国防科技大学 一种含有折叠翼的高超声速进气道保形整流罩方案

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2635076B1 (fr) * 1988-08-04 1994-09-23 Onera (Off Nat Aerospatiale) Entree d'air supersonique et hypersonique bidimensionnelle et symetrique pour l'air de combustion d'un moteur d'aeronef
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 .
FR2870513B1 (fr) * 2004-05-24 2006-08-11 Airbus France Sas Nacelle de reacteur pour avion supersonique
FR2872781B1 (fr) * 2004-07-08 2007-10-05 Airbus France Sas Plancher pour aeronef
US7837142B2 (en) * 2006-10-12 2010-11-23 Aerion Corporation Supersonic aircraft jet engine
FR2912992B1 (fr) * 2007-02-23 2009-12-04 Novac Modoran Avion supersonique a prises d'air mobiles.
US9169779B2 (en) * 2007-10-09 2015-10-27 United Technologies Corp. Systems and methods for altering inlet airflow of gas turbine engines
RU2440916C1 (ru) * 2010-07-28 2012-01-27 Открытое акционерное общество "ОКБ Сухого" Самолет интегральной аэродинамической компоновки
RU2472956C2 (ru) * 2011-04-29 2013-01-20 Открытое акционерное общество "ОКБ Сухого" Сверхзвуковой регулируемый воздухозаборник
US9874144B2 (en) * 2015-01-23 2018-01-23 The Boeing Company Supersonic caret inlet system
US9964038B2 (en) * 2015-03-16 2018-05-08 The Boeing Company Supersonic caret inlet system leading edge slat for improved inlet performance at off-design flight conditions
CN113291477A (zh) * 2021-05-19 2021-08-24 中航西安飞机工业集团股份有限公司 一种飞机进气道气流矢量控制结构及飞机姿态控制方法
CN117823281B (zh) * 2024-03-06 2024-06-04 中国空气动力研究与发展中心空天技术研究所 一种品字形排列的多通道宽速域可调进气道

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126174A (en) * 1964-03-24 Air inlet mechanism for supersonic aircrafts
US3062484A (en) * 1953-04-10 1962-11-06 Curtiss Wright Corp Supersonic air inlet construction
US2932945A (en) * 1957-04-16 1960-04-19 Westinghouse Electric Corp Weathercocking supersonic diffuser
GB899625A (en) * 1958-04-03 1962-06-27 English Electric Co Ltd Improvements in and relating to air intakes for air aspirating aircraft engines
US3104522A (en) * 1958-04-03 1963-09-24 English Electric Co Ltd Air intakes for air aspirating aircraft engines
FR1234483A (fr) * 1958-09-01 1960-10-17 Bristol Siddeley Engines Ltd Perfectionnements apportés aux dispositifs d'admission d'air pour avions supersoniques
US3161379A (en) * 1962-08-23 1964-12-15 Bristel Siddeley Engines Ltd Aircraft powerplant
DE1250744B (de) * 1964-01-14 1967-09-21
GB1119701A (en) * 1964-08-13 1968-07-10 Bristol Siddeley Engines Ltd Guards for air intakes of jet engines
US3265331A (en) * 1964-09-18 1966-08-09 Gen Electric Supersonic inlet
FR1552118A (de) * 1967-11-17 1969-01-03
US3799475A (en) * 1971-06-11 1974-03-26 Nasa Airflow control system for supersonic inlets
US4007891A (en) * 1975-09-12 1977-02-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Jet engine air intake system
US4372505A (en) * 1979-12-17 1983-02-08 The Boeing Company Supersonic inlet having variable area sideplate openings

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113247277A (zh) * 2021-06-30 2021-08-13 中国人民解放军国防科技大学 一种含有折叠翼的高超声速进气道保形整流罩方案

Also Published As

Publication number Publication date
FR2635075B1 (fr) 1994-09-23
FR2635075A1 (fr) 1990-02-09
EP0354103A1 (de) 1990-02-07
JP2686149B2 (ja) 1997-12-08
US5005782A (en) 1991-04-09
JPH0277396A (ja) 1990-03-16
EP0354103B1 (de) 1992-01-08

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee