FR1234483A - Improvements to air intake systems for supersonic airplanes - Google Patents

Improvements to air intake systems for supersonic airplanes

Info

Publication number
FR1234483A
FR1234483A FR803934A FR803934A FR1234483A FR 1234483 A FR1234483 A FR 1234483A FR 803934 A FR803934 A FR 803934A FR 803934 A FR803934 A FR 803934A FR 1234483 A FR1234483 A FR 1234483A
Authority
FR
France
Prior art keywords
air intake
intake systems
supersonic airplanes
airplanes
supersonic
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
FR803934A
Other languages
French (fr)
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.)
Bristol Siddeley Engines Ltd
Original Assignee
Bristol Siddeley Engines 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.)
Filing date
Publication date
Application filed by Bristol Siddeley Engines Ltd filed Critical Bristol Siddeley Engines Ltd
Application granted granted Critical
Publication of FR1234483A publication Critical patent/FR1234483A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR803934A 1958-09-01 1959-08-31 Improvements to air intake systems for supersonic airplanes Expired FR1234483A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1234483X 1958-09-01

Publications (1)

Publication Number Publication Date
FR1234483A true FR1234483A (en) 1960-10-17

Family

ID=10884732

Family Applications (1)

Application Number Title Priority Date Filing Date
FR803934A Expired FR1234483A (en) 1958-09-01 1959-08-31 Improvements to air intake systems for supersonic airplanes

Country Status (1)

Country Link
FR (1) FR1234483A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3186661A (en) * 1960-05-13 1965-06-01 Bristol Siddeley Engines Ltd Aircraft propulsion power plants
EP0354103A1 (en) * 1988-08-04 1990-02-07 Office National D'etudes Et De Recherches Aerospatiales (Onera) Bidimensional and asymmetrical supersonic air intake for the combustion air of an aircraft engine
US5004187A (en) * 1988-08-04 1991-04-02 Office National D'etudes Et De Recherches Aerospatiales Symmetrical, two dimensional, supersonic and hypersonic air intake for the combustion air of an aircraft engine
EP3069999A1 (en) * 2015-03-16 2016-09-21 The Boeing Company Supersonic caret inlet system leading edge slat for improved inlet performance at off-design flight conditions

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3186661A (en) * 1960-05-13 1965-06-01 Bristol Siddeley Engines Ltd Aircraft propulsion power plants
EP0354103A1 (en) * 1988-08-04 1990-02-07 Office National D'etudes Et De Recherches Aerospatiales (Onera) Bidimensional and asymmetrical supersonic air intake for the combustion air of an aircraft engine
FR2635075A1 (en) * 1988-08-04 1990-02-09 Onera (Off Nat Aerospatiale) TWO-DIMENSIONAL AND ASYMMETRIC SUPERSONIC AIR INLET FOR COMBUSTION AIR OF AN AIRCRAFT ENGINE
US5004187A (en) * 1988-08-04 1991-04-02 Office National D'etudes Et De Recherches Aerospatiales Symmetrical, two dimensional, supersonic and hypersonic air intake for the combustion air of an aircraft engine
EP3069999A1 (en) * 2015-03-16 2016-09-21 The Boeing Company Supersonic caret inlet system leading edge slat for improved inlet performance at off-design flight conditions
CN106043716A (en) * 2015-03-16 2016-10-26 波音公司 Supersonic caret inlet system leading edge slat for improved inlet performance at off-design flight conditions
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
RU2699329C2 (en) * 2015-03-16 2019-09-04 Зе Боинг Компани Supersonic inlet device for jet engine of aircraft and method of supporting attached shock wave in such device
AU2016200187B2 (en) * 2015-03-16 2020-02-27 The Boeing Company Supersonic caret inlet system leading edge slat for improved inlet performance at off-design flight conditions
CN106043716B (en) * 2015-03-16 2021-03-16 波音公司 Supersonic Carlt air intake system leading edge slat for improved air intake performance under off-design flight conditions

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