FR1066135A - Air inlet device for supplying devices such as reactors in subsonic and supersonic conditions - Google Patents

Air inlet device for supplying devices such as reactors in subsonic and supersonic conditions

Info

Publication number
FR1066135A
FR1066135A FR1066135DA FR1066135A FR 1066135 A FR1066135 A FR 1066135A FR 1066135D A FR1066135D A FR 1066135DA FR 1066135 A FR1066135 A FR 1066135A
Authority
FR
France
Prior art keywords
subsonic
reactors
air inlet
inlet device
supplying devices
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
Other languages
French (fr)
Inventor
Kleber Toure
Jean-Rene Lauzely
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of FR1066135A publication Critical patent/FR1066135A/en
Expired 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

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)
FR1066135D 1952-05-28 1952-05-28 Air inlet device for supplying devices such as reactors in subsonic and supersonic conditions Expired FR1066135A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1066135T 1952-05-28

Publications (1)

Publication Number Publication Date
FR1066135A true FR1066135A (en) 1954-06-02

Family

ID=9602563

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1066135D Expired FR1066135A (en) 1952-05-28 1952-05-28 Air inlet device for supplying devices such as reactors in subsonic and supersonic conditions

Country Status (1)

Country Link
FR (1) FR1066135A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1078375B (en) * 1958-08-08 1960-03-24 Ernst Heinkel Flugzeugbau G M Adjustable air intake especially for jet engines
DE1121414B (en) * 1958-07-24 1962-01-04 Ernst Heinkel Flugzeugbau G M Device for controlling additional air in a jet engine
US3111843A (en) * 1960-08-01 1963-11-26 Cook Electric Co Hypersonic wind tunnel
US3111842A (en) * 1960-07-19 1963-11-26 Cook Electric Co Supersonic wind tunnel
DE1210258B (en) * 1961-09-22 1966-02-03 Rolls Royce Bypass gas turbine jet engine
DE1247073B (en) * 1961-09-12 1967-08-10 Bristol Siddeley Engines Ltd Method and device for cooling a supersonic gas turbine jet engine
EP4148245A3 (en) * 2021-09-10 2023-06-28 Rohr, Inc. Aircraft propulsion system with variable area inlet

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1121414B (en) * 1958-07-24 1962-01-04 Ernst Heinkel Flugzeugbau G M Device for controlling additional air in a jet engine
DE1078375B (en) * 1958-08-08 1960-03-24 Ernst Heinkel Flugzeugbau G M Adjustable air intake especially for jet engines
US3111842A (en) * 1960-07-19 1963-11-26 Cook Electric Co Supersonic wind tunnel
US3111843A (en) * 1960-08-01 1963-11-26 Cook Electric Co Hypersonic wind tunnel
DE1247073B (en) * 1961-09-12 1967-08-10 Bristol Siddeley Engines Ltd Method and device for cooling a supersonic gas turbine jet engine
DE1210258B (en) * 1961-09-22 1966-02-03 Rolls Royce Bypass gas turbine jet engine
EP4148245A3 (en) * 2021-09-10 2023-06-28 Rohr, Inc. Aircraft propulsion system with variable area inlet
US11840985B2 (en) 2021-09-10 2023-12-12 Rohr, Inc. Aircraft propulsion system with variable area inlet

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