FR2370865A1 - Diffuseur a entree d'air supersonique pour propulseur aeronautique aerobie, notamment pour stato-reacteur - Google Patents

Diffuseur a entree d'air supersonique pour propulseur aeronautique aerobie, notamment pour stato-reacteur

Info

Publication number
FR2370865A1
FR2370865A1 FR7733969A FR7733969A FR2370865A1 FR 2370865 A1 FR2370865 A1 FR 2370865A1 FR 7733969 A FR7733969 A FR 7733969A FR 7733969 A FR7733969 A FR 7733969A FR 2370865 A1 FR2370865 A1 FR 2370865A1
Authority
FR
France
Prior art keywords
air inlet
stato
aeronautical
aerobic
thruster
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.)
Granted
Application number
FR7733969A
Other languages
English (en)
French (fr)
Other versions
FR2370865B3 (en:Method
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
Publication of FR2370865A1 publication Critical patent/FR2370865A1/fr
Application granted granted Critical
Publication of FR2370865B3 publication Critical patent/FR2370865B3/fr
Granted 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)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Aeration Devices For Treatment Of Activated Polluted Sludge (AREA)
FR7733969A 1976-11-16 1977-11-10 Diffuseur a entree d'air supersonique pour propulseur aeronautique aerobie, notamment pour stato-reacteur Granted FR2370865A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19762652114 DE2652114A1 (de) 1976-11-16 1976-11-16 Ueberschalleinlaufdiffusor fuer ein luftatmendes flugtriebwerk, insbesondere staustrahltriebwerk

Publications (2)

Publication Number Publication Date
FR2370865A1 true FR2370865A1 (fr) 1978-06-09
FR2370865B3 FR2370865B3 (en:Method) 1980-08-14

Family

ID=5993247

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7733969A Granted FR2370865A1 (fr) 1976-11-16 1977-11-10 Diffuseur a entree d'air supersonique pour propulseur aeronautique aerobie, notamment pour stato-reacteur

Country Status (3)

Country Link
DE (1) DE2652114A1 (en:Method)
FR (1) FR2370865A1 (en:Method)
GB (1) GB1591994A (en:Method)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0392520A1 (de) * 1989-04-14 1990-10-17 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Turbinen-Staustrahltriebwerk

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3011796C2 (de) * 1980-03-27 1982-11-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Überschall-Lufteinlauf für Strahltriebwerke, insbesondere für Staustrahltriebwerke zum Antrieb von Flugkörpern

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0392520A1 (de) * 1989-04-14 1990-10-17 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Turbinen-Staustrahltriebwerk

Also Published As

Publication number Publication date
DE2652114A1 (de) 1978-05-18
FR2370865B3 (en:Method) 1980-08-14
GB1591994A (en) 1981-07-01

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Legal Events

Date Code Title Description
ST Notification of lapse