FR2511339B1 - Entree d'air reglable, notamment diffuseur bidimensionnel a choc oblique pour turboreacteurs d'entrainement d'aeronefs a haute puissance - Google Patents

Entree d'air reglable, notamment diffuseur bidimensionnel a choc oblique pour turboreacteurs d'entrainement d'aeronefs a haute puissance

Info

Publication number
FR2511339B1
FR2511339B1 FR7919808A FR7919808A FR2511339B1 FR 2511339 B1 FR2511339 B1 FR 2511339B1 FR 7919808 A FR7919808 A FR 7919808A FR 7919808 A FR7919808 A FR 7919808A FR 2511339 B1 FR2511339 B1 FR 2511339B1
Authority
FR
France
Prior art keywords
turboreactors
air intake
adjustable air
oblique shock
power aircraft
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
FR7919808A
Other languages
English (en)
Other versions
FR2511339A1 (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.)
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 FR2511339A1 publication Critical patent/FR2511339A1/fr
Application granted granted Critical
Publication of FR2511339B1 publication Critical patent/FR2511339B1/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • 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
    • F02C7/057—Control or regulation
    • 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
    • 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
    • B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0273—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for jet engines

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)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
FR7919808A 1978-08-02 1979-08-01 Entree d'air reglable, notamment diffuseur bidimensionnel a choc oblique pour turboreacteurs d'entrainement d'aeronefs a haute puissance Expired FR2511339B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19782833771 DE2833771C2 (de) 1978-08-02 1978-08-02 Verstellbarer Lufteinlauf, insbesondere zweidimensionaler Schrägstoßdiffusor für Gasturbinenstrahltriebwerke zum Antrieb von Hochleistungsflugzeugen

Publications (2)

Publication Number Publication Date
FR2511339A1 FR2511339A1 (fr) 1983-02-18
FR2511339B1 true FR2511339B1 (fr) 1985-07-26

Family

ID=6045966

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7919808A Expired FR2511339B1 (fr) 1978-08-02 1979-08-01 Entree d'air reglable, notamment diffuseur bidimensionnel a choc oblique pour turboreacteurs d'entrainement d'aeronefs a haute puissance

Country Status (3)

Country Link
DE (1) DE2833771C2 (fr)
FR (1) FR2511339B1 (fr)
GB (1) GB2097863B (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE35387E (en) * 1985-04-09 1996-12-03 Dynamic Engineering, Inc. Superfragile tactical fighter aircraft and method of flying it in supernormal flight
BR8601586A (pt) * 1985-04-09 1986-12-30 Dei Tech Inc Aviao de caca tatico super agil e processo de pilotar o mesmo
DE3835664A1 (de) * 1988-10-20 1990-04-26 Messerschmitt Boelkow Blohm Variabler lufteinlauf fuer hochleistungsflugzeuge
DE3835663A1 (de) * 1988-10-20 1990-04-26 Messerschmitt Boelkow Blohm Einrichtung zum steuern eines lufteinlaufs an hochleistungsflugzeugen
DE3835665A1 (de) * 1988-10-20 1990-04-26 Messerschmitt Boelkow Blohm Steuerung fuer einen lufteinlauf von hochleistungsflugzeugen
DE3835669A1 (de) * 1988-10-20 1990-04-26 Messerschmitt Boelkow Blohm Lufteinlauf fuer hochleistungsflugzeuge
DE3835668A1 (de) * 1988-10-20 1990-04-26 Messerschmitt Boelkow Blohm Steuerbarer lufteinlauf fuer hochleistungsflugzeuge
DE3835667A1 (de) * 1988-10-20 1990-04-26 Messerschmitt Boelkow Blohm Lufteinlaufsteuerung fuer hochleistungsflugzeuge
DE4223413C2 (de) * 1992-07-16 1996-01-18 Daimler Benz Aerospace Ag Einlaufsystem für Über- und Hyperschallflugzeuge

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2971328A (en) * 1958-07-22 1961-02-14 United Aircraft Corp Control system for air inlet bypass
FR1313327A (fr) * 1961-11-17 1962-12-28 Nord Aviation Instrument de bord pour le contrôle d'une entrée d'air de forme variable pour un moteur supersonique
DE2358926C3 (de) * 1973-11-27 1979-08-02 Messerschitt-Boelkow-Blohm Gmbh, 8000 Muenchen Regelung von verstellbaren Überschallufteinläufen, insbesondere zweidimensionalen SchrägstoBdiffusoren für Gasturbinenstrahltriebwerke zum Antrieb von Hochleistungsflugzeugen

Also Published As

Publication number Publication date
FR2511339A1 (fr) 1983-02-18
DE2833771C2 (de) 1985-12-19
DE2833771A1 (de) 1982-09-09
GB2097863A (en) 1982-11-10
GB2097863B (en) 1983-06-02

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Legal Events

Date Code Title Description
TP Transmission of property
ST Notification of lapse