GB2097863B - Variable air inlet for gas turbine engine - Google Patents

Variable air inlet for gas turbine engine

Info

Publication number
GB2097863B
GB2097863B GB7923380A GB7923380A GB2097863B GB 2097863 B GB2097863 B GB 2097863B GB 7923380 A GB7923380 A GB 7923380A GB 7923380 A GB7923380 A GB 7923380A GB 2097863 B GB2097863 B GB 2097863B
Authority
GB
United Kingdom
Prior art keywords
air inlet
gas turbine
turbine engine
variable air
variable
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
GB7923380A
Other versions
GB2097863A (en
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 GB2097863A publication Critical patent/GB2097863A/en
Application granted granted Critical
Publication of GB2097863B publication Critical patent/GB2097863B/en
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)
GB7923380A 1978-08-02 1979-07-05 Variable air inlet for gas turbine engine Expired GB2097863B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19782833771 DE2833771C2 (en) 1978-08-02 1978-08-02 Adjustable air inlet, in particular two-dimensional angled shock diffuser for gas turbine jet engines for propelling high-performance aircraft

Publications (2)

Publication Number Publication Date
GB2097863A GB2097863A (en) 1982-11-10
GB2097863B true GB2097863B (en) 1983-06-02

Family

ID=6045966

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7923380A Expired GB2097863B (en) 1978-08-02 1979-07-05 Variable air inlet for gas turbine engine

Country Status (3)

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

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
ES9100002A1 (en) * 1985-04-09 1991-01-01 Dynamic Eng Inc Super Agile aircraft and method of flying it in supernormal flight.
DE3835668A1 (en) * 1988-10-20 1990-04-26 Messerschmitt Boelkow Blohm Controllable air inlet on high-performance aircraft
DE3835664A1 (en) * 1988-10-20 1990-04-26 Messerschmitt Boelkow Blohm Variable air inlet for high-performance aircraft
DE3835665A1 (en) * 1988-10-20 1990-04-26 Messerschmitt Boelkow Blohm Controller for an air inlet for high-performance aircraft
DE3835669A1 (en) * 1988-10-20 1990-04-26 Messerschmitt Boelkow Blohm Air inlet for high-performance aircraft
DE3835667A1 (en) * 1988-10-20 1990-04-26 Messerschmitt Boelkow Blohm Air-inlet controller for high-performance aircraft
DE3835663A1 (en) * 1988-10-20 1990-04-26 Messerschmitt Boelkow Blohm Device for controlling an air inlet on high-performance aircraft
DE4223413C2 (en) * 1992-07-16 1996-01-18 Daimler Benz Aerospace Ag Infeed system for supersonic and hypersonic aircraft

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 (en) * 1961-11-17 1962-12-28 Nord Aviation On-board instrument for controlling an air inlet of variable shape for a supersonic engine
DE2358926C3 (en) * 1973-11-27 1979-08-02 Messerschitt-Boelkow-Blohm Gmbh, 8000 Muenchen Regulation of adjustable supersonic air inlets, in particular two-dimensional oblique thrust diffusers for gas turbine jet engines for propelling high-performance aircraft

Also Published As

Publication number Publication date
DE2833771C2 (en) 1985-12-19
FR2511339A1 (en) 1983-02-18
GB2097863A (en) 1982-11-10
FR2511339B1 (en) 1985-07-26
DE2833771A1 (en) 1982-09-09

Similar Documents

Publication Publication Date Title
JPS566024A (en) Air inlet port for gas turbine engine
GB2019500B (en) Air manifold for a gas turbine engine
GB2044359B (en) Gas turbine engine air intakes
ZA777122B (en) Inlet air cleaner assembly for turbine engines
GB2030657B (en) Blade for gas turbine engine
GB2036169B (en) Inlet air passage for an engine
JPS5575537A (en) Gas turbine engine
JPS5560624A (en) Airrcooled turbine for gas turbine engine
JPS5587826A (en) Gas turbine engine
JPS54160911A (en) Blade for gas turbine engine
GB2015651B (en) Gas turbine engine combustion equipment
JPS55131531A (en) Gas turbine engine
GB2019945A (en) Partial span inlet guide vane for crossconnected gas turbine engines
JPS55123924A (en) Gas turbine engine
GB2073325B (en) Gas turbine aircraft engine air intake
JPS5641436A (en) Exhaust nozzle for gas turbine engines
JPS5596322A (en) Exhaust gas turbine supercharger
JPS54134207A (en) Combustion chamber for gas turbine engine
JPS566004A (en) Gas turbine engine
GB2032532B (en) Gas turbine engine compressor control
JPS55139935A (en) Gas turbine engine
GB2044361B (en) Gas turbine engine
AU529701B2 (en) Inlet air cleaner for gas turbine engine
JPS56129723A (en) Air intake part for gas turbine engine
GB2038425B (en) Gas turbine engine

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940705