JPS5777295A - Method of increasing composite thrust in aircraft - Google Patents

Method of increasing composite thrust in aircraft

Info

Publication number
JPS5777295A
JPS5777295A JP13785481A JP13785481A JPS5777295A JP S5777295 A JPS5777295 A JP S5777295A JP 13785481 A JP13785481 A JP 13785481A JP 13785481 A JP13785481 A JP 13785481A JP S5777295 A JPS5777295 A JP S5777295A
Authority
JP
Japan
Prior art keywords
aircraft
composite thrust
increasing composite
increasing
thrust
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.)
Pending
Application number
JP13785481A
Other languages
English (en)
Japanese (ja)
Inventor
Reeberuto Geruharuto
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 JPS5777295A publication Critical patent/JPS5777295A/ja
Pending 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Jet Pumps And Other Pumps (AREA)
JP13785481A 1980-09-03 1981-09-03 Method of increasing composite thrust in aircraft Pending JPS5777295A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19803033101 DE3033101C2 (de) 1980-09-03 1980-09-03 Anordnung zur Erhöhung der resultierenden Vortriebskraft bei Flugzeugen

Publications (1)

Publication Number Publication Date
JPS5777295A true JPS5777295A (en) 1982-05-14

Family

ID=6111003

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13785481A Pending JPS5777295A (en) 1980-09-03 1981-09-03 Method of increasing composite thrust in aircraft

Country Status (4)

Country Link
JP (1) JPS5777295A (enrdf_load_stackoverflow)
DE (1) DE3033101C2 (enrdf_load_stackoverflow)
FR (1) FR2489245A1 (enrdf_load_stackoverflow)
GB (1) GB2083420B (enrdf_load_stackoverflow)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3274535D1 (en) * 1981-10-15 1987-01-15 Aeritalia Spa Aircraft with jet propulsion
AU555526B2 (en) * 1982-10-29 1986-09-25 General Electric Company Aircraft engine nacelle
GB2149456B (en) * 1983-11-08 1987-07-29 Rolls Royce Exhaust mixing in turbofan aeroengines
DE3345154C2 (de) * 1983-12-14 1987-02-12 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Tragflügel für Luftfahrzeuge
CA1324999C (en) * 1986-04-30 1993-12-07 Walter M. Presz, Jr. Bodies with reduced surface drag
GB2207468A (en) * 1987-06-01 1989-02-01 Secr Defence Vortex silencing in gas turbine engines
JP2606289Y2 (ja) * 1993-06-07 2000-10-10 富士重工業株式会社 航空機のナセル装置
US10723464B2 (en) 2015-08-26 2020-07-28 Rohr, Inc. Injector nozzle configuration for swirl anti-icing system
US10393020B2 (en) 2015-08-26 2019-08-27 Rohr, Inc. Injector nozzle configuration for swirl anti-icing system

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2641468C2 (de) * 1976-09-15 1985-06-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Flugzeug mit oberhalb der Tragflügel angeordneten Triebwerken

Also Published As

Publication number Publication date
GB2083420B (en) 1984-06-27
DE3033101C2 (de) 1984-11-22
FR2489245B3 (enrdf_load_stackoverflow) 1983-06-03
DE3033101A1 (de) 1982-03-11
FR2489245A1 (fr) 1982-03-05
GB2083420A (en) 1982-03-24

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