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FR2703322B1 - Avion de transport à arrière tronqué. - Google Patents

Avion de transport à arrière tronqué.

Info

Publication number
FR2703322B1
FR2703322B1 FR9403348A FR9403348A FR2703322B1 FR 2703322 B1 FR2703322 B1 FR 2703322B1 FR 9403348 A FR9403348 A FR 9403348A FR 9403348 A FR9403348 A FR 9403348A FR 2703322 B1 FR2703322 B1 FR 2703322B1
Authority
FR
France
Prior art keywords
transport aircraft
rear transport
truncated rear
truncated
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 - Fee Related
Application number
FR9403348A
Other languages
English (en)
Other versions
FR2703322A1 (fr
Inventor
Gerhard Lobert
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
Deutsche Aerospace 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 Deutsche Aerospace AG filed Critical Deutsche Aerospace AG
Publication of FR2703322A1 publication Critical patent/FR2703322A1/fr
Application granted granted Critical
Publication of FR2703322B1 publication Critical patent/FR2703322B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0045—Fuselages characterised by special shapes
    • 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0226—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising boundary layer control means
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
FR9403348A 1993-03-27 1994-03-22 Avion de transport à arrière tronqué. Expired - Fee Related FR2703322B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4310017A DE4310017C2 (de) 1993-03-27 1993-03-27 Transportflugzeug mit stumpfem Heck

Publications (2)

Publication Number Publication Date
FR2703322A1 FR2703322A1 (fr) 1994-10-07
FR2703322B1 true FR2703322B1 (fr) 1997-01-31

Family

ID=6484035

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9403348A Expired - Fee Related FR2703322B1 (fr) 1993-03-27 1994-03-22 Avion de transport à arrière tronqué.

Country Status (4)

Country Link
US (1) US5480110A (fr)
DE (1) DE4310017C2 (fr)
FR (1) FR2703322B1 (fr)
RU (1) RU2094307C1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7226325B1 (en) * 2001-04-11 2007-06-05 The United States Of America As Represented By The Secretary Of The Navy Device for stabilizing re-entrant cavity flows past high-speed underwater vehicles
WO2009143518A2 (fr) * 2008-05-23 2009-11-26 David Birkenstock Système de contrôle de couche frontière et procédés à cet effet
FR2997681B1 (fr) * 2012-11-08 2015-05-15 Snecma Avion propulse par un turboreacteur a soufflantes contrarotatives
US12187443B2 (en) * 2020-02-14 2025-01-07 Bombardier Inc. Excess thrust control for an aircraft

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2399839A (en) * 1943-09-29 1946-05-07 Harry L Vorse Flying machine
DE906660C (de) * 1945-03-31 1954-03-15 Anxionnaz Rene Einrichtung zum Vermindern des Luftwiderstandes eines Luftfahrzeuges
GB954365A (en) * 1959-06-27 1964-04-08 Svenska Aeroplan Ab Jet propulsion engine power plant installation for aircraft
GB1041048A (en) * 1962-09-25 1966-09-01 Vickers Armstrongs Aircraft Improvements in aircraft having jet-propulsion power-plants
US3289977A (en) * 1965-01-11 1966-12-06 Staats Francis Lloyd Aircraft device
US3317162A (en) * 1965-07-13 1967-05-02 Charles H Grant Aircraft wing with internal air passages for increased lift
FR1460060A (fr) * 1965-10-15 1966-06-17 Nord Aviation Fuselage de grande capacité et aérodyne correspondant
DE1900380A1 (de) * 1969-01-04 1970-11-26 Hamburger Flugzeugbau Gmbh Luftfahrzeug mit drei im Bereich des Rumpfhecks angeordneten Strahltriebwerken
AT304274B (de) * 1969-03-17 1972-12-27 Hanz Fimml Dipl Ing Einrichtung zur Auftriebserzeugung für ein Flugzeug mit an den Tragflächen austretenden Gasstrahlen
GB1443333A (en) * 1972-08-12 1976-07-21 Mtu Muenchen Gmbh Aircraft having apparatus for augmenting the lift of the aircraft
US4033526A (en) * 1974-05-31 1977-07-05 William Benson Aerodynamic flow body
US4643268A (en) * 1982-04-05 1987-02-17 American Antigravity Co., Inc. Air lifted and propelled vehicle
US4749151A (en) * 1985-09-19 1988-06-07 The Boeing Company Apparatus for re-energizing boundary layer air
US5016837A (en) * 1987-06-25 1991-05-21 Venturi Applications, Inc. Venturi enhanced airfoil
US5114097A (en) * 1991-04-29 1992-05-19 Williams International Corporation Aircraft
US5299760A (en) * 1992-07-07 1994-04-05 The Dee Howard Company S-duct for a turbo-jet aircraft engine
US5368258A (en) * 1993-08-05 1994-11-29 Rohr, Inc. Arrangement for maintaining laminar air flow over gaps in aircraft engine nacelle surfaces

Also Published As

Publication number Publication date
RU2094307C1 (ru) 1997-10-27
DE4310017A1 (de) 1994-09-29
US5480110A (en) 1996-01-02
DE4310017C2 (de) 1995-06-14
RU94009999A (ru) 1997-03-20
FR2703322A1 (fr) 1994-10-07

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Legal Events

Date Code Title Description
ST Notification of lapse