DE60006925D1 - Profilierter Triebwerkgondelstiel für einen Flugzeugflügel - Google Patents

Profilierter Triebwerkgondelstiel für einen Flugzeugflügel

Info

Publication number
DE60006925D1
DE60006925D1 DE60006925T DE60006925T DE60006925D1 DE 60006925 D1 DE60006925 D1 DE 60006925D1 DE 60006925 T DE60006925 T DE 60006925T DE 60006925 T DE60006925 T DE 60006925T DE 60006925 D1 DE60006925 D1 DE 60006925D1
Authority
DE
Germany
Prior art keywords
airplane wing
engine pylon
profiled
profiled engine
pylon
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 - Lifetime
Application number
DE60006925T
Other languages
English (en)
Other versions
DE60006925T2 (de
Inventor
Jean-Louis Cambon
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 Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of DE60006925D1 publication Critical patent/DE60006925D1/de
Application granted granted Critical
Publication of DE60006925T2 publication Critical patent/DE60006925T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B64C7/02—Nacelles

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60006925T 1999-12-27 2000-10-30 Profilierter Triebwerkgondelstiel für einen Flugzeugflügel Expired - Lifetime DE60006925T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9916539 1999-12-27
FR9916539A FR2802896B1 (fr) 1999-12-27 1999-12-27 Mat de suspension profile de voilure d'aeronef

Publications (2)

Publication Number Publication Date
DE60006925D1 true DE60006925D1 (de) 2004-01-15
DE60006925T2 DE60006925T2 (de) 2004-10-28

Family

ID=9553876

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60006925T Expired - Lifetime DE60006925T2 (de) 1999-12-27 2000-10-30 Profilierter Triebwerkgondelstiel für einen Flugzeugflügel

Country Status (6)

Country Link
US (1) US6378804B1 (de)
EP (1) EP1112929B1 (de)
CA (1) CA2327374C (de)
DE (1) DE60006925T2 (de)
ES (1) ES2207472T3 (de)
FR (1) FR2802896B1 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2898336B1 (fr) * 2006-03-07 2009-02-27 Airbus France Sas Carenage aerodynamique destine a etre rapporte fixement sous une aile d'aeronef
FR2922520B1 (fr) * 2007-10-22 2010-04-23 Airbus France Procede de reduction de la trainee de compressibilite d'une voilure et conteneur mettant en oeuvre ce procede
EP2402251A3 (de) 2010-07-01 2015-08-05 Rolls-Royce plc Triebwerkeinbau
GB201011056D0 (en) 2010-07-01 2010-08-18 Rolls Royce Plc Pylon for attaching a gas turbine engine
GB2488172B (en) * 2011-02-21 2014-01-29 Rolls Royce Plc Flow-modifying formation for aircraft wing
FR3000721B1 (fr) * 2013-01-09 2016-10-14 Airbus Operations Sas Ensemble propulsif d'aeronef comprenant un carenage aerodynamique arriere de mat d'accrochage a parois laterales profilees pour l'injection d'air frais le long d'un plancher de protection thermique
WO2015010315A1 (en) 2013-07-26 2015-01-29 Mra Systems, Inc. Aircraft engine pylon
CA3084384A1 (en) * 2017-10-19 2019-04-25 Bombardier Inc. Aircraft pylon fairing
EP3666642A1 (de) 2018-12-10 2020-06-17 Bombardier Inc. Flugzeugflügelanordnungen
GB2580930A (en) * 2019-01-30 2020-08-05 Airbus Operations Ltd Fairing for folding wing tip

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3960345A (en) * 1975-05-16 1976-06-01 Grumman Aerospace Corporation Means to reduce and/or eliminate vortices, caused by wing body combinations
US4067518A (en) * 1976-05-20 1978-01-10 Lockheed Corporation Drag reducer for lift surface of aircraft
US4712750A (en) * 1986-05-02 1987-12-15 The Boeing Company Temperature control device for jet engine nacelle associated structure
US4867394A (en) * 1988-06-23 1989-09-19 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Compression pylon
GB8928038D0 (en) 1989-12-12 1990-02-14 British Aerospace Aircraft wing pylon extensions for minimised aerodymanic penalties

Also Published As

Publication number Publication date
FR2802896B1 (fr) 2002-03-29
EP1112929B1 (de) 2003-12-03
US6378804B1 (en) 2002-04-30
ES2207472T3 (es) 2004-06-01
CA2327374A1 (fr) 2001-06-27
CA2327374C (fr) 2008-10-21
EP1112929A1 (de) 2001-07-04
DE60006925T2 (de) 2004-10-28
FR2802896A1 (fr) 2001-06-29

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