DE69404867D1 - Flügel/triebwerksgondel-kombination eines flugzeuges - Google Patents

Flügel/triebwerksgondel-kombination eines flugzeuges

Info

Publication number
DE69404867D1
DE69404867D1 DE69404867T DE69404867T DE69404867D1 DE 69404867 D1 DE69404867 D1 DE 69404867D1 DE 69404867 T DE69404867 T DE 69404867T DE 69404867 T DE69404867 T DE 69404867T DE 69404867 D1 DE69404867 D1 DE 69404867D1
Authority
DE
Germany
Prior art keywords
airplane
wing
combination
engine gondola
gondola
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
DE69404867T
Other languages
English (en)
Other versions
DE69404867T2 (de
Inventor
Wesley Lord
Andrea Karalus
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DE69404867D1 publication Critical patent/DE69404867D1/de
Publication of DE69404867T2 publication Critical patent/DE69404867T2/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)
  • Wind Motors (AREA)
DE69404867T 1993-12-21 1994-11-30 Flügel/triebwerksgondel-kombination eines flugzeuges Expired - Lifetime DE69404867T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/171,301 US5443230A (en) 1993-12-21 1993-12-21 Aircraft wing/nacelle combination
PCT/US1994/013774 WO1995017334A1 (en) 1993-12-21 1994-11-30 Aircraft wing/nacelle combination

Publications (2)

Publication Number Publication Date
DE69404867D1 true DE69404867D1 (de) 1997-09-11
DE69404867T2 DE69404867T2 (de) 1998-01-22

Family

ID=22623256

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69404867T Expired - Lifetime DE69404867T2 (de) 1993-12-21 1994-11-30 Flügel/triebwerksgondel-kombination eines flugzeuges

Country Status (4)

Country Link
US (1) US5443230A (de)
EP (1) EP0735970B1 (de)
DE (1) DE69404867T2 (de)
WO (1) WO1995017334A1 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3714722B2 (ja) * 1996-05-09 2005-11-09 本田技研工業株式会社 剥離抑制装置
US5934607A (en) * 1997-01-21 1999-08-10 Lockheed Martin Corporation Shock suppression supersonic aircraft
US6588703B1 (en) 2000-02-08 2003-07-08 Lockheed Martin Corporation Passive aerodynamic sonic boom suppression for supersonic aircraft
GB2359052B (en) * 2000-02-09 2003-09-17 Rolls Royce Plc Engine arrangement
FR2899201B1 (fr) * 2006-03-31 2009-02-13 Airbus France Sas Agencement d'aile d'aeronef comportant un mat d'accrochage de moteur definissant en zone avant un canal lateral d'ecoulement d'air
FR2901538B1 (fr) * 2006-05-23 2008-07-18 Airbus France Sas Aeronef comportant un dispositif de reduction de la trainee induite
US7798875B1 (en) 2006-10-20 2010-09-21 Brunswick Corporation Helical marine strut
US7770841B2 (en) * 2006-12-22 2010-08-10 Calvin Burgess Inverted airfoil pylon for an aircraft
US8950702B2 (en) * 2008-01-18 2015-02-10 United Technologies Corporation Pylon and engine mount configuration
FR2935353B1 (fr) * 2008-09-03 2010-09-10 Airbus France Mat pour la suspension d'un turbomoteur sous une aile d'aeronef
DE102009033554A1 (de) * 2009-07-16 2011-01-20 Reintjes Gmbh Propellergondel
GB201011056D0 (en) 2010-07-01 2010-08-18 Rolls Royce Plc Pylon for attaching a gas turbine engine
US8727275B2 (en) 2012-01-27 2014-05-20 Rohr, Inc. Nacelle
CN103612746B (zh) 2013-10-24 2016-09-21 中国商用飞机有限责任公司 翼吊布局飞机中吊挂的整流罩结构
US9908631B2 (en) 2015-11-30 2018-03-06 Embraer S.A. Optimized aircraft pylon fairing
CA3084384A1 (en) * 2017-10-19 2019-04-25 Bombardier Inc. Aircraft pylon fairing
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
US20240060430A1 (en) * 2022-08-17 2024-02-22 General Electric Company Gas turbine engine

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1990606A (en) * 1930-10-11 1935-02-12 Firm Junkers Motorenbau G M B Shafting for power transmission
GB1118340A (en) * 1966-12-30 1968-07-03 Rolls Royce Mounting means for an aircraft engine
US4449683A (en) * 1979-01-03 1984-05-22 The Boeing Company Aerodynamically contoured, low drag wing engine and engine nacelle combination
GB8321281D0 (en) * 1983-08-06 1983-09-28 British Aerospace Underwing engine installation
FR2555960B1 (fr) * 1983-12-06 1986-09-19 Aerospatiale Aile d'aeronef en fleche pourvue d'un systeme hypersustentateur et d'un mat de suspension de moteur, ainsi que mat de suspension de moteur pour une telle aile
US4801058A (en) * 1987-02-05 1989-01-31 Rolls-Royce Plc Aircraft and powerplant combinations
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

Also Published As

Publication number Publication date
DE69404867T2 (de) 1998-01-22
US5443230A (en) 1995-08-22
EP0735970A1 (de) 1996-10-09
EP0735970B1 (de) 1997-08-06
WO1995017334A1 (en) 1995-06-29

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