FR2100606B1 - - Google Patents

Info

Publication number
FR2100606B1
FR2100606B1 FR707042824A FR7042824A FR2100606B1 FR 2100606 B1 FR2100606 B1 FR 2100606B1 FR 707042824 A FR707042824 A FR 707042824A FR 7042824 A FR7042824 A FR 7042824A FR 2100606 B1 FR2100606 B1 FR 2100606B1
Authority
FR
France
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
FR707042824A
Other versions
FR2100606A1 (fr
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.)
Vereinigte Flugtechnische Werke Fokker GmbH
Original Assignee
Vereinigte Flugtechnische Werke Fokker GmbH
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
Priority claimed from DE19691960005 external-priority patent/DE1960005B/de
Application filed by Vereinigte Flugtechnische Werke Fokker GmbH filed Critical Vereinigte Flugtechnische Werke Fokker GmbH
Publication of FR2100606A1 publication Critical patent/FR2100606A1/fr
Application granted granted Critical
Publication of FR2100606B1 publication Critical patent/FR2100606B1/fr
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02Aircraft characterised by the type or position of power plant
    • B64D27/16Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • B64D27/40
    • B64D27/404

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)
  • Tires In General (AREA)
FR707042824A 1969-11-29 1970-11-27 Expired FR2100606B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19691960005 DE1960005B (de) 1969-11-29 Aufhängung eines Triebwerkes an einem Luftfahrzeug

Publications (2)

Publication Number Publication Date
FR2100606A1 FR2100606A1 (fr) 1972-03-24
FR2100606B1 true FR2100606B1 (fr) 1974-07-12

Family

ID=5752467

Family Applications (1)

Application Number Title Priority Date Filing Date
FR707042824A Expired FR2100606B1 (fr) 1969-11-29 1970-11-27

Country Status (4)

Country Link
US (1) US3727862A (fr)
JP (1) JPS5511560B1 (fr)
FR (1) FR2100606B1 (fr)
GB (1) GB1328410A (fr)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1411601A (en) * 1972-03-04 1975-10-29 Rolls Royce Ducted fan gas turbine engine supported by an aircraft wing mainspar
US3809340A (en) * 1972-12-26 1974-05-07 A Dolgy Devices for mounting an engine on an aircraft pylon
US3907220A (en) * 1974-03-14 1975-09-23 United Aircraft Corp Rear engine redundant mount
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
US4603822A (en) * 1983-12-08 1986-08-05 The Boeing Company Aft engine mount
US5028001A (en) * 1987-03-13 1991-07-02 General Electric Company Method of vibration isolating an aircraft engine
US4875655A (en) * 1987-03-13 1989-10-24 General Electric Company Vibration isolating engine mount
US4776533A (en) * 1987-03-20 1988-10-11 The Jepson Burns Corporation Aircraft seat track fitting assembly
US4805851A (en) * 1987-08-10 1989-02-21 Herbst Paul T Turbine engine mounting bracket assembly
US4917331A (en) * 1988-11-10 1990-04-17 The Boeing Company Apparatus and methods for reducing aircraft lifting surface flutter
US5351930A (en) * 1992-08-11 1994-10-04 Lord Corporation Mounting for engines and the like
FR2738034B1 (fr) * 1995-08-23 1997-09-19 Snecma Dispositif de suspension d'un turbopropulseur
JP3714722B2 (ja) * 1996-05-09 2005-11-09 本田技研工業株式会社 剥離抑制装置
US6328293B1 (en) 1998-09-18 2001-12-11 Lord Corporation Multi-linkage suspension system including outboard isolators
JP3980775B2 (ja) 1998-10-28 2007-09-26 本田技研工業株式会社 飛行機の造波抵抗低減方法
EP0995674B1 (fr) 1998-10-19 2003-08-20 Honda Giken Kogyo Kabushiki Kaisha Procédé pour la réduction de la résistance d'onde sur des avions
JP2000118500A (ja) 1998-10-19 2000-04-25 Honda Motor Co Ltd 飛行機の造波抵抗低減方法
GB2375513B (en) 2001-05-19 2005-03-23 Rolls Royce Plc A mounting arrangement for a gas turbine engine
FR2872784B1 (fr) * 2004-07-09 2007-10-12 Eurocopter France Systeme de suspension d'un moteur d'aeronef a voilure tournante
FR2873986B1 (fr) * 2004-08-04 2007-12-21 Airbus France Sas Ensemble moteur pour aeronef
US7878448B2 (en) 2005-04-04 2011-02-01 Lord Corporation Aircraft auxiliary power unit suspension system for isolating an aircraft auxiliary power unit
US8628040B2 (en) 2006-01-30 2014-01-14 The Boeing Company Aircraft configuration
US8016233B2 (en) * 2006-01-30 2011-09-13 The Boeing Company Aircraft configuration
JP4657192B2 (ja) * 2006-11-08 2011-03-23 本田技研工業株式会社 飛行機の主翼構造
US7900865B2 (en) 2006-12-19 2011-03-08 The Boeing Company Airplane configuration
CA2913375A1 (fr) * 2007-10-19 2009-04-30 Lord Corporation Systeme de suspension pour groupe auxiliaire d'energie d'avion muni d'un element elastomere
US7784773B1 (en) 2009-08-04 2010-08-31 Itt Manufacturing Enterprises, Inc. Isolator useful for in-line mounting with a strut
US20130232768A1 (en) 2012-03-12 2013-09-12 United Technologies Corporation Turbine engine case mount and dismount
EP2641831B1 (fr) * 2012-03-22 2014-12-24 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Atterrisseur à patins pour un giravion
US10384790B2 (en) * 2016-02-01 2019-08-20 Bell Textron Inc. Engine mount assemblies for aircraft
US10220951B2 (en) * 2016-02-01 2019-03-05 Bell Helicopter Textron Inc. Sleeved bolt assemblies for aircraft engine mount assemblies
CN208170542U (zh) 2017-12-25 2018-11-30 广东志高暖通设备股份有限公司 一种空调窗机及其风门组件
US10814995B2 (en) * 2017-08-29 2020-10-27 Spirit Aerosystems, Inc. High-mounted aircraft nacelle
US20220136440A1 (en) 2020-10-30 2022-05-05 Raytheon Technologies Corporation Gas turbine engine mounted above wing and with camber
US11613372B2 (en) * 2020-11-09 2023-03-28 Rohr, Inc. Ducted fan case attachment structure

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4C (de) * 1877-07-05 J. E. CHRISTOPH zu Niesky Kontinuirlicher Maischdestillirapparat mit eigenthümlicher Maisch- u. Spirituskolonne, neuem Maischregulator und neuem Schlemperegulator
DE89C (de) * 1877-08-02 Deutsche Werkzeugmaschinen -Fabrik, vormals SONDERMANN & STIER in Chemnitz Fleisch-Hackmaschine
FR838666A (fr) * 1937-11-23 1939-03-13 Perfectionnement à la suspension des moteurs d'avions et autres organes sur des supports soumis à des mouvements alternatifs et notamment les ailes
US2761638A (en) * 1953-11-17 1956-09-04 Gordon L Getline Vibration-isolating power plant mounting system
US3057582A (en) * 1959-05-12 1962-10-09 Rolls Royce Improved engine mounting
US3288404A (en) * 1964-08-24 1966-11-29 Lord Corp Engine mounting system

Also Published As

Publication number Publication date
US3727862A (en) 1973-04-17
FR2100606A1 (fr) 1972-03-24
GB1328410A (en) 1973-08-30
JPS5511560B1 (fr) 1980-03-26
DE1960005A1 (de) 1971-06-09

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Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property
ST Notification of lapse