DE60029502D1 - Abgestimmte Jettriebwerks- Befestigungsvorrichtung - Google Patents

Abgestimmte Jettriebwerks- Befestigungsvorrichtung

Info

Publication number
DE60029502D1
DE60029502D1 DE60029502T DE60029502T DE60029502D1 DE 60029502 D1 DE60029502 D1 DE 60029502D1 DE 60029502 T DE60029502 T DE 60029502T DE 60029502 T DE60029502 T DE 60029502T DE 60029502 D1 DE60029502 D1 DE 60029502D1
Authority
DE
Germany
Prior art keywords
tuned
attachment device
jet engine
engine attachment
jet
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
DE60029502T
Other languages
English (en)
Other versions
DE60029502T2 (de
Inventor
James R Schnelz
Donald T Powell
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of DE60029502D1 publication Critical patent/DE60029502D1/de
Publication of DE60029502T2 publication Critical patent/DE60029502T2/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
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)
DE60029502T 1999-02-26 2000-01-27 Abgestimmtes Triebwerkhalterungssystem für ein Düsenflugzeug Expired - Lifetime DE60029502T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US259092 1999-02-26
US09/259,092 US6189830B1 (en) 1999-02-26 1999-02-26 Tuned engine mounting system for jet aircraft

Publications (2)

Publication Number Publication Date
DE60029502D1 true DE60029502D1 (de) 2006-09-07
DE60029502T2 DE60029502T2 (de) 2007-02-22

Family

ID=22983496

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60029502T Expired - Lifetime DE60029502T2 (de) 1999-02-26 2000-01-27 Abgestimmtes Triebwerkhalterungssystem für ein Düsenflugzeug

Country Status (3)

Country Link
US (1) US6189830B1 (de)
EP (1) EP1031507B1 (de)
DE (1) DE60029502T2 (de)

Families Citing this family (46)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2799432A1 (fr) * 1999-10-07 2001-04-13 Snecma Suspension a securite integree pour groupes motopropulseurs d'aeronefs
FR2818614B1 (fr) * 2000-12-21 2003-01-31 Snecma Moteurs Piece de suspension d'un turboreacteur
ITMI20011060A1 (it) 2001-05-22 2002-11-22 Ausimont Spa Composizioni fluoroelastomeriche
FR2825976B1 (fr) * 2001-06-13 2003-09-05 Eads Airbus Sa Dispositif de reprise d'efforts generes par un moteur d'aeronef
FR2828167B1 (fr) * 2001-07-31 2003-11-21 Airbus France Dispositif d'accrochage d'un moteur sur un aeronef
US6915989B2 (en) 2002-05-01 2005-07-12 The Boeing Company Aircraft multi-axis modal suppression system
FR2855495B1 (fr) * 2003-05-27 2006-11-24 Snecma Moteurs Dispositif d'accrochage avant de moteur d'avion
FR2855494B1 (fr) * 2003-05-27 2006-09-22 Snecma Moteurs Dispositif d'accrocharge arriere de moteur d'avion
FR2862612B1 (fr) * 2003-11-25 2006-02-17 Airbus France Dispositif d'accrochage d'un moteur sous une voilure d'aeronef
FR2867155B1 (fr) * 2004-03-08 2007-06-29 Snecma Moteurs Suspension d'un moteur a la structure d'un avion
US7617166B2 (en) * 2004-04-14 2009-11-10 The Boeing Company Neural network for aeroelastic analysis
ITMI20041253A1 (it) 2004-06-22 2004-09-22 Solvay Solexis Spa Gel di fluoroelastomeri
FR2873985B1 (fr) * 2004-08-04 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
FR2883839B1 (fr) * 2005-03-29 2007-06-29 Snecma Moteurs Sa Suspension arriere de turboreacteur
US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
FR2887851B1 (fr) 2005-06-29 2007-08-17 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2887852B1 (fr) * 2005-06-29 2007-08-17 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891253B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Attache arriere d'un moteur d'aeronef a deux manilles
FR2891803B1 (fr) * 2005-10-07 2007-11-30 Airbus France Sas Structure rigide pour mat d'accrochage de moteur d'aeronef, et mat comportant une telle structure
FR2894934B1 (fr) * 2005-12-15 2009-11-13 Airbus France Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente
US11242805B2 (en) 2007-08-01 2022-02-08 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11346289B2 (en) 2007-08-01 2022-05-31 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US8256707B2 (en) * 2007-08-01 2012-09-04 United Technologies Corporation Engine mounting configuration for a turbofan gas turbine engine
US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11149650B2 (en) 2007-08-01 2021-10-19 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US20150377123A1 (en) 2007-08-01 2015-12-31 United Technologies Corporation Turbine section of high bypass turbofan
US8844265B2 (en) 2007-08-01 2014-09-30 United Technologies Corporation Turbine section of high bypass turbofan
FR2920138B1 (fr) 2007-08-24 2010-03-12 Airbus France Dispositif d'accrochage de moteur d'aeronef comportant un dispositif de reprise des efforts de poussee a encombrement reduit
US8118251B2 (en) * 2008-01-18 2012-02-21 United Technologies Corporation Mounting system for a gas turbine engine
US8167237B2 (en) 2008-03-21 2012-05-01 United Technologies Corporation Mounting system for a gas turbine engine
US8128021B2 (en) * 2008-06-02 2012-03-06 United Technologies Corporation Engine mount system for a turbofan gas turbine engine
US20140174056A1 (en) 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8695920B2 (en) 2008-06-02 2014-04-15 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8807477B2 (en) 2008-06-02 2014-08-19 United Technologies Corporation Gas turbine engine compressor arrangement
US8800914B2 (en) 2008-06-02 2014-08-12 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8511605B2 (en) 2008-06-02 2013-08-20 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
FR2966125B1 (fr) * 2010-10-15 2013-04-26 Aircelle Sa Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aeronef
US20130074517A1 (en) * 2011-09-23 2013-03-28 United Technologies Corporation Gas turbine engine mount assembly
US9388875B2 (en) * 2011-10-18 2016-07-12 The Boeing Company Aeroelastic tuned mass damper
US9410441B2 (en) 2012-09-13 2016-08-09 Pratt & Whitney Canada Corp. Turboprop engine with compressor turbine shroud
WO2014055102A1 (en) * 2012-10-01 2014-04-10 United Technologies Corporation Low weight large fan gas turbine engine
US10266273B2 (en) 2013-07-26 2019-04-23 Mra Systems, Llc Aircraft engine pylon
EP3058202A4 (de) 2013-10-16 2017-06-28 United Technologies Corporation Turbogebläsemotor mit gezielter modularer wirkung
US11273923B2 (en) * 2019-07-12 2022-03-15 Spirit Aerosystems, Inc. Fail-safe engine support system
FR3103465A1 (fr) * 2019-11-27 2021-05-28 Airbus Operations Systeme d’attache moteur avant pour un moteur d’aeronef qui comporte une structure allegee
US11560840B2 (en) * 2020-10-16 2023-01-24 General Electric Company Damper engine mount links

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2891743A (en) * 1954-06-08 1959-06-23 Textron Inc Airplane engine suspension and mounts therefor
GB2010969A (en) * 1977-12-22 1979-07-04 Rolls Royce Mounting for Gas Turbine Jet Propulsion Engine
GB8300748D0 (en) * 1983-01-12 1983-02-16 British Aerospace Power plant attachment for aircraft wings
US4717094A (en) * 1986-05-19 1988-01-05 The Boeing Company Aircraft engine mount system with vibration isolators
US4917331A (en) 1988-11-10 1990-04-17 The Boeing Company Apparatus and methods for reducing aircraft lifting surface flutter
US5054715A (en) 1988-11-10 1991-10-08 The Boeing Company Apparatus and methods for reducing aircraft lifting surface flutter
US5065959A (en) 1989-11-21 1991-11-19 The Boeing Company Vibration damping aircraft engine attachment
FR2676707B1 (fr) * 1991-05-23 1993-08-13 Snecma Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux.
FR2680353B1 (fr) * 1991-08-14 1993-10-15 Snecma Structure d'accrochage arriere d'un turboreacteur.
US5687948A (en) 1995-09-26 1997-11-18 Lord Corporation Vibration isolation system including a passive tuned vibration absorber
FR2755944B1 (fr) * 1996-11-21 1998-12-24 Snecma Suspension avant redondante pour turbomachine

Also Published As

Publication number Publication date
US6189830B1 (en) 2001-02-20
EP1031507B1 (de) 2006-07-26
DE60029502T2 (de) 2007-02-22
EP1031507A2 (de) 2000-08-30
EP1031507A3 (de) 2001-02-28

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition