DE69511682T2 - Sicherheitseinrichtung für ein Triebwerks-Aufhängungssystem - Google Patents

Sicherheitseinrichtung für ein Triebwerks-Aufhängungssystem

Info

Publication number
DE69511682T2
DE69511682T2 DE69511682T DE69511682T DE69511682T2 DE 69511682 T2 DE69511682 T2 DE 69511682T2 DE 69511682 T DE69511682 T DE 69511682T DE 69511682 T DE69511682 T DE 69511682T DE 69511682 T2 DE69511682 T2 DE 69511682T2
Authority
DE
Germany
Prior art keywords
safety device
suspension system
engine suspension
engine
safety
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
DE69511682T
Other languages
English (en)
Other versions
DE69511682D1 (de
Inventor
Kenneth E Hey
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 DE69511682D1 publication Critical patent/DE69511682D1/de
Publication of DE69511682T2 publication Critical patent/DE69511682T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B64D27/40—
    • B64D27/404—
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C11/00—Pivots; Pivotal connections
    • F16C11/04—Pivotal connections
    • F16C11/045—Pivotal connections with at least a pair of arms pivoting relatively to at least one other arm, all arms being mounted on one pin
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00—Articles relating to transporting
    • F16C2326/43—Aeroplanes; Helicopters
    • 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
    • Y02T50/40—Weight reduction
DE69511682T 1995-03-24 1995-11-08 Sicherheitseinrichtung für ein Triebwerks-Aufhängungssystem Expired - Lifetime DE69511682T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/410,487 US5649417A (en) 1995-03-24 1995-03-24 Fail-safe engine mount system

Publications (2)

Publication Number Publication Date
DE69511682D1 DE69511682D1 (de) 1999-09-30
DE69511682T2 true DE69511682T2 (de) 1999-12-23

Family

ID=23624941

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69511682T Expired - Lifetime DE69511682T2 (de) 1995-03-24 1995-11-08 Sicherheitseinrichtung für ein Triebwerks-Aufhängungssystem

Country Status (5)

Country Link
US (1) US5649417A (de)
EP (1) EP0744338B1 (de)
DE (1) DE69511682T2 (de)
RU (1) RU2167788C2 (de)
UA (1) UA44706C2 (de)

Families Citing this family (55)

* Cited by examiner, † Cited by third party
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US5860623A (en) * 1995-05-03 1999-01-19 The Boeing Company Three link failsafe engine mount
US5927644A (en) * 1997-10-08 1999-07-27 General Electric Company Double failsafe engine mount
US5921500A (en) * 1997-10-08 1999-07-13 General Electric Company Integrated failsafe engine mount
FR2774358B1 (fr) 1998-02-04 2000-04-21 Aerospatiale Dispositif d'accrochage d'un moteur d'aeronef
US6170252B1 (en) 1998-12-14 2001-01-09 United Technologies Corporation Locator for a gearbox mount
US6212974B1 (en) 1998-12-17 2001-04-10 United Technologies Corporation Variable stiffness positioning link for a gearbox
FR2793767B1 (fr) * 1999-05-17 2001-09-21 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef
FR2799432A1 (fr) * 1999-10-07 2001-04-13 Snecma Suspension a securite integree pour groupes motopropulseurs d'aeronefs
GB9927425D0 (en) * 1999-11-20 2000-01-19 Rolls Royce Plc A gas turbine engine mounting arrangement
US6330995B1 (en) * 2000-02-29 2001-12-18 General Electric Company Aircraft engine mount
FR2818614B1 (fr) 2000-12-21 2003-01-31 Snecma Moteurs Piece de suspension d'un turboreacteur
FR2828167B1 (fr) * 2001-07-31 2003-11-21 Airbus France Dispositif d'accrochage d'un moteur sur un aeronef
US6517027B1 (en) * 2001-12-03 2003-02-11 Pratt & Whitney Canada Corp. Flexible/fixed support for engine cowl
FR2855494B1 (fr) * 2003-05-27 2006-09-22 Snecma Moteurs Dispositif d'accrocharge arriere de moteur d'avion
FR2855495B1 (fr) * 2003-05-27 2006-11-24 Snecma Moteurs Dispositif d'accrochage avant 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
US6843449B1 (en) * 2004-02-09 2005-01-18 General Electric Company Fail-safe aircraft engine mounting system
FR2867155B1 (fr) * 2004-03-08 2007-06-29 Snecma Moteurs Suspension d'un moteur a la structure d'un avion
FR2868041B1 (fr) * 2004-03-25 2006-05-26 Snecma Moteurs Sa Suspension d'un moteur d'avion
FR2869874B1 (fr) * 2004-05-04 2006-06-23 Snecma Moteurs Sa Moteur d'avion avec des moyens de suspension a la structure d'un avion
FR2883839B1 (fr) * 2005-03-29 2007-06-29 Snecma Moteurs Sa Suspension arriere de turboreacteur
GB0507721D0 (en) 2005-04-16 2005-05-25 Rolls Royce Plc Gas turbine engine mounting arrangement
FR2887853B1 (fr) * 2005-06-29 2007-08-17 Airbus France Sas Attache moteur pour aeronef destinee a etre interposee entre un moteur et un mat d'accrochage
FR2891245B1 (fr) * 2005-09-26 2007-10-26 Airbus France Sas Procede de montage d'un moteur d'aeronef sur une structure rigide d'un mat d'accrochage du moteur
GB0603539D0 (en) * 2006-02-22 2006-04-05 Airbus Uk Ltd Control surface failsafe drop link
DE102006027707A1 (de) 2006-06-14 2007-12-20 Airbus Deutschland Gmbh Heckstruktur für ein Luft- oder Raumfahrzeug
FR2905932B1 (fr) * 2006-09-20 2008-12-05 Airbus France Sa Agencement pour attache de dispositif d'accrochage d'un moteur d'aeronef
US7810239B2 (en) * 2006-10-23 2010-10-12 United Technologies Corporation Engine mount bearing sleeve repair
FR2931800B1 (fr) * 2008-05-29 2010-07-30 Airbus France Dispositif de reprise des efforts de poussee pour mat d'accrochage de moteur d'aeronef, comprenant des bielles laterales a butees de palonnier integrees
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
US8342444B2 (en) * 2008-12-16 2013-01-01 The Boeing Company Fail safe extended torque box strut-to-wing mount
GB2466297B (en) 2008-12-22 2010-11-10 Rolls Royce Plc Catcher pin assembly
US20100189502A1 (en) * 2009-01-22 2010-07-29 Basta Samuel T Watercraft lift system
EP2580119B1 (de) * 2010-06-14 2017-03-08 LORD Corporation System und verfahren zur montage eines hubschraubermotors
FR2966125B1 (fr) * 2010-10-15 2013-04-26 Aircelle Sa Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aeronef
US9211955B1 (en) * 2012-12-10 2015-12-15 The Boeing Company Methods and apparatus for supporting engines and nacelles relative to aircraft wings
US9365278B2 (en) * 2013-01-21 2016-06-14 The Boeing Company Variation compensating assembly
FR3001714B1 (fr) * 2013-02-05 2016-08-26 Astrium Sas Dispositif de support et de maintien de reservoirs cryogeniques
WO2014189588A2 (en) * 2013-03-15 2014-11-27 United Technologies Corporation Engine mount waiting fail safe lug joint with reduced dynamic amplification factor
FR3003896B1 (fr) * 2013-03-29 2015-03-20 Snecma Dispositif d'articulation a rotule pour la suspension d'une turbomachine a un pylone ou la suspension d'un equipement au corps de la turbomachine
GB201314667D0 (en) * 2013-08-16 2013-10-02 Rolls Royce Plc A panel attachment system
US10059412B1 (en) 2014-04-11 2018-08-28 Basta Inc. Boat lift systems and methods
CN107108039B (zh) 2015-01-07 2019-08-30 洛德公司 飞行器发动机安装架
US10598211B2 (en) * 2016-05-23 2020-03-24 United Technologies Corporation Spherical bearing sleeve configured with one or more discrete collars
US10570950B2 (en) 2016-05-23 2020-02-25 United Technologies Corporation Spherical joint assembly with a spherical bearing between integral collars
US10858083B1 (en) 2017-01-22 2020-12-08 Basta Ip Inc. Bunk mounting systems and methods for watercraft lifts
FR3073823B1 (fr) * 2017-11-21 2019-11-08 Airbus Operations Attache moteur arriere pour un moteur d'aeronef
FR3075175B1 (fr) * 2017-12-20 2019-12-13 Safran Aircraft Engines Dispositif de suspension
USD892025S1 (en) * 2018-07-23 2020-08-04 Caterpillar Inc. Filter bracket
FR3091520A1 (fr) * 2019-01-09 2020-07-10 Airbus Operations (S.A.S.) Attache-moteur d’aéronef comprenant au moins un système d’immobilisation en translation d’un pion de cisaillement comportant une plaque d’obturation, procédé de montage de ladite attache-moteur et aéronef comprenant ladite attache-moteur
FR3091519A1 (fr) 2019-01-09 2020-07-10 Airbus Operations (S.A.S.) Attache-moteur d’aéronef comprenant au moins un système d’immobilisation en translation de type fourchette d’un pion de cisaillement, procédé de montage de ladite attache-moteur et aéronef comprenant ladite attache-moteur
US11820510B2 (en) * 2019-03-26 2023-11-21 Yaborã Industria Aeronautica S.A. Quickly adjustable fail-safe link bar assemblies especially useful for connecting structural components of an aircraft
US11479104B2 (en) 2019-07-24 2022-10-25 Honeywell International Inc. System and method for gas turbine engine mount with seal
US11549554B2 (en) * 2020-04-16 2023-01-10 General Electric Company Bearings with visually distinct wear indicators
FR3128205A1 (fr) * 2021-10-14 2023-04-21 Airbus Operations Assemblage d’un mat avec un moteur d’un aéronef

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1236917A (en) * 1967-06-14 1971-06-23 Rolls Royce Improvements in or relating to means for supporting a gas turbine engine in an aircraft
US4055041A (en) * 1974-11-08 1977-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Integrated gas turbine engine-nacelle
EP0164352B1 (de) * 1983-12-08 1987-11-19 The Boeing Company Triebwerkshinteraufhängung
US4717094A (en) * 1986-05-19 1988-01-05 The Boeing Company Aircraft engine mount system with vibration isolators
FR2599708A1 (fr) * 1986-06-10 1987-12-11 Snecma Dispositif d'accrochage arriere de securite d'un turboreacteur sur un mat d'avion
GB2224707B (en) * 1988-11-12 1992-06-10 Rolls Royce Plc Improvements in or relating to engine mounting integrity
DE69012071T2 (de) * 1989-12-05 1995-04-13 Rolls Royce Plc Ausfallsichere Haltevorrichtung für Treibwerke.
FR2680353B1 (fr) * 1991-08-14 1993-10-15 Snecma Structure d'accrochage arriere d'un turboreacteur.
US5174525A (en) * 1991-09-26 1992-12-29 General Electric Company Structure for eliminating lift load bending in engine core of turbofan
GB9125011D0 (en) * 1991-11-25 1992-01-22 Rolls Royce Plc A mounting arrangement for a gas turbine engine
US5275357A (en) * 1992-01-16 1994-01-04 General Electric Company Aircraft engine mount
US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
US5351930A (en) * 1992-08-11 1994-10-04 Lord Corporation Mounting for engines and the like
US5277382A (en) * 1992-10-13 1994-01-11 General Electric Company Aircraft engine forward mount
US5303880A (en) * 1992-10-28 1994-04-19 General Electric Company Aircraft engine pin mount

Also Published As

Publication number Publication date
DE69511682D1 (de) 1999-09-30
UA44706C2 (uk) 2002-03-15
EP0744338A1 (de) 1996-11-27
EP0744338B1 (de) 1999-08-25
US5649417A (en) 1997-07-22
RU2167788C2 (ru) 2001-05-27

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