FR2326327A1 - Suspension pour groupes motopropulseur aux aeronefs - Google Patents

Suspension pour groupes motopropulseur aux aeronefs

Info

Publication number
FR2326327A1
FR2326327A1 FR7630408A FR7630408A FR2326327A1 FR 2326327 A1 FR2326327 A1 FR 2326327A1 FR 7630408 A FR7630408 A FR 7630408A FR 7630408 A FR7630408 A FR 7630408A FR 2326327 A1 FR2326327 A1 FR 2326327A1
Authority
FR
France
Prior art keywords
suspension
powertrains
aircraft
aircraft powertrains
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.)
Granted
Application number
FR7630408A
Other languages
English (en)
Other versions
FR2326327B1 (fr
Inventor
Edmund Mahler
Wolfgang Steinkuhler
Rene Imbert
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.)
Dornier GmbH
Original Assignee
Dornier 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
Application filed by Dornier GmbH filed Critical Dornier GmbH
Publication of FR2326327A1 publication Critical patent/FR2326327A1/fr
Application granted granted Critical
Publication of FR2326327B1 publication Critical patent/FR2326327B1/fr
Granted 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
    • B64D27/40—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)
  • Mounting Of Bearings Or Others (AREA)
  • Jib Cranes (AREA)
FR7630408A 1975-10-03 1976-10-01 Suspension pour groupes motopropulseur aux aeronefs Granted FR2326327A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2544272A DE2544272C3 (de) 1975-10-03 1975-10-03 Triebwerksaufhängung an Luftfahrzeugen

Publications (2)

Publication Number Publication Date
FR2326327A1 true FR2326327A1 (fr) 1977-04-29
FR2326327B1 FR2326327B1 (fr) 1980-12-05

Family

ID=5958215

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7630408A Granted FR2326327A1 (fr) 1975-10-03 1976-10-01 Suspension pour groupes motopropulseur aux aeronefs

Country Status (4)

Country Link
US (1) US4079981A (fr)
DE (1) DE2544272C3 (fr)
FR (1) FR2326327A1 (fr)
GB (1) GB1507415A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0018252A1 (fr) * 1979-04-09 1980-10-29 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Dispositif de suspension d'un groupe propulsif à une cellule d'avion, outillage et procédé pour la mise en oeuvre
EP1090838A1 (fr) * 1999-10-07 2001-04-11 Snecma Moteurs Suspension à sécurité intégrée pour groupes motopropulseurs d'aéronefs

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5064144A (en) * 1987-05-19 1991-11-12 The Boeing Company Engine mounting assembly
FR2635751B1 (fr) * 1988-09-01 1991-01-04 Snecma Dispositif de fixation d'une biellette de suspension d'un turboreacteur
FR2694537B1 (fr) * 1992-08-06 1994-10-28 Aerospatiale Dispositif d'accrochage d'une turbomachine sur une structure d'aéronef.
US5379970A (en) * 1993-04-02 1995-01-10 General Electric Company Mounting bracket arrangement
US6095456A (en) * 1996-12-23 2000-08-01 The Boeing Company Strut-wing interface having dual upper links
US6126110A (en) * 1997-12-22 2000-10-03 Mcdonnell Douglas Corporation Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon
FR2890377B1 (fr) * 2005-09-05 2007-10-05 Airbus France Sas Agencement adapte pour raccorder un palonnier a un mat d'accrochage de moteur d'aeronef
FR2924094B1 (fr) * 2007-11-23 2010-01-15 Snecma Turboreacteur suspendu a un pylone d'aeronef
FR2928347B1 (fr) * 2008-03-07 2010-06-25 Aircelle Sa Structure d'accrochage pour turboreacteur
US9157394B2 (en) * 2012-08-15 2015-10-13 United Technologies Corporation Adjustable cable for exhaust duct liner hanger
CN104176624B (zh) * 2013-05-22 2016-01-20 亿和塑胶电子制品(深圳)有限公司 一种起吊装夹器
FR3014996B1 (fr) * 2013-12-16 2016-11-04 Microturbo Suspension d'un element tubulaire dans un compartiment d'aeronef
US10472079B2 (en) * 2014-05-02 2019-11-12 Sikorsky Aircraft Corporation Articulated mounts
DE102017129060A1 (de) * 2017-12-06 2019-06-06 Rolls-Royce Deutschland Ltd & Co Kg Integrierte Tragstruktur für ein Flugzeugtriebwerk und dessen Zubehörkomponenten
FR3086925B1 (fr) * 2018-10-08 2020-09-11 Safran Aircraft Engines Ensemble de suspension pour une turbomachine

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2815184A (en) * 1954-04-02 1957-12-03 Northrop Aircraft Inc Aircraft engine hoist and mounting system

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2349717A (en) * 1943-07-13 1944-05-23 Hinckley Myers Division Of Ken Work sling
US2703252A (en) * 1952-04-02 1955-03-01 Rohr Aircraft Corp Multiple tilting arc support

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2815184A (en) * 1954-04-02 1957-12-03 Northrop Aircraft Inc Aircraft engine hoist and mounting system

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0018252A1 (fr) * 1979-04-09 1980-10-29 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Dispositif de suspension d'un groupe propulsif à une cellule d'avion, outillage et procédé pour la mise en oeuvre
FR2453779A1 (fr) * 1979-04-09 1980-11-07 Snecma Dispositif de suspension d'un groupe propulsif a une cellule d'avion, outillage et procede pour la mise en oeuvre
US4346861A (en) * 1979-04-09 1982-08-31 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Apparatus for hanging a propulsion unit on an aircraft cell, tooling and process for using same
EP1090838A1 (fr) * 1999-10-07 2001-04-11 Snecma Moteurs Suspension à sécurité intégrée pour groupes motopropulseurs d'aéronefs
FR2799432A1 (fr) * 1999-10-07 2001-04-13 Snecma Suspension a securite integree pour groupes motopropulseurs d'aeronefs
US6474596B1 (en) 1999-10-07 2002-11-05 Snecma Moteurs Suspension system with intrinsic safety features for aircraft powerplants

Also Published As

Publication number Publication date
GB1507415A (en) 1978-04-12
US4079981A (en) 1978-03-21
DE2544272C3 (de) 1979-02-22
DE2544272B2 (de) 1978-07-06
FR2326327B1 (fr) 1980-12-05
DE2544272A1 (de) 1977-04-14

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Legal Events

Date Code Title Description
ST Notification of lapse