BE841225A - Systeme de montage d'un moteur sur la structure d'un avion - Google Patents

Systeme de montage d'un moteur sur la structure d'un avion

Info

Publication number
BE841225A
BE841225A BE166521A BE166521A BE841225A BE 841225 A BE841225 A BE 841225A BE 166521 A BE166521 A BE 166521A BE 166521 A BE166521 A BE 166521A BE 841225 A BE841225 A BE 841225A
Authority
BE
Belgium
Prior art keywords
aircraft
engine
mounting
Prior art date
Application number
BE166521A
Other languages
English (en)
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 filed Critical
Publication of BE841225A publication Critical patent/BE841225A/fr

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
    • B64D27/02—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE166521A 1975-04-29 1976-04-28 Systeme de montage d'un moteur sur la structure d'un avion BE841225A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/572,647 US4022018A (en) 1975-04-29 1975-04-29 Mounting system for a thrust generating engine

Publications (1)

Publication Number Publication Date
BE841225A true BE841225A (fr) 1976-08-16

Family

ID=24288755

Family Applications (1)

Application Number Title Priority Date Filing Date
BE166521A BE841225A (fr) 1975-04-29 1976-04-28 Systeme de montage d'un moteur sur la structure d'un avion

Country Status (8)

Country Link
US (1) US4022018A (fr)
JP (1) JPS5950560B2 (fr)
BE (1) BE841225A (fr)
CA (1) CA1038360A (fr)
DE (1) DE2618283A1 (fr)
FR (1) FR2309402A1 (fr)
GB (1) GB1540654A (fr)
IT (1) IT1060001B (fr)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4147029A (en) * 1976-01-02 1979-04-03 General Electric Company Long duct mixed flow gas turbine engine
EP0070578B1 (fr) * 1979-05-01 1989-02-01 Brooklands Aerospace Group Plc Hélice carénée
GB2061389B (en) * 1979-10-23 1983-05-18 Rolls Royce Rod installation for a gas turbine engine
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
GB2129501B (en) * 1982-11-09 1987-07-08 Rolls Royce Gas turbine engine casing
US4658579A (en) * 1983-07-14 1987-04-21 United Technologies Corporation Load sharing for engine nacelle
US4603821A (en) * 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine
DE3408592A1 (de) * 1984-03-09 1985-09-12 Erno Raumfahrttechnik Gmbh, 2800 Bremen Gaserzeugungsanlage, insbesondere fuer orbitalstationen und satelliten
US4805851A (en) * 1987-08-10 1989-02-21 Herbst Paul T Turbine engine mounting bracket assembly
GB2224707B (en) * 1988-11-12 1992-06-10 Rolls Royce Plc Improvements in or relating to engine mounting integrity
FR2661213B1 (fr) * 1990-04-19 1992-07-03 Snecma Moteur d'aviation a tres grand taux de dilution et du type dit contrafan avant.
JPH0472864U (fr) * 1990-10-26 1992-06-26
US5307623A (en) * 1991-05-28 1994-05-03 General Electric Company Apparatus and method for the diassembly of an ultra high bypass engine
FR2694537B1 (fr) * 1992-08-06 1994-10-28 Aerospatiale Dispositif d'accrochage d'une turbomachine sur une structure d'aéronef.
US5319922A (en) * 1992-12-04 1994-06-14 General Electric Company Aircraft gas turbine engine backbone deflection control
FR2698848B1 (fr) * 1992-12-07 1995-03-24 Aerospatiale Balance de poussée pour un moteur d'avion.
US5385013A (en) * 1993-03-03 1995-01-31 General Electric Company Aircraft gas turbine engine backbone deflection thermal control
US5452575A (en) * 1993-09-07 1995-09-26 General Electric Company Aircraft gas turbine engine thrust mount
US5443229A (en) * 1993-12-13 1995-08-22 General Electric Company Aircraft gas turbine engine sideways mount
GB2320525A (en) * 1996-12-18 1998-06-24 British Aerospace Mounting of powerplant in aircraft
DE19713365C1 (de) * 1997-04-01 1998-10-22 Deutsch Zentr Luft & Raumfahrt Triebwerksaufhängung, insbesondere für Propellerflugzeuge, mit einem Stabwerk zur Befestigung eines Triebwerks
GB2407134B (en) * 2003-10-16 2008-04-16 Rolls Royce Plc Aircraft engine mounting assembly
US7083143B2 (en) * 2003-10-17 2006-08-01 The Boeing Company Apparatuses and methods for attaching engines and other structures to aircraft wings
FR2867158B1 (fr) * 2004-03-04 2007-06-08 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
FR2867156B1 (fr) * 2004-03-04 2006-06-02 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
FR2926788B1 (fr) * 2008-01-25 2010-04-02 Snecma Fixation d'un turboreacteur multiflux a un aeronef
US8621874B2 (en) * 2009-08-25 2014-01-07 Honeywell International Inc. Turbomachine core coupling assembly
US9988155B2 (en) 2013-02-07 2018-06-05 United Technologies Corporation System and method for aft mount of gas turbine engine
US10814993B2 (en) 2017-08-21 2020-10-27 Raytheon Technologies Corporation Inlet cowl deflection limiting strut
US11407518B2 (en) * 2020-02-19 2022-08-09 General Electric Company Aircraft and propulsion engine mount system

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR955254A (fr) * 1950-01-11
US2344735A (en) * 1942-02-27 1944-03-21 United Aircraft Corp Engine mount
FR967640A (fr) * 1948-06-03 1950-11-08 Montage et fixation d'un turbo-propulseur dans la cellule d'un avion
US2965338A (en) * 1956-04-09 1960-12-20 Rolls Royce Engine mounting
US3327965A (en) * 1965-09-27 1967-06-27 Douglas Aircraft Inc Flexible engine pylon
GB1411601A (en) * 1972-03-04 1975-10-29 Rolls Royce Ducted fan gas turbine engine supported by an aircraft wing mainspar
US3907220A (en) * 1974-03-14 1975-09-23 United Aircraft Corp Rear engine redundant mount

Also Published As

Publication number Publication date
US4022018A (en) 1977-05-10
JPS5950560B2 (ja) 1984-12-08
DE2618283A1 (de) 1976-12-23
DE2618283C2 (fr) 1987-02-05
GB1540654A (en) 1979-02-14
FR2309402A1 (fr) 1976-11-26
JPS51131100A (en) 1976-11-15
IT1060001B (it) 1982-07-10
FR2309402B1 (fr) 1982-06-04
CA1038360A (fr) 1978-09-12

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Legal Events

Date Code Title Description
RE Patent lapsed

Owner name: GENERAL ELECTRIC CY

Effective date: 19890430