DE2550525C3 - Vorrichtung zum Anbringen eines Strahltriebwerkes an einem Flugzeug - Google Patents

Vorrichtung zum Anbringen eines Strahltriebwerkes an einem Flugzeug

Info

Publication number
DE2550525C3
DE2550525C3 DE2550525A DE2550525A DE2550525C3 DE 2550525 C3 DE2550525 C3 DE 2550525C3 DE 2550525 A DE2550525 A DE 2550525A DE 2550525 A DE2550525 A DE 2550525A DE 2550525 C3 DE2550525 C3 DE 2550525C3
Authority
DE
Germany
Prior art keywords
nacelle
jet engine
engine
carrier
connecting device
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
Application number
DE2550525A
Other languages
German (de)
English (en)
Other versions
DE2550525A1 (de
DE2550525B2 (de
Inventor
Paul Joseph Vaux-Le-Penil Legrand
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of DE2550525A1 publication Critical patent/DE2550525A1/de
Publication of DE2550525B2 publication Critical patent/DE2550525B2/de
Application granted granted Critical
Publication of DE2550525C3 publication Critical patent/DE2550525C3/de
Expired 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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/08—Inspection panels for power plants
    • 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
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
DE2550525A 1974-11-13 1975-11-11 Vorrichtung zum Anbringen eines Strahltriebwerkes an einem Flugzeug Expired DE2550525C3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7437468A FR2291091A1 (fr) 1974-11-13 1974-11-13 Dispositif de montage sur avion d'un turboreacteur

Publications (3)

Publication Number Publication Date
DE2550525A1 DE2550525A1 (de) 1976-05-20
DE2550525B2 DE2550525B2 (de) 1980-12-18
DE2550525C3 true DE2550525C3 (de) 1981-09-10

Family

ID=9144898

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2550525A Expired DE2550525C3 (de) 1974-11-13 1975-11-11 Vorrichtung zum Anbringen eines Strahltriebwerkes an einem Flugzeug

Country Status (4)

Country Link
US (1) US4037809A (https=)
DE (1) DE2550525C3 (https=)
FR (1) FR2291091A1 (https=)
GB (1) GB1520759A (https=)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4437627A (en) 1982-03-12 1984-03-20 The Boeing Company Integrated power plant installation system

Families Citing this family (65)

* Cited by examiner, † Cited by third party
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GB1521847A (en) * 1976-04-30 1978-08-16 Rolls Royce Attachment for attaching jet propulsion engines to vehicle structure
US4150802A (en) * 1977-05-31 1979-04-24 The Boeing Company Aircraft engine installation
US4283028A (en) * 1979-12-03 1981-08-11 The Boeing Company Adjustable wedge fitting for sharing the thrust load of a jet engine
US4361296A (en) * 1980-03-10 1982-11-30 The Boeing Company Uniflange coupling assembly
US4474346A (en) * 1982-07-02 1984-10-02 The Boeing Company Collapsible cowl structure for gas-turbine engine strut
US4506850A (en) * 1983-01-04 1985-03-26 The Boeing Company Engine installation for aircraft
US4555078A (en) * 1983-12-27 1985-11-26 Societe Belge D'exploitation De La Navigation Aerienne (Sabena) Apparatus for the suspension of an aircraft engine cowling
FR2560854B1 (fr) * 1984-03-07 1986-09-12 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
GB8416019D0 (en) * 1984-06-22 1984-07-25 British Aerospace Structural joint
US4697763A (en) * 1985-10-31 1987-10-06 The Boeing Company Hinge system for thrust reverser cowl
GB2188987B (en) * 1986-04-09 1990-02-14 Rolls Royce A turbofan gas turbine engine and mountings therefor
US4825648A (en) * 1987-03-02 1989-05-02 General Electric Company Turbofan engine having a split cowl
FR2622507B1 (https=) * 1987-10-28 1990-01-26 Snecma
FR2622930B1 (fr) * 1987-11-06 1990-03-23 Aerospatiale Capotage pour turboreacteur a double flux
GB8822798D0 (en) * 1988-09-28 1988-11-02 Short Brothers Ltd Ducted fan turbine engine
FR2661213B1 (fr) * 1990-04-19 1992-07-03 Snecma Moteur d'aviation a tres grand taux de dilution et du type dit contrafan avant.
US5222360A (en) * 1991-10-30 1993-06-29 General Electric Company Apparatus for removably attaching a core frame to a vane frame with a stable mid ring
US5174525A (en) * 1991-09-26 1992-12-29 General Electric Company Structure for eliminating lift load bending in engine core of turbofan
US5251435A (en) * 1991-10-30 1993-10-12 General Electric Company Reverser inner cowl with integral bifurcation walls and core cowl
GB2266080A (en) * 1992-04-16 1993-10-20 Rolls Royce Plc Mounting arrangement for a gas turbine engine.
GB9301457D0 (en) * 1993-01-26 1993-03-17 Short Brothers Plc An aircraft propulsuve power unit
US5641133A (en) * 1994-05-11 1997-06-24 Mcdonnell Douglas Helicopter Co. Rotorcraft fuselage modal frequency placement using resilient mounting connections
UA26001C2 (uk) * 1994-08-23 1999-02-26 Запорізьке Машинобудівне Конструкторське Бюро "Прогрес" Ім. Академіка О.Г. Івченка Пристрій кріплеhhя капота реактивhого двигуhа літальhого апарата
FR2731049B1 (fr) * 1995-02-28 1997-05-09 Aerospatiale Dispositif de fixation d'une bouche d'entree d'air sur un reacteur et reacteur comportant un tel dispositif
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
FR2771330B1 (fr) * 1997-11-26 2004-02-27 Aerospatiale Procede de fabrication d'un panneau composite monolithique articule avec des moyens raidisseurs integres, panneau articule obtenu et capot articule dans un aeronef
FR2771710B1 (fr) * 1997-12-03 2000-02-11 Aerospatiale Dispositif d'ouverture commun a deux capots adjacents de nacelle de moteur d'avion
US6267327B1 (en) * 1999-04-02 2001-07-31 Allison Advanced Development Company Coupling system for connecting a gas turbine engine to an aircraft mounted exhaust system
FR2825976B1 (fr) * 2001-06-13 2003-09-05 Eads Airbus Sa Dispositif de reprise d'efforts generes par un moteur d'aeronef
GB0315431D0 (en) * 2003-07-02 2003-08-06 Rolls Royce Plc Aircraft configuration
GB0320371D0 (en) * 2003-08-29 2003-10-01 Rolls Royce Plc A closure panel arrangement
FR2861364B1 (fr) * 2003-10-22 2006-02-03 Airbus France Dispositif de montage d'un carenage dispose entre une entree d'air d'un moteur d'aeronef et un mat.
FR2862945B1 (fr) * 2003-12-01 2006-04-28 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef.
ES2264625B1 (es) * 2004-12-15 2007-12-01 GAMESA INNOVATION & TECHNOLOGY, S.L. Procedimiento de retirada de la cubierta de un aerogenerador.
ES2316257B1 (es) * 2006-10-31 2010-01-12 Airbus España, S.L. Cono de cola para aeronave con carena movil y estructura de soporte de unidad auxiliar de energia y de sus elementos anexos.
FR2912378B1 (fr) * 2007-02-14 2009-03-20 Aircelle Sa Nacelle de moteur a reaction pour un avion
FR2914700B1 (fr) * 2007-04-04 2009-05-22 Aircelle Sa Inverseur de poussee pour moteur a reaction
FR2916426B1 (fr) * 2007-05-22 2010-04-02 Aircelle Sa Ensemble arriere de nacelle pour turboreacteur.
US11242805B2 (en) 2007-08-01 2022-02-08 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
US20150377123A1 (en) 2007-08-01 2015-12-31 United 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
US11346289B2 (en) 2007-08-01 2022-05-31 Raytheon 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
US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon Technologies Corporation Turbine section of high bypass turbofan
FR2920174A1 (fr) * 2007-08-20 2009-02-27 Aircelle Sa Dispositif de liaison entre les deux demi-coquilles d'une nacelle de moteur d'aeronef, et nacelle equipee d'un tel dispositif
US8438859B2 (en) * 2008-01-08 2013-05-14 Rolls-Royce North American Technologies, Inc. Integrated bypass engine structure
FR2952615B1 (fr) * 2009-11-18 2011-12-09 Aircelle Sa Ensemble de maintien de l'interface d'une structure externe fixe d'une nacelle et d'un carter de turboreacteur
US8398018B2 (en) * 2009-11-27 2013-03-19 Rohr, Inc. Fan cowl support for a turbo fan engine
US8876042B2 (en) * 2009-12-21 2014-11-04 General Electric Company Integrated nacelle assembly
FR2962765B1 (fr) * 2010-07-13 2012-07-27 Snecma Turboreacteur avec un element de nacelle fixe au carter intermediaire
FR2970513B1 (fr) * 2011-01-14 2015-07-31 Aircelle Sa Dispositif de liaison d'un cadre avant a un carter de soufflante
FR2978734B1 (fr) * 2011-08-05 2015-01-02 Airbus Operations Sas Dispositif de liaison plus particulierement adapte pour assurer la liaison entre une entree d'air et une motorisation d'une nacelle d'aeronef
FR2983836B1 (fr) 2011-12-08 2014-12-19 Airbus Operations Sas Outillage d'aide a la construction et a la maintenance des aeronefs
US9217390B2 (en) * 2012-06-28 2015-12-22 United Technologies Corporation Thrust reverser maintenance actuation system
EP3181458B1 (en) * 2015-12-15 2019-10-16 Airbus Operations, S.L. Suspension system for an aircraft auxiliary power unit
US10543927B2 (en) 2016-11-18 2020-01-28 Rohr, Inc. Lockable track system for a translating nacelle structure
US11046446B2 (en) 2017-03-02 2021-06-29 Bell Helicopter Textron Inc. Tiltrotor aircraft rotating proprotor assembly
US10994853B2 (en) 2017-03-02 2021-05-04 Bell Helicopter Textron Inc. Tiltrotor aircraft rotating proprotor assembly
US10533603B2 (en) 2017-03-02 2020-01-14 Bell Helicopter Textron Inc. Roller track assembly for a tiltrotor proprotor door
US10539180B2 (en) 2017-03-02 2020-01-21 Bell Helicopter Textron Inc. Bogie mechanism for a tiltrotor proprotor door
FR3079215B1 (fr) * 2018-03-22 2020-11-20 Airbus Operations Sas Carenage avant d'un mat d'aeronef comprenant une coiffe mobile et aeronef equipe dudit carenage avant
US10875627B2 (en) 2018-05-01 2020-12-29 Bell Helicopter Textron Inc. Movable cover for a proprotor nacelle
GB201808514D0 (en) * 2018-05-24 2018-07-11 Rolls Royce Plc Mounting System and Mounting Method for Gas Turbine Aero Engine
US12246845B2 (en) 2021-05-20 2025-03-11 General Electric Company Methods and apparatus for mounting a gas turbine engine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2783003A (en) * 1951-10-16 1957-02-26 Lockheed Aircraft Corp Aircraft engine installation
GB711719A (en) * 1951-12-20 1954-07-07 Sncan Improvements in aircraft equipped with a propelling motor at the rear
US2958480A (en) * 1953-06-30 1960-11-01 Saulnier Raymond Aircraft with low aspect-ratio wing
US2944331A (en) * 1955-11-07 1960-07-12 Gen Electric Engine installation frame
US2982497A (en) * 1958-03-28 1961-05-02 Bendix Corp Clamp ring release mechanism for aircraft booster
US3084507A (en) * 1958-06-17 1963-04-09 Douglas Aircraft Co Inc Jet engine sound suppressor and reverser
GB875295A (en) * 1958-11-26 1961-08-16 Rolls Royce Improvements in or relating to engine mounting
US3194515A (en) * 1963-12-06 1965-07-13 Northrop Corp Jet aircraft structure for engine removal
GB1074068A (en) * 1964-09-22 1967-06-28 Rolls Royce Mounting arrangement for gas turbine jet propulsion engines
US3637042A (en) * 1970-07-27 1972-01-25 Rohr Corp Method and apparatus for suppressing the noise of jet-propelled aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4437627A (en) 1982-03-12 1984-03-20 The Boeing Company Integrated power plant installation system

Also Published As

Publication number Publication date
US4037809A (en) 1977-07-26
FR2291091A1 (fr) 1976-06-11
DE2550525A1 (de) 1976-05-20
FR2291091B1 (https=) 1977-10-21
DE2550525B2 (de) 1980-12-18
GB1520759A (en) 1978-08-09

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
8339 Ceased/non-payment of the annual fee