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FR2426609A1 - Appareil de montage pour reacteur d'avion a tuyere a flux melange - Google Patents

Appareil de montage pour reacteur d'avion a tuyere a flux melange

Info

Publication number
FR2426609A1
FR2426609A1 FR7901370A FR7901370A FR2426609A1 FR 2426609 A1 FR2426609 A1 FR 2426609A1 FR 7901370 A FR7901370 A FR 7901370A FR 7901370 A FR7901370 A FR 7901370A FR 2426609 A1 FR2426609 A1 FR 2426609A1
Authority
FR
France
Prior art keywords
reactor
airplane
mounting device
flow tube
mixed flow
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
FR7901370A
Other languages
English (en)
Other versions
FR2426609B3 (fr
Inventor
Patrick Murphy
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
Publication of FR2426609A1 publication Critical patent/FR2426609A1/fr
Application granted granted Critical
Publication of FR2426609B3 publication Critical patent/FR2426609B3/fr
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • B64D27/402—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
    • 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
    • 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
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supports For Pipes And Cables (AREA)

Abstract

Le réacteur a une partie noyau 14 enfermée dans un logement 16, et une partie ventilateur 18 enfermée dans un carter 20, et l'appareil de support comprend une structure de support principale 34, une bielle de poussée principale 48, un dispositif de support postérieur 50, et deux dispositifs de support antérieurs 52, l'agencement étant tel que la bielle de poussée s'oppose à la poussée du réacteur en créant un premier couple de forces, et le dispositif de support postérieur et les dispositifs de support antérieurs créent un couple de forces opposé
FR7901370A 1978-05-22 1979-01-19 Appareil de montage pour reacteur d'avion a tuyere a flux melange Granted FR2426609A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/908,080 US4266741A (en) 1978-05-22 1978-05-22 Mounting apparatus for fan jet engine having mixed flow nozzle installation

Publications (2)

Publication Number Publication Date
FR2426609A1 true FR2426609A1 (fr) 1979-12-21
FR2426609B3 FR2426609B3 (fr) 1981-10-16

Family

ID=25425141

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7901370A Granted FR2426609A1 (fr) 1978-05-22 1979-01-19 Appareil de montage pour reacteur d'avion a tuyere a flux melange

Country Status (6)

Country Link
US (1) US4266741A (fr)
JP (1) JPS54153498A (fr)
DE (1) DE2902635A1 (fr)
FR (1) FR2426609A1 (fr)
GB (1) GB2021696B (fr)
IT (1) IT1114372B (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2993535A1 (fr) * 2012-07-20 2014-01-24 Airbus Operations Sas Ensemble propulsif comprenant un turboreacteur a double flux de tres grand diametre et son dispositif d'accrochage sous la voilure d'un aeronef
FR3074151A1 (fr) * 2017-11-28 2019-05-31 Safran Nacelles Dispositif de levage et de transport d'un ensemble propulsif d'un aeronef

Families Citing this family (75)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4428189A (en) * 1980-04-02 1984-01-31 United Technologies Corporation Case deflection control in aircraft gas turbine engines
GB8300748D0 (en) * 1983-01-12 1983-02-16 British Aerospace Power plant attachment for aircraft wings
US4658579A (en) * 1983-07-14 1987-04-21 United Technologies Corporation Load sharing for engine nacelle
GB2148398A (en) * 1983-10-25 1985-05-30 Alan Edward Coppin A support housing for machinery
US4634081A (en) * 1983-12-30 1987-01-06 The Boeing Company Aft engine mount with vibration isolators
US4571936A (en) * 1985-07-10 1986-02-25 The United States Of America As Represented By The Secretary Of The Air Force Length adjustable strut link with low aerodynamic drag
GB2188987B (en) * 1986-04-09 1990-02-14 Rolls Royce A turbofan gas turbine engine and mountings therefor
US4934140A (en) * 1988-05-13 1990-06-19 United Technologies Corporation Modular gas turbine engine
GB2220034B (en) * 1988-06-22 1992-12-02 Rolls Royce Plc Aerodynamic loading in gas turbine engines
WO1991005150A1 (fr) * 1989-09-29 1991-04-18 Sundstrand Corporation, Inc. Structure de support pour moteur geodesique
US5127606A (en) * 1990-11-16 1992-07-07 Allied-Signal Inc. Aircraft engine mount adapter and method
GB9116986D0 (en) * 1991-08-07 1991-10-09 Rolls Royce Plc Gas turbine engine nacelle assembly
US5174525A (en) * 1991-09-26 1992-12-29 General Electric Company Structure for eliminating lift load bending in engine core of turbofan
US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
GB2266080A (en) * 1992-04-16 1993-10-20 Rolls Royce Plc Mounting arrangement for a gas turbine engine.
US5319922A (en) * 1992-12-04 1994-06-14 General Electric Company Aircraft gas turbine engine backbone deflection control
US5452575A (en) * 1993-09-07 1995-09-26 General Electric Company Aircraft gas turbine engine thrust mount
US5524847A (en) * 1993-09-07 1996-06-11 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
US5443229A (en) * 1993-12-13 1995-08-22 General Electric Company Aircraft gas turbine engine sideways mount
US6328293B1 (en) 1998-09-18 2001-12-11 Lord Corporation Multi-linkage suspension system including outboard isolators
US6401448B1 (en) * 2000-08-31 2002-06-11 General Electric Company System for mounting aircraft engines
KR100417979B1 (ko) * 2001-07-24 2004-02-11 한국항공우주산업 주식회사 항공기의 엔진 착탈장치
US7010906B2 (en) * 2001-11-02 2006-03-14 Rolls-Royce Plc Gas turbine engine haveing a disconnect panel for routing pipes and harnesses between a first and a second zone
US6607165B1 (en) 2002-06-28 2003-08-19 General Electric Company Aircraft engine mount with single thrust link
FR2851226B1 (fr) 2003-02-19 2005-05-20 Snecma Moteurs Structure porteuse pour un turbopropulseur et ensemble comportant une telle structure porteuse
US7083143B2 (en) * 2003-10-17 2006-08-01 The Boeing Company Apparatuses and methods for attaching engines and other structures to aircraft wings
FR2862945B1 (fr) * 2003-12-01 2006-04-28 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef.
GB0328671D0 (en) * 2003-12-11 2004-01-14 Rolls Royce Plc Aircraft engine mounting
FR2867157B1 (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.
FR2873987B1 (fr) * 2004-08-05 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
FR2873988B1 (fr) * 2004-08-05 2007-12-21 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
US7419121B2 (en) * 2004-12-09 2008-09-02 Honeywell International Inc. Integrated mount duct for use with airborne auxiliary power units and other turbomachines
SE528948C2 (sv) * 2004-12-23 2007-03-20 Volvo Aero Corp Ringformad vridstyv statisk komponent för en flygplansmotor
US20060145001A1 (en) * 2004-12-30 2006-07-06 Smith Matthew C Fan cowl door elimination
FR2885878B1 (fr) * 2005-05-23 2007-06-29 Airbus France Sas Ensemble moteur pour aeronef
FR2885877B1 (fr) * 2005-05-23 2008-12-12 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2887521B1 (fr) * 2005-06-28 2007-08-17 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un dispositif d'accrochage d'un tel moteur
GB0516066D0 (en) * 2005-08-04 2005-09-14 Airbus Uk Ltd Removal of components from aircraft
FR2891247B1 (fr) * 2005-09-26 2009-04-03 Airbus France Sas Ensemble pour aeronef comprenant un element de voilure ainsi qu'un mat d'accrochage
FR2891246B1 (fr) * 2005-09-26 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un dispositif d'accrochage d'un tel moteur
FR2891254B1 (fr) * 2005-09-29 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef
FR2891526B1 (fr) * 2005-10-03 2007-11-02 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2903076B1 (fr) * 2006-06-30 2009-05-29 Aircelle Sa Nacelle structurante
FR2905990A1 (fr) 2006-09-20 2008-03-21 Snecma Sa Systeme propulsif a pylone integre pour avion.
FR2909974B1 (fr) * 2006-12-13 2009-02-06 Aircelle Sa Nacelle pour turboreacteur double flux
FR2919347B1 (fr) * 2007-07-26 2009-11-20 Snecma Enveloppe externe de conduite de soufflante dans une turbomachine.
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
US20150377123A1 (en) 2007-08-01 2015-12-31 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
US11149650B2 (en) 2007-08-01 2021-10-19 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
US8256707B2 (en) * 2007-08-01 2012-09-04 United Technologies Corporation Engine mounting configuration for a turbofan gas turbine engine
GB0722772D0 (en) 2007-11-21 2008-01-02 Airbus Uk Ltd Aircraft engine pylon attachment
FR2924684B1 (fr) * 2007-12-07 2010-01-01 Snecma Suspension d'un turboreacteur a un aeronef
US8118251B2 (en) * 2008-01-18 2012-02-21 United Technologies Corporation Mounting system for a gas turbine engine
FR2928180B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant une structure annulaire de transfert d'efforts entourant le carter central d'un turboreacteur.
FR2928181B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant un turboreacteur avec des structures de renfort reliant le carter de soufflante au carter central.
FR2928136B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante.
FR2931134B1 (fr) * 2008-05-14 2010-06-18 Airbus France Mat d'accrochage de moteur d'aeronef comprenant un caisson de section en forme de cercle ou d'ellipse
US8313293B2 (en) * 2009-05-15 2012-11-20 Pratt & Whitney Canada Corp. Turbofan mounting system
US8979491B2 (en) 2009-05-15 2015-03-17 Pratt & Whitney Canada Corp. Turbofan mounting arrangement
US8567202B2 (en) * 2009-05-15 2013-10-29 Pratt & Whitney Canada Corp. Support links with lockable adjustment feature
FR2963390B1 (fr) * 2010-07-30 2012-08-31 Snecma Turboreacteur lateral perfectionne pour limiter ses deformations
US20130232768A1 (en) 2012-03-12 2013-09-12 United Technologies Corporation Turbine engine case mount and dismount
US9637241B2 (en) 2012-03-16 2017-05-02 The Boeing Company Engine mounting system for an aircraft
US9151181B2 (en) 2012-06-19 2015-10-06 United Technologies Corporation Metallic rails on composite fan case
US9211955B1 (en) * 2012-12-10 2015-12-15 The Boeing Company Methods and apparatus for supporting engines and nacelles relative to aircraft wings
FR3002288B1 (fr) * 2013-02-20 2022-11-25 Snecma Suspension d'un turboreacteur par double support arriere
FR3010147B1 (fr) * 2013-08-28 2015-08-21 Snecma Suspension isostatique d'un turboreacteur par double support arriere
GB201418396D0 (en) * 2014-10-17 2014-12-03 Rolls Royce Plc Gas turbine engine support structures
FR3078108B1 (fr) * 2018-02-20 2020-01-31 Safran Nacelles Ensemble propulsif comportant des points de levage disposes sur des supports de verins d’inverseur de poussee
US11613372B2 (en) * 2020-11-09 2023-03-28 Rohr, Inc. Ducted fan case attachment structure
US12091181B2 (en) 2021-12-13 2024-09-17 Spirit Aerosystems, Inc. Aircraft engine attachment assembly
US20230365247A1 (en) * 2022-05-13 2023-11-16 The Boeing Company Strut assembly and method for coupling an engine to a wing of an aircraft

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB506645A (en) * 1937-11-30 1939-05-30 Albert George Elliott Improvements in or relating to the mounting of aircraft engines and propellers
US2815184A (en) * 1954-04-02 1957-12-03 Northrop Aircraft Inc Aircraft engine hoist and mounting system
US3063661A (en) * 1958-03-12 1962-11-13 United Aircraft Corp Ducted fan engine
US3042349A (en) * 1959-11-13 1962-07-03 Gen Electric Removable aircraft engine mounting arrangement
US3222017A (en) * 1964-03-30 1965-12-07 Gen Electric Engine mounting
US3352114A (en) * 1965-07-17 1967-11-14 Rolls Royce Mounting means for separately supporting a gas turbine engine and a jet pipe in an engine pod
US3397855A (en) * 1966-12-01 1968-08-20 United Aircraft Canada Rear mount system for aircraft engines
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
DE1531395A1 (de) * 1967-07-18 1970-01-29 Entwicklungsring Sued Gmbh Triebwerksaufhaengung,insbesondere fuer die Strahltriebwerke von Kurz- oder Senkrechtstartflugzeugen
GB1318748A (en) * 1970-08-11 1973-05-31 Secr Defence Gas turgine ducted fan engines for aircraft
DE2044553C3 (de) * 1970-09-09 1973-12-13 Wandel U. Goltermann, 7410 Reutlingen Laufzeit und Dampfungsentzerrer
US3675418A (en) * 1970-11-19 1972-07-11 United Aircraft Corp Jet engine force frame
GB1411601A (en) * 1972-03-04 1975-10-29 Rolls Royce Ducted fan gas turbine engine supported by an aircraft wing mainspar
US3831888A (en) * 1972-07-27 1974-08-27 Mc Donnell Douglas Corp Aircraft engine suspension system
US3809340A (en) * 1972-12-26 1974-05-07 A Dolgy Devices for mounting an engine on an aircraft pylon
US3844115A (en) * 1973-02-14 1974-10-29 Gen Electric Load distributing thrust mount
US3848832A (en) * 1973-03-09 1974-11-19 Boeing Co Aircraft engine installation
US3907220A (en) * 1974-03-14 1975-09-23 United Aircraft Corp Rear engine redundant mount
GB1516980A (en) * 1974-12-24 1978-07-05 Rolls Royce Mounting ducted fan gas turbine engines on aircraft
GB1504290A (en) * 1975-08-01 1978-03-15 Rolls Royce Gas turbine engine mounting systems

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2993535A1 (fr) * 2012-07-20 2014-01-24 Airbus Operations Sas Ensemble propulsif comprenant un turboreacteur a double flux de tres grand diametre et son dispositif d'accrochage sous la voilure d'un aeronef
FR3074151A1 (fr) * 2017-11-28 2019-05-31 Safran Nacelles Dispositif de levage et de transport d'un ensemble propulsif d'un aeronef

Also Published As

Publication number Publication date
DE2902635A1 (de) 1979-11-29
DE2902635C2 (fr) 1989-10-12
GB2021696A (en) 1979-12-05
IT1114372B (it) 1986-01-27
JPS621879B2 (fr) 1987-01-16
JPS54153498A (en) 1979-12-03
US4266741A (en) 1981-05-12
FR2426609B3 (fr) 1981-10-16
IT7947710A0 (it) 1979-01-19
GB2021696B (en) 1982-09-02

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