FR2295876A1 - Perfectionnement a l'istallation sur les avions des turbomoteurs a double flux - Google Patents

Perfectionnement a l'istallation sur les avions des turbomoteurs a double flux

Info

Publication number
FR2295876A1
FR2295876A1 FR7539719A FR7539719A FR2295876A1 FR 2295876 A1 FR2295876 A1 FR 2295876A1 FR 7539719 A FR7539719 A FR 7539719A FR 7539719 A FR7539719 A FR 7539719A FR 2295876 A1 FR2295876 A1 FR 2295876A1
Authority
FR
France
Prior art keywords
istallation
turbomotors
stream
improvement
aircraft dual
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
FR7539719A
Other languages
English (en)
Other versions
FR2295876B1 (fr
Inventor
Douglas John Nightingale
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of FR2295876A1 publication Critical patent/FR2295876A1/fr
Application granted granted Critical
Publication of FR2295876B1 publication Critical patent/FR2295876B1/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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7539719A 1974-12-24 1975-12-24 Perfectionnement a l'istallation sur les avions des turbomoteurs a double flux Granted FR2295876A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB55768/74A GB1516980A (en) 1974-12-24 1974-12-24 Mounting ducted fan gas turbine engines on aircraft

Publications (2)

Publication Number Publication Date
FR2295876A1 true FR2295876A1 (fr) 1976-07-23
FR2295876B1 FR2295876B1 (fr) 1980-06-06

Family

ID=10474825

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7539719A Granted FR2295876A1 (fr) 1974-12-24 1975-12-24 Perfectionnement a l'istallation sur les avions des turbomoteurs a double flux

Country Status (5)

Country Link
US (1) US4013246A (fr)
JP (1) JPS5945559B2 (fr)
DE (1) DE2557266C2 (fr)
FR (1) FR2295876A1 (fr)
GB (1) GB1516980A (fr)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0132214A1 (fr) * 1983-07-14 1985-01-23 United Technologies Corporation Répartiteur de charge pour les nacelles de turbomoteurs des avions
FR2560854A1 (fr) * 1984-03-07 1985-09-13 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
US5181675A (en) * 1991-05-23 1993-01-26 Societe Nationale D'etude Et Moteurs D'aviation S.N.E. Pod for suspending a turbojet engine unit of the bypass type under the wing of an aircraft
EP0564126A1 (fr) * 1992-03-25 1993-10-06 General Electric Company Montage de reprise de poussée d'un moteur sur un avion
WO2008142098A1 (fr) * 2007-05-23 2008-11-27 Airbus France Mat d'accrochage de moteur pour aeronef comprenant une cale biaise pour la fixation de l'attache moteur avant
FR2928136A1 (fr) * 2008-02-28 2009-09-04 Airbus France Sa Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante.
FR3032180A1 (fr) * 2015-01-30 2016-08-05 Airbus Operations Sas Ensemble propulsif comportant un turboreacteur et un mat d'accrochage permettant une nouvelle distribution des efforts entre le turboreacteur et la voilure
EP3587749A1 (fr) * 2018-06-28 2020-01-01 Rolls-Royce plc Moteur de turbine à gaz

Families Citing this family (51)

* 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
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
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
US4437627A (en) 1982-03-12 1984-03-20 The Boeing Company Integrated power plant installation system
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
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
US4603821A (en) * 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine
DE3434453C2 (de) * 1984-09-20 1986-12-04 Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart Triebwerksaufhängung für Fahrzeuge, insbesondere für propellergetriebene Flugzeuge
US4725019A (en) * 1986-08-11 1988-02-16 The Boeing Company Aircraft engine mount with vertical vibration isolation
US4854525A (en) * 1987-05-19 1989-08-08 The Boeing Company Engine mounting assembly
US5064144A (en) * 1987-05-19 1991-11-12 The Boeing Company Engine mounting assembly
US4805851A (en) * 1987-08-10 1989-02-21 Herbst Paul T Turbine engine mounting bracket assembly
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
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
GB2312251B (en) * 1996-04-18 1999-10-27 Rolls Royce Plc Ducted fan gas turbine engine mounting
US6095456A (en) * 1996-12-23 2000-08-01 The Boeing Company Strut-wing interface having dual upper links
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
FR2862944B1 (fr) * 2003-12-01 2006-02-24 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef
FR2873986B1 (fr) * 2004-08-04 2007-12-21 Airbus France Sas Ensemble moteur pour aeronef
FR2873985B1 (fr) * 2004-08-04 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
FR2873987B1 (fr) * 2004-08-05 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
GB0418454D0 (en) * 2004-08-19 2004-09-22 Rolls Royce Plc An engine mounting assembly
FR2885877B1 (fr) * 2005-05-23 2008-12-12 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2885878B1 (fr) * 2005-05-23 2007-06-29 Airbus France Sas Ensemble moteur pour aeronef
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
FR2891244B1 (fr) * 2005-09-26 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891526B1 (fr) * 2005-10-03 2007-11-02 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2902406B1 (fr) * 2006-06-20 2008-07-18 Airbus France Sas Carenage pour mat de suspension d'un turbomoteur a une aile d'aeronef
FR2903076B1 (fr) * 2006-06-30 2009-05-29 Aircelle Sa Nacelle structurante
FR2915175B1 (fr) * 2007-04-20 2009-07-17 Airbus France Sa Mat d'accrochage de moteur pour aeronef disposant d'une poutre d'attache moteur arriere deportee du caisson
US8438859B2 (en) * 2008-01-08 2013-05-14 Rolls-Royce North American Technologies, Inc. Integrated bypass engine structure
US8950702B2 (en) * 2008-01-18 2015-02-10 United Technologies Corporation Pylon and engine mount configuration
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.
US20140174056A1 (en) 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8567202B2 (en) * 2009-05-15 2013-10-29 Pratt & Whitney Canada Corp. Support links with lockable adjustment feature
US8979491B2 (en) 2009-05-15 2015-03-17 Pratt & Whitney Canada Corp. Turbofan mounting arrangement
US8313293B2 (en) * 2009-05-15 2012-11-20 Pratt & Whitney Canada Corp. Turbofan mounting system
FR2970700B1 (fr) * 2011-01-20 2013-10-11 Airbus Operations Sas Dispositif d'accrochage d'un moteur d'aeronef a un mat
US9637241B2 (en) 2012-03-16 2017-05-02 The Boeing Company Engine mounting system for an aircraft
FR3040369B1 (fr) * 2015-09-02 2018-07-13 Airbus Operations Sas Ensemble moteur d'aeronef comprenant une attache moteur avant amelioree
US10464684B2 (en) 2016-02-01 2019-11-05 Bell Textron Inc. Tapered sockets for aircraft engine mount assemblies
US10384790B2 (en) 2016-02-01 2019-08-20 Bell Textron Inc. Engine mount assemblies for aircraft
US10814993B2 (en) 2017-08-21 2020-10-27 Raytheon Technologies Corporation Inlet cowl deflection limiting strut
GB2575483A (en) * 2018-07-12 2020-01-15 Airbus Operations Ltd Wing assembly mount
FR3167130A1 (fr) 2024-10-09 2026-04-10 Safran Aircraft Engines Ensemble comportant une turbomachine et une structure de liaison et de support de la turbomachine a un aeronef
US12545415B1 (en) 2025-06-06 2026-02-10 Rtx Corporation Gas turbine engine aircraft mounting system

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2102187A1 (fr) * 1970-08-11 1972-04-07 Secretaire Etat Royaume

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR967640A (fr) * 1948-06-03 1950-11-08 Montage et fixation d'un turbo-propulseur dans la cellule d'un avion
US3042349A (en) * 1959-11-13 1962-07-03 Gen Electric Removable aircraft engine mounting arrangement
US3540682A (en) * 1964-12-02 1970-11-17 Gen Electric Turbofan type engine frame and support system
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
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
US3848832A (en) * 1973-03-09 1974-11-19 Boeing Co Aircraft engine installation

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2102187A1 (fr) * 1970-08-11 1972-04-07 Secretaire Etat Royaume

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0132214A1 (fr) * 1983-07-14 1985-01-23 United Technologies Corporation Répartiteur de charge pour les nacelles de turbomoteurs des avions
FR2560854A1 (fr) * 1984-03-07 1985-09-13 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
EP0155887A1 (fr) * 1984-03-07 1985-09-25 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Capotages structuraux participant à la rigidité d'ensemble d'un turboréacteur
US4683717A (en) * 1984-03-07 1987-08-04 Societe Nationale D'etude Et De Construction De Moteur D'aviation "S.N.E.C.M.A." Structural cowlings of twin flow turbo jet engines
US5181675A (en) * 1991-05-23 1993-01-26 Societe Nationale D'etude Et Moteurs D'aviation S.N.E. Pod for suspending a turbojet engine unit of the bypass type under the wing of an aircraft
EP0564126A1 (fr) * 1992-03-25 1993-10-06 General Electric Company Montage de reprise de poussée d'un moteur sur un avion
WO2008142098A1 (fr) * 2007-05-23 2008-11-27 Airbus France Mat d'accrochage de moteur pour aeronef comprenant une cale biaise pour la fixation de l'attache moteur avant
FR2916424A1 (fr) * 2007-05-23 2008-11-28 Airbus France Sa Mat d'accrochage de moteur pour aeronef comprenant une cale biaise pour la fixation de l'attache moteur avant
FR2928136A1 (fr) * 2008-02-28 2009-09-04 Airbus France Sa Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante.
WO2009112777A3 (fr) * 2008-02-28 2009-10-29 Airbus France Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante
RU2487057C2 (ru) * 2008-02-28 2013-07-10 Эрбюс Операсьон Силовая установка летательного аппарата, содержащая узлы подвески двигателя, смещенные вниз на корпусе вентилятора
US9032740B2 (en) 2008-02-28 2015-05-19 Airbus Operations S.A.S. Engine assembly for an aircraft comprising attachments for engines offset below on the fan frame
FR3032180A1 (fr) * 2015-01-30 2016-08-05 Airbus Operations Sas Ensemble propulsif comportant un turboreacteur et un mat d'accrochage permettant une nouvelle distribution des efforts entre le turboreacteur et la voilure
US9919804B2 (en) 2015-01-30 2018-03-20 Airbus Operations Sas Propulsion assembly incorporating a turbofan and a mounting pylon enabling a new distribution of the forces between the turbofan and the wing
EP3587749A1 (fr) * 2018-06-28 2020-01-01 Rolls-Royce plc Moteur de turbine à gaz

Also Published As

Publication number Publication date
JPS5945559B2 (ja) 1984-11-07
GB1516980A (en) 1978-07-05
DE2557266C2 (de) 1983-02-17
JPS51108499A (fr) 1976-09-25
US4013246A (en) 1977-03-22
DE2557266A1 (de) 1976-07-08
FR2295876B1 (fr) 1980-06-06

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Legal Events

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CA Change of address
CD Change of name or company name
ST Notification of lapse