FR2102187A1 - - Google Patents

Info

Publication number
FR2102187A1
FR2102187A1 FR7129352A FR7129352A FR2102187A1 FR 2102187 A1 FR2102187 A1 FR 2102187A1 FR 7129352 A FR7129352 A FR 7129352A FR 7129352 A FR7129352 A FR 7129352A FR 2102187 A1 FR2102187 A1 FR 2102187A1
Authority
FR
France
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
FR7129352A
Other languages
French (fr)
Other versions
FR2102187B1 (enExample
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.)
SECRETAIRE ETAT ROYAUME
Original Assignee
SECRETAIRE ETAT ROYAUME
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 SECRETAIRE ETAT ROYAUME filed Critical SECRETAIRE ETAT ROYAUME
Publication of FR2102187A1 publication Critical patent/FR2102187A1/fr
Application granted granted Critical
Publication of FR2102187B1 publication Critical patent/FR2102187B1/fr
Expired 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
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7129352A 1970-08-11 1971-08-11 Expired FR2102187B1 (enExample)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3857070A GB1318748A (en) 1970-08-11 1970-08-11 Gas turgine ducted fan engines for aircraft

Publications (2)

Publication Number Publication Date
FR2102187A1 true FR2102187A1 (enExample) 1972-04-07
FR2102187B1 FR2102187B1 (enExample) 1975-04-18

Family

ID=10404335

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7129352A Expired FR2102187B1 (enExample) 1970-08-11 1971-08-11

Country Status (4)

Country Link
US (1) US3750983A (enExample)
FR (1) FR2102187B1 (enExample)
GB (1) GB1318748A (enExample)
IT (1) IT938772B (enExample)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2295876A1 (fr) * 1974-12-24 1976-07-23 Rolls Royce Perfectionnement a l'istallation sur les avions des turbomoteurs a double flux
FR2451461A1 (fr) * 1979-03-10 1980-10-10 Rolls Royce Montage de groupe moteur de turbomachine
FR2467776A1 (fr) * 1979-10-23 1981-04-30 Rolls Royce Fuseau porteur pour turboreacteur d'aeronef
EP0028970A1 (fr) * 1979-11-12 1981-05-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Dispositif de fixation de turboréacteurs multiflux
FR2479902A1 (fr) * 1980-04-02 1981-10-09 United Technologies Corp Structure de controle de deviation de carter pour les turbines a gaz d'aeronefs
FR2611810A1 (fr) * 1987-03-02 1988-09-09 Gen Electric Reacteur a double flux comportant un capot fractionne
FR2628388A1 (fr) * 1988-03-08 1989-09-15 Rolls Royce Plc Procede de montage d'un moteur a turbine a gaz a helice carenee
EP0733545A1 (fr) * 1995-03-21 1996-09-25 AEROSPATIALE Société Nationale Industrielle Turboréacteur à double flux à nacelle flottante
FR2902406A1 (fr) * 2006-06-20 2007-12-21 Airbus France Sas Carenage pour mat de suspension d'un turbomoteur a une aile d'aeronef
FR3016660A1 (fr) * 2014-01-23 2015-07-24 Snecma Carter de turbomachine a virole sans empochements et a chapes renforcees par des raidisseurs
FR3031726A1 (fr) * 2015-01-21 2016-07-22 Aircelle Sa Systeme pour la pose et la depose d’un ensemble propulsif sur un mat d’un aeronef

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1411601A (en) * 1972-03-04 1975-10-29 Rolls Royce Ducted fan gas turbine engine supported by an aircraft wing mainspar
US3830058A (en) * 1973-02-26 1974-08-20 Avco Corp Fan engine mounting
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
US4150802A (en) * 1977-05-31 1979-04-24 The Boeing Company Aircraft engine installation
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
US4603822A (en) * 1983-12-08 1986-08-05 The Boeing Company Aft engine mount
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
US4634081A (en) * 1983-12-30 1987-01-06 The Boeing Company Aft engine mount with vibration isolators
US4603821A (en) * 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine
FR2560854B1 (fr) * 1984-03-07 1986-09-12 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
GB2188987B (en) * 1986-04-09 1990-02-14 Rolls Royce A turbofan gas turbine engine and mountings therefor
US4854525A (en) * 1987-05-19 1989-08-08 The Boeing Company Engine mounting assembly
US4790137A (en) * 1987-07-17 1988-12-13 The United States Of America As Represented By The Secretary Of The Air Force Aircraft engine outer duct mounting device
WO1991005150A1 (en) * 1989-09-29 1991-04-18 Sundstrand Corporation, Inc. Geodesic engine mount structure
US5307623A (en) * 1991-05-28 1994-05-03 General Electric Company Apparatus and method for the diassembly of an ultra high bypass engine
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
GB0328671D0 (en) * 2003-12-11 2004-01-14 Rolls Royce Plc Aircraft engine mounting
US7448219B2 (en) * 2004-06-21 2008-11-11 Boeing Co Hingeless flapper valve for flow control
GB2422874A (en) * 2005-02-05 2006-08-09 Alstom Technology Ltd Gas turbine burner expansion bar structure
RU2338668C2 (ru) * 2006-12-28 2008-11-20 Закрытое акционерное общество "Гражданские самолеты Сухого" Пилон подвески двигателя к крылу
FR2920146B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Nacelle a section de sortie adaptable
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.
FR2960855A1 (fr) * 2010-06-03 2011-12-09 Aircelle Sa Nacelle pour turboreacteur avec dispositif de reprise d'efforts circonferentiels
DE102011013076A1 (de) * 2011-03-04 2012-09-06 Rolls-Royce Deutschland Ltd & Co Kg Strahltriebwerksvorrichtung mit einem Nebenstromkanal
US9091210B2 (en) * 2012-04-26 2015-07-28 United Technologies Corporation TEC mount redundant fastening
FR3074855A1 (fr) * 2017-12-11 2019-06-14 Airbus Operations Grille pour la formation d'un flux d'inversion d'un turboreacteur d'aeronef
US10808550B2 (en) * 2018-12-13 2020-10-20 Raytheon Technologies Corporation Fan blade with integral metering device for controlling gas pressure within the fan blade
GB201900609D0 (en) * 2019-01-16 2019-03-06 Rolls Royce Plc Mounting apparatus for gas turbine engine
US11407518B2 (en) * 2020-02-19 2022-08-09 General Electric Company Aircraft and propulsion engine mount system

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1157062A (fr) * 1956-07-30 1958-05-27 Snecma Dispositif de montage des moteurs, en particulier des propulseurs à réaction sur les aérodynes
US3318554A (en) * 1964-09-22 1967-05-09 Rolls Royce Mounting arrangement for engines
US3540682A (en) * 1964-12-02 1970-11-17 Gen Electric Turbofan type engine frame and support system
US3541794A (en) * 1969-04-23 1970-11-24 Gen Electric Bifurcated fan duct thrust reverser

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
NEANT *

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2295876A1 (fr) * 1974-12-24 1976-07-23 Rolls Royce Perfectionnement a l'istallation sur les avions des turbomoteurs a double flux
FR2451461A1 (fr) * 1979-03-10 1980-10-10 Rolls Royce Montage de groupe moteur de turbomachine
FR2467776A1 (fr) * 1979-10-23 1981-04-30 Rolls Royce Fuseau porteur pour turboreacteur d'aeronef
EP0028970A1 (fr) * 1979-11-12 1981-05-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Dispositif de fixation de turboréacteurs multiflux
FR2469566A1 (fr) * 1979-11-12 1981-05-22 Snecma Perfectionnements aux dispositifs de fixation de turboreacteurs multiflux
US4441313A (en) * 1979-11-12 1984-04-10 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Mounting devices for multiple flow turbojet engines
FR2479902A1 (fr) * 1980-04-02 1981-10-09 United Technologies Corp Structure de controle de deviation de carter pour les turbines a gaz d'aeronefs
FR2611810A1 (fr) * 1987-03-02 1988-09-09 Gen Electric Reacteur a double flux comportant un capot fractionne
FR2628388A1 (fr) * 1988-03-08 1989-09-15 Rolls Royce Plc Procede de montage d'un moteur a turbine a gaz a helice carenee
EP0733545A1 (fr) * 1995-03-21 1996-09-25 AEROSPATIALE Société Nationale Industrielle Turboréacteur à double flux à nacelle flottante
FR2732074A1 (fr) * 1995-03-21 1996-09-27 Aerospatiale Turboreacteur a double flux a nacelle flottante
US5642615A (en) * 1995-03-21 1997-07-01 Aerospatiale Societe Nationale Industrielle Turbofan engine with a floating pod
FR2902406A1 (fr) * 2006-06-20 2007-12-21 Airbus France Sas Carenage pour mat de suspension d'un turbomoteur a une aile d'aeronef
WO2007147965A3 (fr) * 2006-06-20 2008-02-14 Airbus France Carenage pour mat de suspension d'un turbomoteur a une aile d'aeronef
RU2391260C1 (ru) * 2006-06-20 2010-06-10 Эрбюс Франс Обтекатель для пилона, посредством которого газотурбинный двигатель подвешивается к крылу летательного аппарата
US8366039B2 (en) 2006-06-20 2013-02-05 Airbus Operations Sas Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft
FR3016660A1 (fr) * 2014-01-23 2015-07-24 Snecma Carter de turbomachine a virole sans empochements et a chapes renforcees par des raidisseurs
WO2015110749A1 (fr) * 2014-01-23 2015-07-30 Snecma Carter de turbomachine à virole sans empochements et à chapes renforcées par des raidisseurs
GB2538897A (en) * 2014-01-23 2016-11-30 Safran Aircraft Engines Turbomachine casing comprising a cavity-free shroud and yokes reinforced by stiffeners
US10371009B2 (en) 2014-01-23 2019-08-06 Safran Aircraft Engines Turbomachine casing comprising a cavity-free shroud and yokes reinforced by stiffeners
GB2538897B (en) * 2014-01-23 2020-11-04 Safran Aircraft Engines Turbomachine casing comprising a cavity-free shroud and yokes reinforced by stiffeners
FR3031726A1 (fr) * 2015-01-21 2016-07-22 Aircelle Sa Systeme pour la pose et la depose d’un ensemble propulsif sur un mat d’un aeronef
WO2016116710A1 (fr) * 2015-01-21 2016-07-28 Aircelle Système pour la pose et la dépose d'un ensemble propulsif sur un mât d'un aéronef
US11186379B2 (en) 2015-01-21 2021-11-30 Safran Nacelles System for installing and removing a propulsion unit on a pylon of an aircraft

Also Published As

Publication number Publication date
US3750983A (en) 1973-08-07
GB1318748A (en) 1973-05-31
DE2140347B2 (de) 1975-11-27
FR2102187B1 (enExample) 1975-04-18
IT938772B (it) 1973-02-10
DE2140347A1 (de) 1972-02-17

Similar Documents

Publication Publication Date Title
AR204384A1 (enExample)
ATA96471A (enExample)
AU2044470A (enExample)
AU1146470A (enExample)
AU1473870A (enExample)
AU2085370A (enExample)
AU1326870A (enExample)
AU1833270A (enExample)
AU2017870A (enExample)
AU1716970A (enExample)
AU1517670A (enExample)
AU2130570A (enExample)
AU1336970A (enExample)
AR195465A1 (enExample)
AU1591370A (enExample)
AU1841070A (enExample)
AU2144270A (enExample)
AU1328670A (enExample)
ATA672271A (enExample)
AU1343870A (enExample)
AU1004470A (enExample)
AU1064870A (enExample)
AU2131570A (enExample)
AU1581370A (enExample)
AU1277070A (enExample)

Legal Events

Date Code Title Description
ST Notification of lapse