IT938772B - Motore a turbina a gas con ventola intubata per aeromobil - Google Patents

Motore a turbina a gas con ventola intubata per aeromobil

Info

Publication number
IT938772B
IT938772B IT27448/71A IT2744871A IT938772B IT 938772 B IT938772 B IT 938772B IT 27448/71 A IT27448/71 A IT 27448/71A IT 2744871 A IT2744871 A IT 2744871A IT 938772 B IT938772 B IT 938772B
Authority
IT
Italy
Prior art keywords
aeromobil
intubated
fan
gas turbine
turbine engine
Prior art date
Application number
IT27448/71A
Other languages
English (en)
Original Assignee
Secr Defence
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 Secr Defence filed Critical Secr Defence
Application granted granted Critical
Publication of IT938772B publication Critical patent/IT938772B/it

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
    • B64D27/404—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)
IT27448/71A 1970-08-11 1971-08-11 Motore a turbina a gas con ventola intubata per aeromobil IT938772B (it)

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 (1)

Publication Number Publication Date
IT938772B true IT938772B (it) 1973-02-10

Family

ID=10404335

Family Applications (1)

Application Number Title Priority Date Filing Date
IT27448/71A IT938772B (it) 1970-08-11 1971-08-11 Motore a turbina a gas con ventola intubata per aeromobil

Country Status (4)

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

Families Citing this family (41)

* 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
GB1516980A (en) * 1974-12-24 1978-07-05 Rolls Royce Mounting ducted fan gas turbine engines on aircraft
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
GB2044358B (en) * 1979-03-10 1983-01-19 Rolls Royce Gas turbine jet engine mounting
GB2061389B (en) * 1979-10-23 1983-05-18 Rolls Royce Rod installation for a gas turbine engine
FR2469566A1 (fr) * 1979-11-12 1981-05-22 Snecma Perfectionnements aux dispositifs de fixation de turboreacteurs multiflux
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
US4428189A (en) * 1980-04-02 1984-01-31 United Technologies Corporation Case deflection control in aircraft gas turbine engines
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
US4603821A (en) * 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine
US4634081A (en) * 1983-12-30 1987-01-06 The Boeing Company Aft engine mount with vibration isolators
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
US4825648A (en) * 1987-03-02 1989-05-02 General Electric Company Turbofan engine having a split cowl
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
GB2215290B (en) * 1988-03-08 1991-09-04 Rolls Royce Plc A method of mounting a ducted fan gas turbine engine on an aircraft
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
FR2732074B1 (fr) * 1995-03-21 1997-06-06 Aerospatiale Turboreacteur a double flux a nacelle flottante
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
FR2902406B1 (fr) * 2006-06-20 2008-07-18 Airbus France Sas Carenage pour mat de suspension d'un turbomoteur a une aile d'aeronef
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
FR3016660B1 (fr) 2014-01-23 2018-10-05 Safran Aircraft Engines Carter de turbomachine a virole sans empochements et a chapes renforcees par des raidisseurs
FR3031726B1 (fr) * 2015-01-21 2017-02-24 Aircelle Sa Systeme pour la pose et la depose d’un ensemble propulsif sur un mat d’un aeronef
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

Also Published As

Publication number Publication date
DE2140347B2 (de) 1975-11-27
US3750983A (en) 1973-08-07
FR2102187B1 (it) 1975-04-18
DE2140347A1 (de) 1972-02-17
FR2102187A1 (it) 1972-04-07
GB1318748A (en) 1973-05-31

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