GB1318748A - Gas turgine ducted fan engines for aircraft - Google Patents

Gas turgine ducted fan engines for aircraft

Info

Publication number
GB1318748A
GB1318748A GB3857070A GB3857070A GB1318748A GB 1318748 A GB1318748 A GB 1318748A GB 3857070 A GB3857070 A GB 3857070A GB 3857070 A GB3857070 A GB 3857070A GB 1318748 A GB1318748 A GB 1318748A
Authority
GB
United Kingdom
Prior art keywords
gas
ducted fan
aircraft
turgine
fan
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
GB3857070A
Other languages
English (en)
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.)
SECR DEFENCE
UK Secretary of State for Defence
Original Assignee
SECR DEFENCE
UK Secretary of State for 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, UK Secretary of State for Defence filed Critical SECR DEFENCE
Priority to GB3857070A priority Critical patent/GB1318748A/en
Priority to US00169971A priority patent/US3750983A/en
Priority to DE19712140347 priority patent/DE2140347C3/de
Priority to IT27448/71A priority patent/IT938772B/it
Priority to FR7129352A priority patent/FR2102187B1/fr
Publication of GB1318748A publication Critical patent/GB1318748A/en
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)
GB3857070A 1970-08-11 1970-08-11 Gas turgine ducted fan engines for aircraft Expired GB1318748A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB3857070A GB1318748A (en) 1970-08-11 1970-08-11 Gas turgine ducted fan engines for aircraft
US00169971A US3750983A (en) 1970-08-11 1971-08-09 Gas turbine ducted fan engines for aircraft
DE19712140347 DE2140347C3 (de) 1970-08-11 1971-08-11 Gasturbinen-Gebläsestrahltriebwerk
IT27448/71A IT938772B (it) 1970-08-11 1971-08-11 Motore a turbina a gas con ventola intubata per aeromobil
FR7129352A FR2102187B1 (enExample) 1970-08-11 1971-08-11

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
GB1318748A true GB1318748A (en) 1973-05-31

Family

ID=10404335

Family Applications (1)

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

Country Status (4)

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

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3039869A1 (de) * 1979-10-23 1981-05-07 Rolls-Royce Ltd., London Triebwerksgondelaufbau
GB2202588A (en) * 1987-03-02 1988-09-28 Gen Electric Turbofan engine
RU2338668C2 (ru) * 2006-12-28 2008-11-20 Закрытое акционерное общество "Гражданские самолеты Сухого" Пилон подвески двигателя к крылу
CN109896023A (zh) * 2017-12-11 2019-06-18 空中客车运营简化股份公司 格栅和涡轮风扇发动机及飞行器

Families Citing this family (38)

* 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
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
DE3374545D1 (en) * 1983-12-08 1987-12-23 Boeing Co 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
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
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

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3039869A1 (de) * 1979-10-23 1981-05-07 Rolls-Royce Ltd., London Triebwerksgondelaufbau
GB2202588A (en) * 1987-03-02 1988-09-28 Gen Electric Turbofan engine
US4825648A (en) * 1987-03-02 1989-05-02 General Electric Company Turbofan engine having a split cowl
GB2202588B (en) * 1987-03-02 1991-09-25 Gen Electric Turbofan engine
RU2338668C2 (ru) * 2006-12-28 2008-11-20 Закрытое акционерное общество "Гражданские самолеты Сухого" Пилон подвески двигателя к крылу
CN109896023A (zh) * 2017-12-11 2019-06-18 空中客车运营简化股份公司 格栅和涡轮风扇发动机及飞行器

Also Published As

Publication number Publication date
DE2140347B2 (de) 1975-11-27
FR2102187A1 (enExample) 1972-04-07
DE2140347A1 (de) 1972-02-17
US3750983A (en) 1973-08-07
FR2102187B1 (enExample) 1975-04-18
IT938772B (it) 1973-02-10

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees