GB1411601A - Ducted fan gas turbine engine supported by an aircraft wing mainspar - Google Patents

Ducted fan gas turbine engine supported by an aircraft wing mainspar

Info

Publication number
GB1411601A
GB1411601A GB1024272A GB1024272A GB1411601A GB 1411601 A GB1411601 A GB 1411601A GB 1024272 A GB1024272 A GB 1024272A GB 1024272 A GB1024272 A GB 1024272A GB 1411601 A GB1411601 A GB 1411601A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
ducted fan
mainspar
aircraft wing
turbine engine
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
GB1024272A
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.)
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
Priority to GB1024272A priority Critical patent/GB1411601A/en
Priority to US00336044A priority patent/US3837602A/en
Priority to IT21035/73A priority patent/IT979619B/it
Priority to DE19732310313 priority patent/DE2310313A1/de
Priority to FR7307301A priority patent/FR2174886B1/fr
Priority to JP48025024A priority patent/JPS48104297A/ja
Publication of GB1411601A publication Critical patent/GB1411601A/en
Expired 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB1024272A 1972-03-04 1972-03-04 Ducted fan gas turbine engine supported by an aircraft wing mainspar Expired GB1411601A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
GB1024272A GB1411601A (en) 1972-03-04 1972-03-04 Ducted fan gas turbine engine supported by an aircraft wing mainspar
US00336044A US3837602A (en) 1972-03-04 1973-02-26 Mountings for power plants
IT21035/73A IT979619B (it) 1972-03-04 1973-02-28 Supporti per apparati motori
DE19732310313 DE2310313A1 (de) 1972-03-04 1973-03-01 Triebwerksanlage
FR7307301A FR2174886B1 (enExample) 1972-03-04 1973-03-01
JP48025024A JPS48104297A (enExample) 1972-03-04 1973-03-02

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1024272A GB1411601A (en) 1972-03-04 1972-03-04 Ducted fan gas turbine engine supported by an aircraft wing mainspar

Publications (1)

Publication Number Publication Date
GB1411601A true GB1411601A (en) 1975-10-29

Family

ID=9964250

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1024272A Expired GB1411601A (en) 1972-03-04 1972-03-04 Ducted fan gas turbine engine supported by an aircraft wing mainspar

Country Status (6)

Country Link
US (1) US3837602A (enExample)
JP (1) JPS48104297A (enExample)
DE (1) DE2310313A1 (enExample)
FR (1) FR2174886B1 (enExample)
GB (1) GB1411601A (enExample)
IT (1) IT979619B (enExample)

Cited By (2)

* 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
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1516980A (en) * 1974-12-24 1978-07-05 Rolls Royce Mounting ducted fan gas turbine engines on aircraft
US4022018A (en) * 1975-04-29 1977-05-10 General Electric Company Mounting system for a thrust generating engine
US4043522A (en) * 1975-12-22 1977-08-23 The Boeing Company Common pod for housing a plurality of different turbofan jet propulsion engines
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
US4634081A (en) * 1983-12-30 1987-01-06 The Boeing Company Aft engine mount with vibration isolators
GB2188987B (en) * 1986-04-09 1990-02-14 Rolls Royce A turbofan gas turbine engine and mountings therefor
US7850116B2 (en) * 2006-05-26 2010-12-14 The Boeing Company Ducted open rotor apparatus and method
RU2338668C2 (ru) * 2006-12-28 2008-11-20 Закрытое акционерное общество "Гражданские самолеты Сухого" Пилон подвески двигателя к крылу
US8720815B2 (en) 2010-04-27 2014-05-13 Rolls-Royce Corporation Aircraft propulsion system
WO2015157114A1 (en) * 2014-04-11 2015-10-15 Sada-Salinas Jaime G Modular nacelles to provide vertical takeoff and landing (vtol) capabilities to fixed wing aerial vehicles, and associated systems and methods
FR3043648B1 (fr) * 2015-11-13 2018-11-16 Safran Aircraft Engines Voilure propulsive d'un aeronef
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2936978A (en) * 1957-03-29 1960-05-17 United Aircraft Corp Rear engine mount
US3307807A (en) * 1963-07-17 1967-03-07 Nancy Vos Variable lift wing
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
US3362659A (en) * 1965-07-06 1968-01-09 Razak Charles Kenneth Method and apparatus for landing jet aircraft
FR1471132A (fr) * 1966-03-15 1967-02-24 Rolls Royce Structure pour le montage de moteurs applicables, notamment, aux avions
US3448945A (en) * 1966-08-09 1969-06-10 North American Rockwell Convertible propulsion package
GB1328410A (en) * 1969-11-29 1973-08-30 Ver Flugtechnische Werke Aircraft engine mounting means
GB1318748A (en) * 1970-08-11 1973-05-31 Secr Defence Gas turgine ducted fan engines for aircraft

Cited By (2)

* 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
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet

Also Published As

Publication number Publication date
DE2310313A1 (de) 1973-09-13
FR2174886B1 (enExample) 1977-02-04
JPS48104297A (enExample) 1973-12-27
IT979619B (it) 1974-09-30
US3837602A (en) 1974-09-24
FR2174886A1 (enExample) 1973-10-19

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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