GB9019356D0 - Ultra high bypass engine integrated fan/cowl and transportation/removal - Google Patents

Ultra high bypass engine integrated fan/cowl and transportation/removal

Info

Publication number
GB9019356D0
GB9019356D0 GB909019356A GB9019356A GB9019356D0 GB 9019356 D0 GB9019356 D0 GB 9019356D0 GB 909019356 A GB909019356 A GB 909019356A GB 9019356 A GB9019356 A GB 9019356A GB 9019356 D0 GB9019356 D0 GB 9019356D0
Authority
GB
United Kingdom
Prior art keywords
cowl
transportation
removal
ultra high
high bypass
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.)
Withdrawn
Application number
GB909019356A
Other versions
GB2238082A (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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB9019356D0 publication Critical patent/GB9019356D0/en
Publication of GB2238082A publication Critical patent/GB2238082A/en
Withdrawn legal-status Critical Current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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
GB9019356A 1989-09-07 1990-09-05 Disassembling and removing ultra high bypass gas turbine engine components Withdrawn GB2238082A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US40397489A 1989-09-07 1989-09-07

Publications (2)

Publication Number Publication Date
GB9019356D0 true GB9019356D0 (en) 1990-10-17
GB2238082A GB2238082A (en) 1991-05-22

Family

ID=23597620

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9019356A Withdrawn GB2238082A (en) 1989-09-07 1990-09-05 Disassembling and removing ultra high bypass gas turbine engine components

Country Status (6)

Country Link
JP (1) JPH03141829A (en)
CA (1) CA2021087A1 (en)
DE (1) DE4025775A1 (en)
FR (1) FR2651537A1 (en)
GB (1) GB2238082A (en)
IT (1) IT1242998B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107738223A (en) * 2017-11-13 2018-02-27 山东太古飞机工程有限公司 The dismounting auxiliary mould of aircraft engine first order stator blade radome fairing

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2866070B1 (en) * 2004-02-05 2008-12-05 Snecma Moteurs TURBOREACTOR WITH HIGH DILUTION RATE
GB0520850D0 (en) 2005-10-14 2005-11-23 Rolls Royce Plc Fan static structure
US20100047077A1 (en) * 2007-12-28 2010-02-25 General Electric Company Ferry Flight Engine Fairing Kit
US20100043228A1 (en) * 2007-12-28 2010-02-25 James Lloyd Daniels Method of Preparing an Engine for Ferry Flight
US8469309B2 (en) * 2008-12-24 2013-06-25 General Electric Company Monolithic structure for mounting aircraft engine
US8814512B2 (en) 2011-07-05 2014-08-26 United Technologies Corporation Fan disk apparatus and method
GB201810606D0 (en) * 2018-06-28 2018-08-15 Rolls Royce Plc Gas turbine engine
GB201817936D0 (en) 2018-11-02 2018-12-19 Rolls Royce Plc Method of upgrading a modular gas turbine engine
GB201817935D0 (en) * 2018-11-02 2018-12-19 Rolls Royce Plc Method of replacing a module
GB202001971D0 (en) * 2020-02-13 2020-04-01 Rolls Royce Plc Nacelle for gas turbine engine and aircraft comprising the same

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1093050A (en) * 1965-03-16 1967-11-29 Rolls Royce Aircraft engine mounting
US3398535A (en) * 1966-05-25 1968-08-27 Gen Electric Engine supporting structure
FR2153787A5 (en) * 1971-09-23 1973-05-04 Inst Francais Du Petrole
FR2096708B1 (en) * 1970-06-22 1974-03-22 Snecma
US3703081A (en) * 1970-11-20 1972-11-21 Gen Electric Gas turbine engine
JPS5022165U (en) * 1973-06-23 1975-03-12
GB1533551A (en) * 1974-11-08 1978-11-29 Gen Electric Gas turbofan engines
JPS5268609A (en) * 1975-12-04 1977-06-07 Agency Of Ind Science & Technol Fixing device for static wing in turbo-fan engine
US4825648A (en) * 1987-03-02 1989-05-02 General Electric Company Turbofan engine having a split cowl
US4934140A (en) * 1988-05-13 1990-06-19 United Technologies Corporation Modular gas turbine engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107738223A (en) * 2017-11-13 2018-02-27 山东太古飞机工程有限公司 The dismounting auxiliary mould of aircraft engine first order stator blade radome fairing
CN107738223B (en) * 2017-11-13 2023-11-10 山东太古飞机工程有限公司 Auxiliary assembly and disassembly tool for fairing of first-stage stator blade of aircraft engine

Also Published As

Publication number Publication date
JPH03141829A (en) 1991-06-17
IT9021336A1 (en) 1992-03-01
IT9021336A0 (en) 1990-08-30
FR2651537A1 (en) 1991-03-08
CA2021087A1 (en) 1991-03-08
IT1242998B (en) 1994-05-23
GB2238082A (en) 1991-05-22
DE4025775A1 (en) 1991-03-28

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)