IT1242998B - Ventilatore e cofano integrato per motore a derivazione ultra alta e suo trasporto e rimozione - Google Patents

Ventilatore e cofano integrato per motore a derivazione ultra alta e suo trasporto e rimozione

Info

Publication number
IT1242998B
IT1242998B IT02133690A IT2133690A IT1242998B IT 1242998 B IT1242998 B IT 1242998B IT 02133690 A IT02133690 A IT 02133690A IT 2133690 A IT2133690 A IT 2133690A IT 1242998 B IT1242998 B IT 1242998B
Authority
IT
Italy
Prior art keywords
fan
transport
removal
ultra high
derivation engine
Prior art date
Application number
IT02133690A
Other languages
English (en)
Other versions
IT9021336A0 (it
IT9021336A1 (it
Inventor
Eugene Jesus Antuna
Donald Frederick Keck
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT9021336A0 publication Critical patent/IT9021336A0/it
Publication of IT9021336A1 publication Critical patent/IT9021336A1/it
Application granted granted Critical
Publication of IT1242998B publication Critical patent/IT1242998B/it

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
    • 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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/02—Power-plant nacelles, fairings or cowlings associated with wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IT02133690A 1989-09-07 1990-08-30 Ventilatore e cofano integrato per motore a derivazione ultra alta e suo trasporto e rimozione IT1242998B (it)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
IT9021336A0 IT9021336A0 (it) 1990-08-30
IT9021336A1 IT9021336A1 (it) 1992-03-01
IT1242998B true IT1242998B (it) 1994-05-23

Family

ID=23597620

Family Applications (1)

Application Number Title Priority Date Filing Date
IT02133690A IT1242998B (it) 1989-09-07 1990-08-30 Ventilatore e cofano integrato per motore a derivazione ultra alta e suo trasporto e rimozione

Country Status (6)

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

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2866070B1 (fr) * 2004-02-05 2008-12-05 Snecma Moteurs Turboreacteur a fort taux de dilution
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
CN107738223B (zh) * 2017-11-13 2023-11-10 山东太古飞机工程有限公司 飞机发动机第一级静子叶片整流罩的拆装辅助工装
GB201810606D0 (en) * 2018-06-28 2018-08-15 Rolls Royce Plc Gas turbine engine
GB201817935D0 (en) * 2018-11-02 2018-12-19 Rolls Royce Plc Method of replacing a module
GB201817936D0 (en) * 2018-11-02 2018-12-19 Rolls Royce Plc Method of upgrading a modular gas turbine engine
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 (it) * 1971-09-23 1973-05-04 Inst Francais Du Petrole
FR2096708B1 (it) * 1970-06-22 1974-03-22 Snecma
US3703081A (en) * 1970-11-20 1972-11-21 Gen Electric Gas turbine engine
JPS5022165U (it) * 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

Also Published As

Publication number Publication date
IT9021336A0 (it) 1990-08-30
GB2238082A (en) 1991-05-22
JPH03141829A (ja) 1991-06-17
IT9021336A1 (it) 1992-03-01
DE4025775A1 (de) 1991-03-28
GB9019356D0 (en) 1990-10-17
FR2651537A1 (fr) 1991-03-08
CA2021087A1 (en) 1991-03-08

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Legal Events

Date Code Title Description
0001 Granted