GB8805527D0 - Method of mounting ducted fan gas turbine engine on aircraft - Google Patents

Method of mounting ducted fan gas turbine engine on aircraft

Info

Publication number
GB8805527D0
GB8805527D0 GB888805527A GB8805527A GB8805527D0 GB 8805527 D0 GB8805527 D0 GB 8805527D0 GB 888805527 A GB888805527 A GB 888805527A GB 8805527 A GB8805527 A GB 8805527A GB 8805527 D0 GB8805527 D0 GB 8805527D0
Authority
GB
United Kingdom
Prior art keywords
aircraft
mounting
gas turbine
turbine engine
ducted 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.)
Granted
Application number
GB888805527A
Other versions
GB2215290B (en
GB2215290A (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 GB8805527A priority Critical patent/GB2215290B/en
Publication of GB8805527D0 publication Critical patent/GB8805527D0/en
Priority to DE3902325A priority patent/DE3902325A1/en
Priority to JP1022468A priority patent/JPH01229799A/en
Priority to FR898901432A priority patent/FR2628388B1/en
Publication of GB2215290A publication Critical patent/GB2215290A/en
Application granted granted Critical
Publication of GB2215290B publication Critical patent/GB2215290B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64D27/40—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
    • B64D27/02—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
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Vibration Prevention Devices (AREA)
GB8805527A 1988-03-08 1988-03-08 A method of mounting a ducted fan gas turbine engine on an aircraft Expired - Fee Related GB2215290B (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB8805527A GB2215290B (en) 1988-03-08 1988-03-08 A method of mounting a ducted fan gas turbine engine on an aircraft
DE3902325A DE3902325A1 (en) 1988-03-08 1989-01-26 Method for attaching a bypass fan gas-turbine engine to an aircraft
JP1022468A JPH01229799A (en) 1988-03-08 1989-01-31 Method of loading ducted fan-gas turbine engine on aircraft
FR898901432A FR2628388B1 (en) 1988-03-08 1989-02-03 METHOD FOR MOUNTING A GAS TURBINE ENGINE WITH A FAIRED PROPELLER

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8805527A GB2215290B (en) 1988-03-08 1988-03-08 A method of mounting a ducted fan gas turbine engine on an aircraft

Publications (3)

Publication Number Publication Date
GB8805527D0 true GB8805527D0 (en) 1988-04-07
GB2215290A GB2215290A (en) 1989-09-20
GB2215290B GB2215290B (en) 1991-09-04

Family

ID=10633071

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8805527A Expired - Fee Related GB2215290B (en) 1988-03-08 1988-03-08 A method of mounting a ducted fan gas turbine engine on an aircraft

Country Status (4)

Country Link
JP (1) JPH01229799A (en)
DE (1) DE3902325A1 (en)
FR (1) FR2628388B1 (en)
GB (1) GB2215290B (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2275308B (en) * 1993-02-20 1997-02-26 Rolls Royce Plc A mounting for coupling a turbofan gas turbine engine to an aircraft structure
GB2312251B (en) * 1996-04-18 1999-10-27 Rolls Royce Plc Ducted fan gas turbine engine mounting
FR2862611B1 (en) * 2003-11-25 2007-03-09 Airbus France DEVICE FOR ATTACHING AN ENGINE UNDER AN AIRCRAFT SAIL
FR2885878B1 (en) * 2005-05-23 2007-06-29 Airbus France Sas AIRCRAFT ENGINE ASSEMBLY
FR2885877B1 (en) * 2005-05-23 2008-12-12 Airbus France Sas AIRBORNE TURBOJET ENGINEERING MACHINE
FR2891246B1 (en) * 2005-09-26 2007-10-26 Airbus France Sas ENGINE ASSEMBLY FOR AN AIRCRAFT COMPRISING AN ENGINE AND A DEVICE FOR HITCHING SUCH AN ENGINE
FR2981046B1 (en) * 2011-10-06 2013-10-25 Aircelle Sa PROPELLANT AIRCRAFT ASSEMBLY
US10266273B2 (en) 2013-07-26 2019-04-23 Mra Systems, Llc Aircraft engine pylon
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1318748A (en) * 1970-08-11 1973-05-31 Secr Defence Gas turgine ducted fan engines for aircraft
GB1521847A (en) * 1976-04-30 1978-08-16 Rolls Royce Attachment for attaching jet propulsion engines to vehicle structure
GB2061389B (en) * 1979-10-23 1983-05-18 Rolls Royce Rod installation for a gas turbine engine
US4361296A (en) * 1980-03-10 1982-11-30 The Boeing Company Uniflange coupling assembly
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
GB2119857A (en) * 1982-04-30 1983-11-23 Rolls Royce Ducted fan gas turbine engine
JPS5945559A (en) * 1982-09-08 1984-03-14 Toshiba Corp Control device
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
JPS6112134A (en) * 1984-06-27 1986-01-20 Mitsubishi Electric Corp Radio receiver

Also Published As

Publication number Publication date
DE3902325A1 (en) 1989-09-21
FR2628388A1 (en) 1989-09-15
GB2215290B (en) 1991-09-04
GB2215290A (en) 1989-09-20
JPH01229799A (en) 1989-09-13
FR2628388B1 (en) 1991-10-18

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20000308