DE3902325A1 - Verfahren zum aufhaengen eines mantelstrom-fan-gasturbinentriebwerks an einem flugzeug - Google Patents

Verfahren zum aufhaengen eines mantelstrom-fan-gasturbinentriebwerks an einem flugzeug

Info

Publication number
DE3902325A1
DE3902325A1 DE3902325A DE3902325A DE3902325A1 DE 3902325 A1 DE3902325 A1 DE 3902325A1 DE 3902325 A DE3902325 A DE 3902325A DE 3902325 A DE3902325 A DE 3902325A DE 3902325 A1 DE3902325 A1 DE 3902325A1
Authority
DE
Germany
Prior art keywords
pylon
turbine engine
aircraft
fan gas
gas turbine
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Withdrawn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
DE3902325A
Other languages
German (de)
English (en)
Inventor
Arnold Charles Newton
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
Publication of DE3902325A1 publication Critical patent/DE3902325A1/de
Withdrawn legal-status Critical Current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; 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)
DE3902325A 1988-03-08 1989-01-26 Verfahren zum aufhaengen eines mantelstrom-fan-gasturbinentriebwerks an einem flugzeug Withdrawn DE3902325A1 (de)

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 (1)

Publication Number Publication Date
DE3902325A1 true DE3902325A1 (de) 1989-09-21

Family

ID=10633071

Family Applications (1)

Application Number Title Priority Date Filing Date
DE3902325A Withdrawn DE3902325A1 (de) 1988-03-08 1989-01-26 Verfahren zum aufhaengen eines mantelstrom-fan-gasturbinentriebwerks an einem flugzeug

Country Status (4)

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

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 (fr) * 2003-11-25 2007-03-09 Airbus France Dispositif d'accrochage d'un moteur sous une voilure d'aeronef
FR2885878B1 (fr) * 2005-05-23 2007-06-29 Airbus France Sas Ensemble moteur pour aeronef
FR2885877B1 (fr) * 2005-05-23 2008-12-12 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2891246B1 (fr) * 2005-09-26 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un dispositif d'accrochage d'un tel moteur
FR2981046B1 (fr) * 2011-10-06 2013-10-25 Aircelle Sa Ensemble propulsif d'aeronef
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

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4361296A (en) * 1980-03-10 1982-11-30 The Boeing Company Uniflange coupling assembly
US4384453A (en) * 1979-10-23 1983-05-24 Rolls-Royce Limited Pod installation for a gas turbine engine
GB2119857A (en) * 1982-04-30 1983-11-23 Rolls Royce Ducted fan gas turbine engine
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
US4603821A (en) * 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine

Family Cites Families (5)

* 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
JPS5945559A (ja) * 1982-09-08 1984-03-14 Toshiba Corp 制御装置
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
JPS6112134A (ja) * 1984-06-27 1986-01-20 Mitsubishi Electric Corp 無線受信機

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4384453A (en) * 1979-10-23 1983-05-24 Rolls-Royce Limited Pod 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
US4603821A (en) * 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine

Also Published As

Publication number Publication date
JPH01229799A (ja) 1989-09-13
FR2628388A1 (fr) 1989-09-15
GB2215290A (en) 1989-09-20
GB8805527D0 (en) 1988-04-07
GB2215290B (en) 1991-09-04
FR2628388B1 (fr) 1991-10-18

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Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
8139 Disposal/non-payment of the annual fee