FR2628388B1 - Procede de montage d'un moteur a turbine a gaz a helice carenee - Google Patents

Procede de montage d'un moteur a turbine a gaz a helice carenee

Info

Publication number
FR2628388B1
FR2628388B1 FR898901432A FR8901432A FR2628388B1 FR 2628388 B1 FR2628388 B1 FR 2628388B1 FR 898901432 A FR898901432 A FR 898901432A FR 8901432 A FR8901432 A FR 8901432A FR 2628388 B1 FR2628388 B1 FR 2628388B1
Authority
FR
France
Prior art keywords
mounting
gas turbine
turbine engine
faired propeller
faired
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 - Fee Related
Application number
FR898901432A
Other languages
English (en)
Other versions
FR2628388A1 (fr
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 FR2628388A1 publication Critical patent/FR2628388A1/fr
Application granted granted Critical
Publication of FR2628388B1 publication Critical patent/FR2628388B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/16Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • B64D27/406Suspension 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)
FR898901432A 1988-03-08 1989-02-03 Procede de montage d'un moteur a turbine a gaz a helice carenee Expired - Fee Related FR2628388B1 (fr)

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 (2)

Publication Number Publication Date
FR2628388A1 FR2628388A1 (fr) 1989-09-15
FR2628388B1 true FR2628388B1 (fr) 1991-10-18

Family

ID=10633071

Family Applications (1)

Application Number Title Priority Date Filing Date
FR898901432A Expired - Fee Related FR2628388B1 (fr) 1988-03-08 1989-02-03 Procede de montage d'un moteur a turbine a gaz a helice carenee

Country Status (4)

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

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
FR2885877B1 (fr) * 2005-05-23 2008-12-12 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2885878B1 (fr) * 2005-05-23 2007-06-29 Airbus France Sas Ensemble moteur 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

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
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
US4361296A (en) * 1980-03-10 1982-11-30 The Boeing Company Uniflange coupling assembly
GB2119857A (en) * 1982-04-30 1983-11-23 Rolls Royce Ducted fan gas turbine engine
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
US4603821A (en) * 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine
JPS6112134A (ja) * 1984-06-27 1986-01-20 Mitsubishi Electric Corp 無線受信機

Also Published As

Publication number Publication date
GB8805527D0 (en) 1988-04-07
GB2215290A (en) 1989-09-20
GB2215290B (en) 1991-09-04
FR2628388A1 (fr) 1989-09-15
DE3902325A1 (de) 1989-09-21
JPH01229799A (ja) 1989-09-13

Similar Documents

Publication Publication Date Title
GB2165964B (en) Combustion system for a gas turbine engine
DE3562796D1 (en) Control device for a combustion engine with turbo compressor
GB2314126B (en) Cooled blades for a gas turbine engine
GB2222452B (en) System for cooling an internal combustion engine including a turbocharger
GB2173863B (en) A propeller module for an aero gas turbine engine
GB9000458D0 (en) Cooled blades for a gas turbine engine
FR2586453B1 (fr) Carburateur pour moteur a turbine a gaz
GB2275308B (en) A mounting for coupling a turbofan gas turbine engine to an aircraft structure
FR2594886B1 (fr) Module propulsif pour un moteur aeronautique a turbine a gaz
FR2623250B1 (fr) Dispositif de ventilation pour la nacelle d'un moteur a turbine a gaz notamment pour un aeronef
GB2220711B (en) Stator assembly for a gas turbine engine
GB9125011D0 (en) A mounting arrangement for a gas turbine engine
FR2619161B1 (fr) Chassis assemble pour moteur a turbine a gaz
GB9208398D0 (en) Mounting arrangement for a gas turbine engine
GB2219045B (en) Gas turbine engine fuel system
FR2589427B1 (fr) Module d'helice pour un moteur a turbine a gaz aeronautique
GB2150277B (en) Combustion apparatus for a gas turbine engine
GB9022387D0 (en) Fuel control system for a gas turbine engine
GB8911332D0 (en) A variable pitch propeller module for an aero gas turbine engine powerplant
FR2640690B1 (fr) Systeme et procede de commande d'un moteur a turbines a gaz
GB2216192B (en) Fuel purging system for a turbine engine
GB2226852B (en) A combustion system of an internal combustion engine
EP0335168A3 (en) Method of operating a combustion engine
FR2628388B1 (fr) Procede de montage d'un moteur a turbine a gaz a helice carenee
DE3474191D1 (en) Fuel control system for a gas turbine engine

Legal Events

Date Code Title Description
ST Notification of lapse