FR2747735B1 - Support de moteur a turbine a gaz a soufflante canalisee - Google Patents

Support de moteur a turbine a gaz a soufflante canalisee

Info

Publication number
FR2747735B1
FR2747735B1 FR9704225A FR9704225A FR2747735B1 FR 2747735 B1 FR2747735 B1 FR 2747735B1 FR 9704225 A FR9704225 A FR 9704225A FR 9704225 A FR9704225 A FR 9704225A FR 2747735 B1 FR2747735 B1 FR 2747735B1
Authority
FR
France
Prior art keywords
support
gas turbine
turbine engine
channel blower
blower
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
FR9704225A
Other languages
English (en)
Other versions
FR2747735A1 (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 FR2747735A1 publication Critical patent/FR2747735A1/fr
Application granted granted Critical
Publication of FR2747735B1 publication Critical patent/FR2747735B1/fr
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; 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
FR9704225A 1996-04-18 1997-04-07 Support de moteur a turbine a gaz a soufflante canalisee Expired - Fee Related FR2747735B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9608064A GB2312251B (en) 1996-04-18 1996-04-18 Ducted fan gas turbine engine mounting

Publications (2)

Publication Number Publication Date
FR2747735A1 FR2747735A1 (fr) 1997-10-24
FR2747735B1 true FR2747735B1 (fr) 2000-09-22

Family

ID=10792298

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9704225A Expired - Fee Related FR2747735B1 (fr) 1996-04-18 1997-04-07 Support de moteur a turbine a gaz a soufflante canalisee

Country Status (3)

Country Link
US (1) US5860276A (fr)
FR (1) FR2747735B1 (fr)
GB (1) GB2312251B (fr)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2320525A (en) * 1996-12-18 1998-06-24 British Aerospace Mounting of powerplant in aircraft
FR2866070B1 (fr) * 2004-02-05 2008-12-05 Snecma Moteurs Turboreacteur a fort taux de dilution
FR2903076B1 (fr) * 2006-06-30 2009-05-29 Aircelle Sa Nacelle structurante
US7900433B2 (en) * 2006-08-31 2011-03-08 United Technologies Corporation Fan exhaust nozzle for turbofan engine
US8413932B2 (en) 2010-04-10 2013-04-09 Aerofex, Inc. Peripheral control ejector
FR2909974B1 (fr) * 2006-12-13 2009-02-06 Aircelle Sa Nacelle pour turboreacteur double flux
US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US20150377123A1 (en) 2007-08-01 2015-12-31 United Technologies Corporation Turbine section of high bypass turbofan
US11149650B2 (en) 2007-08-01 2021-10-19 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US8844265B2 (en) 2007-08-01 2014-09-30 United Technologies Corporation Turbine section of high bypass turbofan
US11242805B2 (en) 2007-08-01 2022-02-08 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US8256707B2 (en) * 2007-08-01 2012-09-04 United Technologies Corporation Engine mounting configuration for a turbofan gas turbine engine
US11346289B2 (en) 2007-08-01 2022-05-31 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US8118251B2 (en) * 2008-01-18 2012-02-21 United Technologies Corporation Mounting system for a gas turbine engine
US8167237B2 (en) * 2008-03-21 2012-05-01 United Technologies Corporation Mounting system for a gas turbine engine
US8511605B2 (en) 2008-06-02 2013-08-20 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US20140174056A1 (en) * 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8807477B2 (en) 2008-06-02 2014-08-19 United Technologies Corporation Gas turbine engine compressor arrangement
US8128021B2 (en) * 2008-06-02 2012-03-06 United Technologies Corporation Engine mount system for a turbofan gas turbine engine
US8800914B2 (en) 2008-06-02 2014-08-12 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8695920B2 (en) 2008-06-02 2014-04-15 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US10179653B2 (en) * 2012-10-02 2019-01-15 United Technologies Corporation Pylon shape with geared turbofan for structural stiffness
US10371047B2 (en) 2013-10-16 2019-08-06 United Technologies Corporation Geared turbofan engine with targeted modular efficiency
FR3014840B1 (fr) 2013-12-17 2017-10-13 Airbus Operations Sas Ensemble pour aeronef comprenant un corps d'attache moteur equipe d'au moins une ferrure de support de manille penetrant dans le caisson du mat d'accrochage
FR3015431B1 (fr) * 2013-12-19 2017-12-15 Airbus Operations Sas Structure primaire de mat d'accrochage renforcee.
FR3015433B1 (fr) 2013-12-23 2016-02-12 Airbus Operations Sas Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage
US10590952B2 (en) * 2015-07-21 2020-03-17 United Technologies Corporation Nacelle assembly
US10040560B2 (en) * 2015-09-30 2018-08-07 The Boeing Company Trailing edge core compartment vent for an aircraft engine
US11697506B2 (en) 2020-05-15 2023-07-11 General Electric Company Methods and apparatus for gas turbine bending isolation

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1516980A (en) * 1974-12-24 1978-07-05 Rolls Royce Mounting ducted fan gas turbine engines on aircraft
US4147029A (en) * 1976-01-02 1979-04-03 General Electric Company Long duct mixed flow gas turbine engine
US4785625A (en) * 1987-04-03 1988-11-22 United Technologies Corporation Ducted fan gas turbine power plant mounting
GB2215290B (en) * 1988-03-08 1991-09-04 Rolls Royce Plc A method of mounting a ducted fan gas turbine engine on an aircraft
US5174525A (en) * 1991-09-26 1992-12-29 General Electric Company Structure for eliminating lift load bending in engine core of turbofan
US5205513A (en) * 1991-09-26 1993-04-27 General Electric Company Method and system for the removal of large turbine engines
GB2275308B (en) * 1993-02-20 1997-02-26 Rolls Royce Plc A mounting for coupling a turbofan gas turbine engine to an aircraft structure
US5524847A (en) * 1993-09-07 1996-06-11 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
US5452575A (en) * 1993-09-07 1995-09-26 General Electric Company Aircraft gas turbine engine thrust mount
US5467941A (en) * 1993-12-30 1995-11-21 The Boeing Company Pylon and engine installation for ultra-high by-pass turbo-fan engines

Also Published As

Publication number Publication date
GB2312251B (en) 1999-10-27
US5860276A (en) 1999-01-19
GB9608064D0 (en) 1996-06-19
FR2747735A1 (fr) 1997-10-24
GB2312251A (en) 1997-10-22

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20151231