DE69204293D1 - Gasturbinengondelanlage. - Google Patents

Gasturbinengondelanlage.

Info

Publication number
DE69204293D1
DE69204293D1 DE69204293T DE69204293T DE69204293D1 DE 69204293 D1 DE69204293 D1 DE 69204293D1 DE 69204293 T DE69204293 T DE 69204293T DE 69204293 T DE69204293 T DE 69204293T DE 69204293 D1 DE69204293 D1 DE 69204293D1
Authority
DE
Germany
Prior art keywords
gas turbine
turbine gondola
gondola
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.)
Expired - Lifetime
Application number
DE69204293T
Other languages
English (en)
Other versions
DE69204293T2 (de
Inventor
Arnold 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
Application granted granted Critical
Publication of DE69204293D1 publication Critical patent/DE69204293D1/de
Publication of DE69204293T2 publication Critical patent/DE69204293T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE69204293T 1991-08-07 1992-06-03 Gasturbinengondelanlage. Expired - Lifetime DE69204293T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB919116986A GB9116986D0 (en) 1991-08-07 1991-08-07 Gas turbine engine nacelle assembly
PCT/GB1992/000994 WO1993002920A1 (en) 1991-08-07 1992-06-03 Gas turbine engine nacelle assembly

Publications (2)

Publication Number Publication Date
DE69204293D1 true DE69204293D1 (de) 1995-09-28
DE69204293T2 DE69204293T2 (de) 1996-01-25

Family

ID=10699607

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69204293T Expired - Lifetime DE69204293T2 (de) 1991-08-07 1992-06-03 Gasturbinengondelanlage.

Country Status (6)

Country Link
US (1) US5497961A (de)
EP (1) EP0597861B1 (de)
JP (1) JPH06509531A (de)
DE (1) DE69204293T2 (de)
GB (1) GB9116986D0 (de)
WO (1) WO1993002920A1 (de)

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* Cited by examiner, † Cited by third party
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EP0784564B1 (de) * 1994-10-18 1998-12-30 United Technologies Corporation Gondel und ihre halterungsvorrichtung auf einem flugzeug
GB9921935D0 (en) 1999-09-17 1999-11-17 Rolls Royce A nacelle assembly for a gas turbine engine
US6220546B1 (en) 1999-12-29 2001-04-24 The Boeing Company Aircraft engine and associated aircraft engine cowl
GB2359052B (en) * 2000-02-09 2003-09-17 Rolls Royce Plc Engine arrangement
JP4426467B2 (ja) * 2003-04-28 2010-03-03 スネクマ ターボプロップエンジンの空気取入口装置
GB0312490D0 (en) * 2003-06-02 2003-07-09 Rolls Royce Plc Aeroengine nacelle
US7090165B2 (en) * 2003-06-02 2006-08-15 Rolls-Royce Plc Aeroengine nacelle
GB0315431D0 (en) * 2003-07-02 2003-08-06 Rolls Royce Plc Aircraft configuration
US7607286B2 (en) * 2004-12-01 2009-10-27 United Technologies Corporation Regenerative turbine blade and vane cooling for a tip turbine engine
EP1828567B1 (de) 2004-12-01 2011-10-12 United Technologies Corporation Diffusor-ansaugung für einen spitzenturbinenmotor
WO2006060006A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine non-metallic tailcone
US8096753B2 (en) * 2004-12-01 2012-01-17 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
WO2006060003A2 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
WO2006060001A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Fan rotor assembly for a tip turbine engine
US7976273B2 (en) * 2004-12-01 2011-07-12 United Technologies Corporation Tip turbine engine support structure
US20090169385A1 (en) * 2004-12-01 2009-07-02 Suciu Gabriel L Fan-turbine rotor assembly with integral inducer section for a tip turbine engine
US7854112B2 (en) * 2004-12-01 2010-12-21 United Technologies Corporation Vectoring transition duct for turbine engine
US7934902B2 (en) * 2004-12-01 2011-05-03 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
WO2006060013A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
US20080219833A1 (en) * 2004-12-01 2008-09-11 United Technologies Corporation Inducer for a Fan Blade of a Tip Turbine Engine
US7882694B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Variable fan inlet guide vane assembly for gas turbine engine
US8365511B2 (en) * 2004-12-01 2013-02-05 United Technologies Corporation Tip turbine engine integral case, vane, mount and mixer
DE602004027766D1 (de) * 2004-12-01 2010-07-29 United Technologies Corp Hydraulische dichtung für ein getriebe eines spitzenturbinenmotors
WO2006059997A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Annular turbine ring rotor
US8087885B2 (en) * 2004-12-01 2012-01-03 United Technologies Corporation Stacked annular components for turbine engines
WO2006059970A2 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
WO2006112807A2 (en) 2004-12-01 2006-10-26 United Technologies Corporation Turbine engine and method for starting a turbine engine
WO2006059985A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Axial compressor for tip turbine engine
EP1828591B1 (de) * 2004-12-01 2010-07-21 United Technologies Corporation Umfangsbrennkammer für spitzenturbinenmotor
US20090148273A1 (en) * 2004-12-01 2009-06-11 Suciu Gabriel L Compressor inlet guide vane for tip turbine engine and corresponding control method
EP1831519B1 (de) * 2004-12-01 2010-08-04 United Technologies Corporation Tip-Turbinentriebwerk mit mehreren Gebläse- und Turbinenstufen
EP1828547B1 (de) 2004-12-01 2011-11-30 United Technologies Corporation Turbofantriebwerk mit einer Mehrzahl von einzeln steuerbaren Einlassleitschaufeln und zugehöriges Steuerverfahren
US8083030B2 (en) * 2004-12-01 2011-12-27 United Technologies Corporation Gearbox lubrication supply system for a tip engine
WO2006059988A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Modular tip turbine engine
US7959406B2 (en) * 2004-12-01 2011-06-14 United Technologies Corporation Close coupled gearbox assembly for a tip turbine engine
US9003759B2 (en) 2004-12-01 2015-04-14 United Technologies Corporation Particle separator for tip turbine engine
US8061968B2 (en) * 2004-12-01 2011-11-22 United Technologies Corporation Counter-rotating compressor case and assembly method for tip turbine engine
US7874802B2 (en) * 2004-12-01 2011-01-25 United Technologies Corporation Tip turbine engine comprising turbine blade clusters and method of assembly
EP1831520B1 (de) * 2004-12-01 2009-02-25 United Technologies Corporation Tip-turbinentriebwerk und entsprechendes betriebsverfahren
EP1825112B1 (de) * 2004-12-01 2013-10-23 United Technologies Corporation Freigetragene tipturbinentriebwerk
WO2006059971A2 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine integral fan, combustor, and turbine case
EP1825177B1 (de) 2004-12-01 2012-01-25 United Technologies Corporation Aufblasbares ablassventil für eine turbomaschine und verfahren zur steuerung von ablassluft
WO2006060009A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Turbine blade engine comprising turbine clusters and radial attachment lock arrangement therefor
US8807936B2 (en) * 2004-12-01 2014-08-19 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
EP1825113B1 (de) 2004-12-01 2012-10-24 United Technologies Corporation Gegenläufiges getriebe für ein tip-turbinen-triebwerk
WO2006059994A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a tip turbine engine
US7980054B2 (en) * 2004-12-01 2011-07-19 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
WO2006060011A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
US7631485B2 (en) 2004-12-01 2009-12-15 United Technologies Corporation Tip turbine engine with a heat exchanger
EP1841960B1 (de) * 2004-12-01 2011-05-25 United Technologies Corporation Starter-generatorsystem für einen spitzenturbinenmotor
EP1828683B1 (de) 2004-12-01 2013-04-10 United Technologies Corporation Brennkammer für turbinenmotor
US9109537B2 (en) * 2004-12-04 2015-08-18 United Technologies Corporation Tip turbine single plane mount
US20060145001A1 (en) * 2004-12-30 2006-07-06 Smith Matthew C Fan cowl door elimination
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
FR2887521B1 (fr) * 2005-06-28 2007-08-17 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un dispositif d'accrochage d'un tel moteur
GB0516066D0 (en) * 2005-08-04 2005-09-14 Airbus Uk Ltd Removal of components from aircraft
FR2891254B1 (fr) * 2005-09-29 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef
FR2900907B1 (fr) * 2006-05-09 2008-12-19 Airbus France Sas Ensemble moteur pour aeronef a nacelle et mat integres
US7721525B2 (en) * 2006-07-19 2010-05-25 Rohr, Inc. Aircraft engine inlet having zone of deformation
FR2905990A1 (fr) * 2006-09-20 2008-03-21 Snecma Sa Systeme propulsif a pylone integre pour avion.
WO2008043903A2 (fr) * 2006-10-11 2008-04-17 Aircelle Nacelle pour turboréacteur double flux
FR2913664B1 (fr) * 2007-03-16 2009-07-24 Aircelle Sa Nacelle pour turboreacteur double flux
FR2907098B1 (fr) * 2006-10-11 2010-04-16 Aircelle Sa Nacelle pour turboreacteur double flux
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
FR2917710A1 (fr) * 2007-06-22 2008-12-26 Aircelle Sa Platine de fixation et longeron de manutention d'ensemble propulsif monobloc d'un aeronef
US11149650B2 (en) 2007-08-01 2021-10-19 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
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
US20150377123A1 (en) 2007-08-01 2015-12-31 United Technologies Corporation Turbine section of high bypass turbofan
US11346289B2 (en) 2007-08-01 2022-05-31 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon Technologies Corporation Turbine section of high bypass turbofan
FR2926285B1 (fr) * 2008-01-15 2009-12-11 Aircelle Sa Nacelle a capotage simplifie
US8118251B2 (en) * 2008-01-18 2012-02-21 United Technologies Corporation Mounting system for a gas turbine engine
FR2928347B1 (fr) * 2008-03-07 2010-06-25 Aircelle Sa Structure d'accrochage pour turboreacteur
US8167237B2 (en) * 2008-03-21 2012-05-01 United Technologies Corporation Mounting system for a gas turbine engine
US8800914B2 (en) 2008-06-02 2014-08-12 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
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
US8695920B2 (en) 2008-06-02 2014-04-15 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US20130232768A1 (en) 2012-03-12 2013-09-12 United Technologies Corporation Turbine engine case mount and dismount
US9091210B2 (en) * 2012-04-26 2015-07-28 United Technologies Corporation TEC mount redundant fastening
US9581108B2 (en) 2013-02-22 2017-02-28 United Technologies Corporation Pivot thrust reverser with multi-point actuation
US9694912B2 (en) 2013-02-22 2017-07-04 United Technologies Corporation ATR guide pins for sliding nacelle
US9435293B2 (en) 2013-02-22 2016-09-06 United Technologies Corporation Full ring sliding nacelle with thrust reverser
FR3010147B1 (fr) 2013-08-28 2015-08-21 Snecma Suspension isostatique d'un turboreacteur par double support arriere
US10371047B2 (en) 2013-10-16 2019-08-06 United Technologies Corporation Geared turbofan engine with targeted modular efficiency
DE102015226546A1 (de) * 2015-12-22 2017-06-22 Rolls-Royce Deutschland Ltd & Co Kg Triebwerksverkleidung
US9972896B2 (en) * 2016-06-23 2018-05-15 General Electric Company Wireless aircraft engine monitoring system

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2863620A (en) * 1952-10-04 1958-12-09 Sud Aviation Jet-propelled aircraft
FR1471132A (fr) * 1966-03-15 1967-02-24 Rolls Royce Structure pour le montage de moteurs applicables, notamment, aux avions
US3561707A (en) * 1969-06-24 1971-02-09 United Aircraft Corp Thrust mount
US3848832A (en) * 1973-03-09 1974-11-19 Boeing Co Aircraft engine installation
GB1516980A (en) * 1974-12-24 1978-07-05 Rolls Royce Mounting ducted fan gas turbine engines on aircraft
US3979087A (en) * 1975-07-02 1976-09-07 United Technologies Corporation Engine mount
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
US4603821A (en) * 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine

Also Published As

Publication number Publication date
EP0597861A1 (de) 1994-05-25
GB9116986D0 (en) 1991-10-09
DE69204293T2 (de) 1996-01-25
JPH06509531A (ja) 1994-10-27
EP0597861B1 (de) 1995-08-23
WO1993002920A1 (en) 1993-02-18
US5497961A (en) 1996-03-12

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