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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JP3599342B2 (ja) * 1994-10-18 2004-12-08 ユナイテッド テクノロジーズ コーポレイション 航空機エンジンのためのナセル及びその取り付け配置
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
US7090165B2 (en) * 2003-06-02 2006-08-15 Rolls-Royce Plc Aeroengine nacelle
GB0312490D0 (en) * 2003-06-02 2003-07-09 Rolls Royce Plc Aeroengine nacelle
GB0315431D0 (en) * 2003-07-02 2003-08-06 Rolls Royce Plc Aircraft configuration
DE602004019710D1 (de) * 2004-12-01 2009-04-09 United Technologies Corp Fernbetätigung für eine verstellbare stufe eines verdichters für einen turbinenmotor
US7959532B2 (en) * 2004-12-01 2011-06-14 United Technologies Corporation Hydraulic seal for a gearbox of a tip turbine engine
DE602004016065D1 (de) * 2004-12-01 2008-10-02 United Technologies Corp Variable gebläseeinlassleitschaufelanordnung, turbinenmotor mit solch einer anordnung und entsprechendes steuerverfahren
US8757959B2 (en) * 2004-12-01 2014-06-24 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
DE602004020125D1 (de) * 2004-12-01 2009-04-30 United Technologies Corp Schmiermittel-versorgungssystem für das getriebe eines tip-turbinen-triebwerks
US8096753B2 (en) * 2004-12-01 2012-01-17 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
US9003759B2 (en) 2004-12-01 2015-04-14 United Technologies Corporation Particle separator for tip turbine engine
DE602004016059D1 (de) 2004-12-01 2008-10-02 United Technologies Corp Tip-turbinentriebwerk mit wärmetauscher
EP1825116A2 (de) * 2004-12-01 2007-08-29 United Technologies Corporation Ejektor-kühlung des aussengehäuses eines tip-turbinen-triebwerks
US7883315B2 (en) * 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
US8468795B2 (en) 2004-12-01 2013-06-25 United Technologies Corporation Diffuser aspiration for a tip turbine engine
EP2333286A1 (de) * 2004-12-01 2011-06-15 United Technologies Corporation Überleitkanal für Schubvektorsteuerung eines Turbinentriebwerks
US8033092B2 (en) * 2004-12-01 2011-10-11 United Technologies Corporation Tip turbine engine integral fan, combustor, and turbine case
WO2006059988A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Modular tip turbine engine
WO2006060006A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine non-metallic tailcone
DE602004031679D1 (de) * 2004-12-01 2011-04-14 United Technologies Corp Regenerative Kühlung einer Leit- und Laufschaufel für ein Tipturbinentriebwerk
US8807936B2 (en) * 2004-12-01 2014-08-19 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
WO2006060005A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Fan-turbine rotor assembly with integral inducer section for a tip turbine engine
EP1825177B1 (de) 2004-12-01 2012-01-25 United Technologies Corporation Aufblasbares ablassventil für eine turbomaschine und verfahren zur steuerung von ablassluft
WO2006059994A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a tip turbine engine
WO2006060004A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Combustor for turbine engine
WO2006060014A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Starter generator system for a tip turbine engine
WO2006059999A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method
EP1825117B1 (de) * 2004-12-01 2012-06-13 United Technologies Corporation Turbinentriebwerk mit von einem differentialgetriebe angetriebenem fan und verdichter
DE602004031986D1 (de) * 2004-12-01 2011-05-05 United Technologies Corp Gebläse-turbinen-rotoranordnung für einen spitzenturbinenmotor
WO2006060010A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Compressor inlet guide vane for tip turbine engine and corresponding control method
WO2006059974A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Close coupled gearbox assembly for a tip turbine engine
US7937927B2 (en) 2004-12-01 2011-05-10 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
US7882695B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Turbine blow down starter for turbine engine
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
EP1825111B1 (de) * 2004-12-01 2011-08-31 United Technologies Corporation Gegenläufiges kompressorgehäuse für ein tip-turbinentriebwerk
DE602004032186D1 (de) * 2004-12-01 2011-05-19 United Technologies Corp Turbinenschaufelgruppe eines Fanrotors sowie Verfahren zur Montage einer solchen Gruppe
WO2006059978A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Cantilevered tip turbine engine
EP1828591B1 (de) * 2004-12-01 2010-07-21 United Technologies Corporation Umfangsbrennkammer für spitzenturbinenmotor
US8152469B2 (en) 2004-12-01 2012-04-10 United Technologies Corporation Annular turbine ring rotor
EP1834071B1 (de) * 2004-12-01 2013-03-13 United Technologies Corporation Einlaufteil für einen lüfterflügel eines spitzenturbinenmotors
WO2006059979A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine integral case, vane, mount, and mixer
WO2006059985A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Axial compressor for tip turbine engine
WO2006059977A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine and corresponding orepating method
DE602004023769D1 (de) * 2004-12-01 2009-12-03 United Technologies Corp Gestapelte ringförmige bauteile für turbinenmotoren
EP1831519B1 (de) * 2004-12-01 2010-08-04 United Technologies Corporation Tip-Turbinentriebwerk mit mehreren Gebläse- und Turbinenstufen
US7976273B2 (en) * 2004-12-01 2011-07-12 United Technologies Corporation Tip turbine engine support structure
WO2006060012A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine comprising turbine blade clusters and method of assembly
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.
RU2453477C2 (ru) * 2006-10-11 2012-06-20 Эрсель Гондола для двухконтурного турбореактивного двигателя
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
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
US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon 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
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
US20150377123A1 (en) 2007-08-01 2015-12-31 United 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
US8807477B2 (en) 2008-06-02 2014-08-19 United Technologies Corporation Gas turbine engine compressor arrangement
US8511605B2 (en) 2008-06-02 2013-08-20 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
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
US20140174056A1 (en) 2008-06-02 2014-06-26 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
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
US9822734B2 (en) 2013-02-22 2017-11-21 United Technologies Corporation Tandem thrust reverser with multi-bar linkage
US9573695B2 (en) 2013-02-22 2017-02-21 United Technologies Corporation Integrated nozzle and plug
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
EP3058202A4 (de) 2013-10-16 2017-06-28 United Technologies Corporation Turbogebläsemotor mit gezielter modularer wirkung
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

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

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