DE69521816T2 - Druckkontrolle eines verdichters mittels messung eines asymetrischen luftstroms - Google Patents

Druckkontrolle eines verdichters mittels messung eines asymetrischen luftstroms

Info

Publication number
DE69521816T2
DE69521816T2 DE69521816T DE69521816T DE69521816T2 DE 69521816 T2 DE69521816 T2 DE 69521816T2 DE 69521816 T DE69521816 T DE 69521816T DE 69521816 T DE69521816 T DE 69521816T DE 69521816 T2 DE69521816 T2 DE 69521816T2
Authority
DE
Germany
Prior art keywords
asymetrical
airflow
compressor
measuring
pressure control
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
DE69521816T
Other languages
English (en)
Other versions
DE69521816D1 (de
Inventor
Kevin M Eveker
Daniel L Gysling
Carl N Nett
Hua O Wang
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DE69521816D1 publication Critical patent/DE69521816D1/de
Publication of DE69521816T2 publication Critical patent/DE69521816T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/001Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/10Purpose of the control system to cope with, or avoid, compressor flow instabilities
    • F05D2270/101Compressor surge or stall

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
DE69521816T 1994-12-14 1995-11-02 Druckkontrolle eines verdichters mittels messung eines asymetrischen luftstroms Expired - Lifetime DE69521816T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US35576394A 1994-12-14 1994-12-14
PCT/US1995/017145 WO1997000381A1 (en) 1994-12-14 1995-11-02 Compressor stall and surge control using airflow asymmetry measurement

Publications (2)

Publication Number Publication Date
DE69521816D1 DE69521816D1 (de) 2001-08-23
DE69521816T2 true DE69521816T2 (de) 2002-04-04

Family

ID=23398743

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69521816T Expired - Lifetime DE69521816T2 (de) 1994-12-14 1995-11-02 Druckkontrolle eines verdichters mittels messung eines asymetrischen luftstroms

Country Status (6)

Country Link
US (1) US5915917A (de)
EP (1) EP0839285B1 (de)
JP (1) JP2997319B2 (de)
AU (1) AU1183997A (de)
DE (1) DE69521816T2 (de)
WO (1) WO1997000381A1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014106522B4 (de) * 2013-05-24 2020-09-03 GM Global Technology Operations LLC (n. d. Gesetzen des Staates Delaware) Systeme und Verfahren zum Detektieren eines Kompressordruckstoßes

Families Citing this family (196)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6141951A (en) * 1998-08-18 2000-11-07 United Technologies Corporation Control system for modulating bleed in response to engine usage
US6289274B1 (en) 1999-08-13 2001-09-11 United Technologies Corporation Fuzzy logic based fuel flow selection system
DE19951476A1 (de) * 1999-10-26 2001-05-03 Wilo Gmbh Rotorpaketbefestigung auf Keramikwelle
US6364602B1 (en) * 2000-01-06 2002-04-02 General Electric Company Method of air-flow measurement and active operating limit line management for compressor surge avoidance
FR2804732B1 (fr) * 2000-02-03 2002-04-12 Snecma Procede de detection precoce des instabilites aerodynamiques dans un compresseur de turbomachine
DE10012380A1 (de) * 2000-03-14 2001-09-20 Man Turbomasch Ag Ghh Borsig Verfahren zum Schutz eines Turbokompressors vor Betrieb im instabilen Arbeitsbereich
US6582183B2 (en) 2000-06-30 2003-06-24 United Technologies Corporation Method and system of flutter control for rotary compression systems
US6506010B1 (en) * 2001-04-17 2003-01-14 General Electric Company Method and apparatus for compressor control and operation in industrial gas turbines using stall precursors
JP2002364582A (ja) * 2001-06-11 2002-12-18 Ishikawajima Harima Heavy Ind Co Ltd 軸流圧縮機におけるストール予知方法
US6503048B1 (en) * 2001-08-27 2003-01-07 Compressor Controls Corporation Method and apparatus for estimating flow in compressors with sidestreams
DE10152026A1 (de) * 2001-10-23 2004-02-19 Mtu Aero Engines Gmbh Warnung vor Pumpgrenze oder Schaufelschaden bei einer Turbomaschine
DE10163649B4 (de) * 2001-12-21 2013-04-25 Mtu Aero Engines Gmbh Turboverdichter und Gasturbine mit Einlaufschwingungswarnung bei Axialschwingung der Luftsäule im Einlauf sowie Auswerteverfahren hierfür
JP4069675B2 (ja) * 2002-05-22 2008-04-02 株式会社日立プラントテクノロジー ターボ圧縮機およびその容量制御方法
CN101082344B (zh) * 2002-08-23 2010-06-16 约克国际公司 用于探测离心压缩机内的旋转失速的方法
US7003426B2 (en) * 2002-10-04 2006-02-21 General Electric Company Method and system for detecting precursors to compressor stall and surge
US6871487B2 (en) * 2003-02-14 2005-03-29 Kulite Semiconductor Products, Inc. System for detecting and compensating for aerodynamic instabilities in turbo-jet engines
US7356999B2 (en) 2003-10-10 2008-04-15 York International Corporation System and method for stability control in a centrifugal compressor
US7905102B2 (en) 2003-10-10 2011-03-15 Johnson Controls Technology Company Control system
US7159401B1 (en) * 2004-12-23 2007-01-09 Kulite Semiconductor Products, Inc. System for detecting and compensating for aerodynamic instabilities in turbo-jet engines
US7465145B2 (en) * 2005-03-17 2008-12-16 United Technologies Corporation Tip clearance control system
US7668704B2 (en) * 2006-01-27 2010-02-23 Ricardo, Inc. Apparatus and method for compressor and turbine performance simulation
JP4890095B2 (ja) * 2006-05-19 2012-03-07 株式会社Ihi ストール予兆検知装置及び方法、並びにエンジン制御システム
US8667688B2 (en) 2006-07-05 2014-03-11 United Technologies Corporation Method of assembly for gas turbine fan drive gear system
US7704178B2 (en) 2006-07-05 2010-04-27 United Technologies Corporation Oil baffle for gas turbine fan drive gear system
US9976437B2 (en) 2006-08-15 2018-05-22 United Technologies Corporation Epicyclic gear train
US8858388B2 (en) 2006-08-15 2014-10-14 United Technologies Corporation Gas turbine engine gear train
US8753243B2 (en) 2006-08-15 2014-06-17 United Technologies Corporation Ring gear mounting arrangement with oil scavenge scheme
US10107231B2 (en) 2006-08-15 2018-10-23 United Technologies Corporation Gas turbine engine with geared architecture
US7827803B1 (en) 2006-09-27 2010-11-09 General Electric Company Method and apparatus for an aerodynamic stability management system
WO2008045081A1 (en) 2006-10-12 2008-04-17 United Technologies Corporation Variable fan nozzle using shape memory material
EP2074298B1 (de) 2006-10-12 2013-03-13 United Technologies Corporation Durch eine düse mit variablem querschnitt unterstützter neustart einens turbinentriebwerks
US8104262B2 (en) 2006-10-12 2012-01-31 United Technologies Corporation Dual function cascade integrated variable area fan nozzle and thrust reverser
US20080273961A1 (en) 2007-03-05 2008-11-06 Rosenkrans William E Flutter sensing and control system for a gas turbine engine
US11486311B2 (en) 2007-08-01 2022-11-01 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
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
US8844265B2 (en) 2007-08-01 2014-09-30 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
US9494084B2 (en) 2007-08-23 2016-11-15 United Technologies Corporation Gas turbine engine with fan variable area nozzle for low fan pressure ratio
US10167813B2 (en) 2007-08-23 2019-01-01 United Technologies Corporation Gas turbine engine with fan variable area nozzle to reduce fan instability
US9701415B2 (en) 2007-08-23 2017-07-11 United Technologies Corporation Gas turbine engine with axial movable fan variable area nozzle
US9957918B2 (en) 2007-08-28 2018-05-01 United Technologies Corporation Gas turbine engine front architecture
US20140157754A1 (en) 2007-09-21 2014-06-12 United Technologies Corporation Gas turbine engine compressor arrangement
US10151248B2 (en) 2007-10-03 2018-12-11 United Technologies Corporation Dual fan gas turbine engine and gear train
US20140174056A1 (en) 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8973364B2 (en) 2008-06-26 2015-03-10 United Technologies Corporation Gas turbine engine with noise attenuating variable area fan nozzle
US9885313B2 (en) 2009-03-17 2018-02-06 United Technologes Corporation Gas turbine engine bifurcation located fan variable area nozzle
GB0915616D0 (en) * 2009-09-08 2009-10-07 Rolls Royce Plc Surge margin regulation
US10041442B2 (en) 2010-06-11 2018-08-07 United Technologies Corporation Variable area fan nozzle
US9995174B2 (en) 2010-10-12 2018-06-12 United Technologies Corporation Planetary gear system arrangement with auxiliary oil system
US10605167B2 (en) 2011-04-15 2020-03-31 United Technologies Corporation Gas turbine engine front center body architecture
US9631558B2 (en) 2012-01-03 2017-04-25 United Technologies Corporation Geared architecture for high speed and small volume fan drive turbine
US9239012B2 (en) 2011-06-08 2016-01-19 United Technologies Corporation Flexible support structure for a geared architecture gas turbine engine
US9410608B2 (en) 2011-06-08 2016-08-09 United Technologies Corporation Flexible support structure for a geared architecture gas turbine engine
US9909505B2 (en) 2011-07-05 2018-03-06 United Technologies Corporation Efficient, low pressure ratio propulsor for gas turbine engines
US9506422B2 (en) 2011-07-05 2016-11-29 United Technologies Corporation Efficient, low pressure ratio propulsor for gas turbine engines
US9938898B2 (en) 2011-07-29 2018-04-10 United Technologies Corporation Geared turbofan bearing arrangement
US9334802B2 (en) 2011-10-31 2016-05-10 United Technologies Corporation Gas turbine engine thermal management system
US9416677B2 (en) 2012-01-10 2016-08-16 United Technologies Corporation Gas turbine engine forward bearing compartment architecture
US9004849B2 (en) 2012-01-10 2015-04-14 United Technologies Corporation Gas turbine engine forward bearing compartment architecture
US10125724B2 (en) 2012-01-17 2018-11-13 United Technologies Corporation Start system for gas turbine engines
US20130186058A1 (en) 2012-01-24 2013-07-25 William G. Sheridan Geared turbomachine fan and compressor rotation
US9970352B2 (en) 2012-01-27 2018-05-15 United Technologies Corporation Turbomachine fan clutch
US9447694B2 (en) 2012-01-30 2016-09-20 United Technologies Corporation Internal manifold for turning mid-turbine frame flow distribution
US9611859B2 (en) 2012-01-31 2017-04-04 United Technologies Corporation Gas turbine engine with high speed low pressure turbine section and bearing support features
US8375699B1 (en) 2012-01-31 2013-02-19 United Technologies Corporation Variable area fan nozzle with wall thickness distribution
US20130192195A1 (en) 2012-01-31 2013-08-01 Eric J. Wehmeier Gas turbine engine with compressor inlet guide vane positioned for starting
US9816442B2 (en) 2012-01-31 2017-11-14 United Technologies Corporation Gas turbine engine with high speed low pressure turbine section
US10400629B2 (en) 2012-01-31 2019-09-03 United Technologies Corporation Gas turbine engine shaft bearing configuration
US20150345426A1 (en) 2012-01-31 2015-12-03 United Technologies Corporation Geared turbofan gas turbine engine architecture
US20150192070A1 (en) 2012-01-31 2015-07-09 United Technologies Corporation Geared turbofan gas turbine engine architecture
US8402741B1 (en) 2012-01-31 2013-03-26 United Technologies Corporation Gas turbine engine shaft bearing configuration
US8863491B2 (en) 2012-01-31 2014-10-21 United Technologies Corporation Gas turbine engine shaft bearing configuration
US10287914B2 (en) 2012-01-31 2019-05-14 United Technologies Corporation Gas turbine engine with high speed low pressure turbine section and bearing support features
US9476320B2 (en) 2012-01-31 2016-10-25 United Technologies Corporation Gas turbine engine aft bearing arrangement
US10502135B2 (en) 2012-01-31 2019-12-10 United Technologies Corporation Buffer system for communicating one or more buffer supply airs throughout a gas turbine engine
US10113434B2 (en) 2012-01-31 2018-10-30 United Technologies Corporation Turbine blade damper seal
US10145266B2 (en) 2012-01-31 2018-12-04 United Technologies Corporation Gas turbine engine shaft bearing arrangement
US20130192191A1 (en) 2012-01-31 2013-08-01 Frederick M. Schwarz Gas turbine engine with high speed low pressure turbine section and bearing support features
US8869508B2 (en) 2012-01-31 2014-10-28 United Technologies Corporation Gas turbine engine variable area fan nozzle control
US9835052B2 (en) 2012-01-31 2017-12-05 United Technologies Corporation Gas turbine engine with high speed low pressure turbine section and bearing support features
US8935913B2 (en) 2012-01-31 2015-01-20 United Technologies Corporation Geared turbofan gas turbine engine architecture
US9394852B2 (en) 2012-01-31 2016-07-19 United Technologies Corporation Variable area fan nozzle with wall thickness distribution
US10724431B2 (en) 2012-01-31 2020-07-28 Raytheon Technologies Corporation Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine
US10018116B2 (en) 2012-01-31 2018-07-10 United Technologies Corporation Gas turbine engine buffer system providing zoned ventilation
US9845726B2 (en) 2012-01-31 2017-12-19 United Technologies Corporation Gas turbine engine with high speed low pressure turbine section
US9169781B2 (en) 2012-01-31 2015-10-27 United Technologies Corporation Turbine engine gearbox
US20130192240A1 (en) 2012-01-31 2013-08-01 Peter M. Munsell Buffer system for a gas turbine engine
US10415468B2 (en) 2012-01-31 2019-09-17 United Technologies Corporation Gas turbine engine buffer system
US9593628B2 (en) 2012-01-31 2017-03-14 United Technologies Corporation Gas turbine engine variable area fan nozzle with ice management
US10240526B2 (en) 2012-01-31 2019-03-26 United Technologies Corporation Gas turbine engine with high speed low pressure turbine section
US8443582B1 (en) 2012-01-31 2013-05-21 United Technologies Corporation Gas turbine engine with geared turbofan and oil thermal management system
US8366382B1 (en) 2012-01-31 2013-02-05 United Technologies Corporation Mid-turbine frame buffer system
US20130192198A1 (en) 2012-01-31 2013-08-01 Lisa I. Brilliant Compressor flowpath
US20130192251A1 (en) 2012-01-31 2013-08-01 Peter M. Munsell Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine
US10837367B2 (en) 2012-02-28 2020-11-17 Raytheon Technologies Corporation Acoustic treatment in an unducted area of a geared turbomachine
US9856745B2 (en) 2012-02-28 2018-01-02 United Technologies Corporation Acoustic treatment in an unducted area of a geared turbomachine
US10060390B2 (en) 2012-02-29 2018-08-28 United Technologies Corporation Bypass duct with angled drag links
US10309232B2 (en) 2012-02-29 2019-06-04 United Technologies Corporation Gas turbine engine with stage dependent material selection for blades and disk
US9297270B2 (en) 2012-02-29 2016-03-29 United Technologies Corporation Gas turbine engine driving multiple fans
US10107191B2 (en) 2012-02-29 2018-10-23 United Technologies Corporation Geared gas turbine engine with reduced fan noise
US8790075B2 (en) 2012-03-30 2014-07-29 United Technologies Corporation Gas turbine engine geared architecture axial retention arrangement
US10036351B2 (en) 2012-04-02 2018-07-31 United Technologies Corporation Geared turbofan with three co-rotating turbines
US10125693B2 (en) 2012-04-02 2018-11-13 United Technologies Corporation Geared turbofan engine with power density range
US10138809B2 (en) 2012-04-02 2018-11-27 United Technologies Corporation Geared turbofan engine with a high ratio of thrust to turbine volume
US10018119B2 (en) 2012-04-02 2018-07-10 United Technologies Corporation Geared architecture with inducer for gas turbine engine
US9074485B2 (en) 2012-04-25 2015-07-07 United Technologies Corporation Geared turbofan with three turbines all counter-rotating
US10036350B2 (en) 2012-04-30 2018-07-31 United Technologies Corporation Geared turbofan with three turbines all co-rotating
US8572943B1 (en) 2012-05-31 2013-11-05 United Technologies Corporation Fundamental gear system architecture
US20150308351A1 (en) 2012-05-31 2015-10-29 United Technologies Corporation Fundamental gear system architecture
US9476323B2 (en) 2012-05-31 2016-10-25 United Technologies Corporation Turbine gear assembly support having symmetrical removal features
US9328818B2 (en) 2012-09-21 2016-05-03 United Technologies Corporation Gear carrier flex mount lubrication
US8753065B2 (en) 2012-09-27 2014-06-17 United Technologies Corporation Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
EP2900968B1 (de) 2012-09-28 2018-10-31 United Technologies Corporation Strömungsmessendes t-rohr mit geteilter zone
US20160138474A1 (en) 2012-09-28 2016-05-19 United Technologies Corporation Low noise compressor rotor for geared turbofan engine
US9624834B2 (en) 2012-09-28 2017-04-18 United Technologies Corporation Low noise compressor rotor for geared turbofan engine
WO2014055102A1 (en) 2012-10-01 2014-04-10 United Technologies Corporation Low weight large fan gas turbine engine
US10036316B2 (en) 2012-10-02 2018-07-31 United Technologies Corporation Geared turbofan engine with high compressor exit temperature
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WO2014058710A1 (en) 2012-10-09 2014-04-17 United Technologies Corporation Improved operability geared turbofan engine including compressor section variable guide vanes
US9932933B2 (en) 2012-12-20 2018-04-03 United Technologies Corporation Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US9920653B2 (en) 2012-12-20 2018-03-20 United Technologies Corporation Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US10436120B2 (en) 2013-02-06 2019-10-08 United Technologies Corporation Exhaust nozzle for an elongated gear turbofan with high bypass ratio
WO2014158439A1 (en) 2013-03-12 2014-10-02 United Technologies Corporation Flexible coupling for geared turbine engine
US11719161B2 (en) 2013-03-14 2023-08-08 Raytheon Technologies Corporation Low noise turbine for geared gas turbine engine
US10605172B2 (en) 2013-03-14 2020-03-31 United Technologies Corporation Low noise turbine for geared gas turbine engine
WO2014151785A1 (en) 2013-03-15 2014-09-25 United Technologies Corporation Turbofan engine bearing and gearbox arrangement
US9624827B2 (en) 2013-03-15 2017-04-18 United Technologies Corporation Thrust efficient turbofan engine
US10724479B2 (en) 2013-03-15 2020-07-28 United Technologies Corporation Thrust efficient turbofan engine
EP2994628A4 (de) 2013-05-09 2017-01-18 United Technologies Corporation Stirnteil für turbofantriebwerk
US10316758B2 (en) 2013-05-09 2019-06-11 United Technologies Corporation Turbofan engine front section
US10215053B2 (en) 2013-07-07 2019-02-26 United Technologies Corporation Fan drive gear system manifold radial tube filters
US20150300264A1 (en) 2013-09-30 2015-10-22 United Technologies Corporation Geared turbofan architecture for regional jet aircraft
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US10267228B2 (en) 2013-10-31 2019-04-23 United Technologies Corporation Geared turbofan arrangement with core split power ratio
WO2015112212A2 (en) 2013-11-01 2015-07-30 United Technologies Corporation Geared turbofan arrangement with core split power ratio
US10502163B2 (en) 2013-11-01 2019-12-10 United Technologies Corporation Geared turbofan arrangement with core split power ratio
US8869504B1 (en) 2013-11-22 2014-10-28 United Technologies Corporation Geared turbofan engine gearbox arrangement
US9976489B2 (en) 2013-12-16 2018-05-22 United Technologies Corporation Gas turbine engine for long range aircraft
US9739205B2 (en) 2013-12-23 2017-08-22 United Technologies Corporation Geared turbofan with a gearbox upstream of a fan drive turbine
WO2015147948A2 (en) 2014-01-20 2015-10-01 United Technologies Corporation Geared gas turbine engine with reduced oil tank size
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US10590775B2 (en) 2014-02-19 2020-03-17 United Technologies Corporation Gas turbine engine airfoil
US9347323B2 (en) 2014-02-19 2016-05-24 United Technologies Corporation Gas turbine engine airfoil total chord relative to span
EP3108117B2 (de) 2014-02-19 2023-10-11 Raytheon Technologies Corporation Gasturbinenmotorschaufel
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WO2015175044A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
WO2015126450A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
EP3108103B1 (de) 2014-02-19 2023-09-27 Raytheon Technologies Corporation Fanschaufel für ein gastrubinentriebwerk
US9140127B2 (en) 2014-02-19 2015-09-22 United Technologies Corporation Gas turbine engine airfoil
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US10605259B2 (en) 2014-02-19 2020-03-31 United Technologies Corporation Gas turbine engine airfoil
WO2015126774A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
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WO2015126454A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
WO2015175058A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
WO2015175056A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
WO2015126452A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
US9567858B2 (en) 2014-02-19 2017-02-14 United Technologies Corporation Gas turbine engine airfoil
EP3108107B1 (de) 2014-02-19 2023-10-11 Raytheon Technologies Corporation Turboluftstrahltriebwerk mit getriebefan und niederdruckverdichterschaufeln
WO2015175043A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
US10280843B2 (en) 2014-03-07 2019-05-07 United Technologies Corporation Geared turbofan with integral front support and carrier
US9879608B2 (en) 2014-03-17 2018-01-30 United Technologies Corporation Oil loss protection for a fan drive gear system
US9828943B2 (en) 2014-06-09 2017-11-28 United Technologies Corporation Variable area nozzle for gas turbine engine
US9976490B2 (en) 2014-07-01 2018-05-22 United Technologies Corporation Geared gas turbine engine with oil deaerator
US10060289B2 (en) 2014-07-29 2018-08-28 United Technologies Corporation Geared gas turbine engine with oil deaerator and air removal
EP3045676A1 (de) * 2015-01-13 2016-07-20 Siemens Aktiengesellschaft Verfahren zur Vermeidung eines rotierenden Strömungsabrisses
US9333603B1 (en) 2015-01-28 2016-05-10 United Technologies Corporation Method of assembling gas turbine engine section
US9915225B2 (en) 2015-02-06 2018-03-13 United Technologies Corporation Propulsion system arrangement for turbofan gas turbine engine
US9470093B2 (en) 2015-03-18 2016-10-18 United Technologies Corporation Turbofan arrangement with blade channel variations
US10371168B2 (en) 2015-04-07 2019-08-06 United Technologies Corporation Modal noise reduction for gas turbine engine
US9874145B2 (en) 2015-04-27 2018-01-23 United Technologies Corporation Lubrication system for gas turbine engines
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US10508562B2 (en) 2015-12-01 2019-12-17 United Technologies Corporation Geared turbofan with four star/planetary gear reduction
US10047757B2 (en) 2016-06-22 2018-08-14 General Electric Company Predicting a surge event in a compressor of a turbomachine
US10669948B2 (en) 2017-01-03 2020-06-02 Raytheon Technologies Corporation Geared turbofan with non-epicyclic gear reduction system
US10738646B2 (en) 2017-06-12 2020-08-11 Raytheon Technologies Corporation Geared turbine engine with gear driving low pressure compressor and fan at common speed, and failsafe overspeed protection and shear section
US10724445B2 (en) 2018-01-03 2020-07-28 Raytheon Technologies Corporation Method of assembly for fan drive gear system with rotating carrier
US11092020B2 (en) 2018-10-18 2021-08-17 Raytheon Technologies Corporation Rotor assembly for gas turbine engines
US10815904B2 (en) * 2019-03-06 2020-10-27 General Electric Company Prognostic health management control for adaptive operability recovery for turbine engines
US11199437B2 (en) * 2019-04-19 2021-12-14 Purdue Research Foundation Utilization of fast-response pressure measurements to nonintrusively monitor blade vibration in axial compressors
US11629649B2 (en) 2020-05-11 2023-04-18 Raytheon Technologies Corporation Gas turbine engine with speed sensor
US11781506B2 (en) 2020-06-03 2023-10-10 Rtx Corporation Splitter and guide vane arrangement for gas turbine engines
US11725594B2 (en) 2020-08-31 2023-08-15 General Electric Company Hybrid electric engine speed regulation
US20220252007A1 (en) * 2021-02-08 2022-08-11 General Electric Company Active compressor stall recovery
US11814968B2 (en) 2021-07-19 2023-11-14 Rtx Corporation Gas turbine engine with idle thrust ratio
US11719245B2 (en) 2021-07-19 2023-08-08 Raytheon Technologies Corporation Compressor arrangement for a gas turbine engine
US11754000B2 (en) 2021-07-19 2023-09-12 Rtx Corporation High and low spool configuration for a gas turbine engine
US11719165B2 (en) * 2021-11-03 2023-08-08 Pratt & Whitney Canada Corp. Air inlet strut for aircraft engine
US20240017823A1 (en) * 2022-07-18 2024-01-18 Textron Innovations Inc. Optimizing usage of supplemental engine power
US12006880B2 (en) 2022-09-12 2024-06-11 General Electric Company High bandwidth control of turbofan/turboprop thrust response using embedded electric machines

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4550564A (en) * 1984-03-19 1985-11-05 United Technologies Corporation Engine surge prevention system
DE3544821A1 (de) * 1985-12-18 1987-06-19 Gutehoffnungshuette Man Verfahren zum regeln von turbokompressoren zur vermeidung des pumpens
US4781524A (en) * 1987-02-12 1988-11-01 Man Gutehoffnungshuette Gmbh Method and apparatus for detecting pressure surges in a turbo-compressor
US4967550A (en) * 1987-04-28 1990-11-06 Rolls-Royce Plc Active control of unsteady motion phenomena in turbomachinery
US5275528A (en) * 1990-08-28 1994-01-04 Rolls-Royce Plc Flow control method and means
DE4140597C1 (en) * 1991-12-10 1993-05-19 Zollmann Gmbh, 7419 Sonnenbuehl, De Tool chuck with inner coolant feed duct - has tool abutting seal exchangeable from outside in tool surrounding recess in clamping nut
JPH06147189A (ja) * 1992-11-11 1994-05-27 Hitachi Ltd 圧縮機の旋回失速防止装置

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014106522B4 (de) * 2013-05-24 2020-09-03 GM Global Technology Operations LLC (n. d. Gesetzen des Staates Delaware) Systeme und Verfahren zum Detektieren eines Kompressordruckstoßes

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US5915917A (en) 1999-06-29
EP0839285A2 (de) 1998-05-06
JP2997319B2 (ja) 2000-01-11
EP0839285B1 (de) 2001-07-18
AU1183997A (en) 1997-01-15
JPH10502992A (ja) 1998-03-17
WO1997000381A1 (en) 1997-01-03
DE69521816D1 (de) 2001-08-23

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