IN2014CN04620A - - Google Patents

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Publication number
IN2014CN04620A
IN2014CN04620A IN4620CHN2014A IN2014CN04620A IN 2014CN04620 A IN2014CN04620 A IN 2014CN04620A IN 4620CHN2014 A IN4620CHN2014 A IN 4620CHN2014A IN 2014CN04620 A IN2014CN04620 A IN 2014CN04620A
Authority
IN
India
Prior art keywords
doublet supports
doublet
supports
frame member
cradles
Prior art date
Application number
Other languages
English (en)
Inventor
William Howard Hasting
Courtney James Tudor
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IN2014CN04620A publication Critical patent/IN2014CN04620A/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246Fastening of diaphragms or stator-rings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • 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
    • F05D2240/00Components
    • F05D2240/10Stators
    • F05D2240/12Fluid guiding means, e.g. vanes
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603Composites; e.g. fibre-reinforced
    • F05D2300/6033Ceramic matrix composites [CMC]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
IN4620CHN2014 2011-12-09 2012-12-07 IN2014CN04620A (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201161568976P 2011-12-09 2011-12-09
US13/652,962 US9303531B2 (en) 2011-12-09 2012-10-16 Quick engine change assembly for outlet guide vanes
PCT/US2012/068424 WO2013086305A1 (en) 2011-12-09 2012-12-07 Quick engine change assembly for outlet guide vanes

Publications (1)

Publication Number Publication Date
IN2014CN04620A true IN2014CN04620A (zh) 2015-09-18

Family

ID=47459147

Family Applications (1)

Application Number Title Priority Date Filing Date
IN4620CHN2014 IN2014CN04620A (zh) 2011-12-09 2012-12-07

Country Status (8)

Country Link
US (1) US9303531B2 (zh)
EP (1) EP2800877B1 (zh)
JP (1) JP5926814B2 (zh)
CN (1) CN104093938B (zh)
BR (1) BR112014013740A2 (zh)
CA (1) CA2858562C (zh)
IN (1) IN2014CN04620A (zh)
WO (1) WO2013086305A1 (zh)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9303531B2 (en) * 2011-12-09 2016-04-05 General Electric Company Quick engine change assembly for outlet guide vanes
US9303520B2 (en) * 2011-12-09 2016-04-05 General Electric Company Double fan outlet guide vane with structural platforms
US20130149130A1 (en) * 2011-12-09 2013-06-13 General Electric Company Fan Hub Frame for Double Outlet Guide Vane
US10655482B2 (en) * 2015-02-05 2020-05-19 Rolls-Royce Corporation Vane assemblies for gas turbine engines
FR3038653B1 (fr) * 2015-07-08 2017-08-04 Snecma Assemblage d'une plateforme rapportee d'aube de soufflante sur un disque de soufflante
US10760589B2 (en) * 2015-12-29 2020-09-01 General Electric Company Turbofan engine assembly and methods of assembling the same
US10443625B2 (en) * 2016-09-21 2019-10-15 General Electric Company Airfoil singlets
US10415399B2 (en) 2017-08-30 2019-09-17 United Technologies Corporation Composite stator with integral platforms for gas turbine engines
FR3072607B1 (fr) * 2017-10-23 2019-12-20 Safran Aircraft Engines Turbomachine comprenant un ensemble de redressement
FR3076571B1 (fr) * 2018-01-10 2020-01-31 Safran Aircraft Engines Redresseur pour turbomachine et procede de demontage d'une aube de ce redresseur
US10724390B2 (en) 2018-03-16 2020-07-28 General Electric Company Collar support assembly for airfoils
US10830074B2 (en) * 2018-07-03 2020-11-10 Raytheon Technologies Corporation Potted stator vane with metal fillet
PL431184A1 (pl) * 2019-09-17 2021-03-22 General Electric Company Polska Spółka Z Ograniczoną Odpowiedzialnością Zespół silnika turbinowego
CA3119231A1 (en) * 2020-05-22 2021-11-22 Immeubles Mfp 1006 Inc. Blower impeller
CN113898614A (zh) * 2020-06-22 2022-01-07 中国航发商用航空发动机有限责任公司 航空发动机风扇出口导向叶片组件的分解工艺
US11828197B2 (en) 2021-12-03 2023-11-28 Rolls-Royce North American Technologies Inc. Outlet guide vane mounting assembly for turbine engines
US11549378B1 (en) * 2022-06-03 2023-01-10 Raytheon Technologies Corporation Airfoil assembly with composite rings and sealing shelf

Family Cites Families (53)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2337619A (en) 1941-04-14 1943-12-28 Hydraulic Brake Co Blade wheel
US2610823A (en) 1947-02-11 1952-09-16 Gen Electric Turbine bucket damping arrangement
US2686656A (en) 1950-04-04 1954-08-17 United Aircraft Corp Blade locking device
US2914300A (en) * 1955-12-22 1959-11-24 Gen Electric Nozzle vane support for turbines
US4256435A (en) 1978-08-02 1981-03-17 Eckel Oliver C Mounting support blocks for pivotal rotor of wind turbine
US4500255A (en) 1981-04-24 1985-02-19 United States Of America As Represented By The Secretary Of The Air Force Spacer structure
US4832568A (en) * 1982-02-26 1989-05-23 General Electric Company Turbomachine airfoil mounting assembly
US4827588A (en) 1988-01-04 1989-05-09 Williams International Corporation Method of making a turbine nozzle
FR2637321B1 (fr) 1988-10-05 1990-11-30 Snecma Rotor de turbomachine muni d'un dispositif de fixation des aubes
GB9007162D0 (en) 1990-03-30 1990-05-30 Courtaulds Plc Preform and composite structure
US5226789A (en) 1991-05-13 1993-07-13 General Electric Company Composite fan stator assembly
US5222360A (en) 1991-10-30 1993-06-29 General Electric Company Apparatus for removably attaching a core frame to a vane frame with a stable mid ring
FR2685383B1 (fr) * 1991-12-18 1994-02-11 Snecma Bras structural du carter d'une turbomachine.
FR2697285B1 (fr) 1992-10-28 1994-11-25 Snecma Système de verrouillage d'extrémités d'aubes.
US5272869A (en) * 1992-12-10 1993-12-28 General Electric Company Turbine frame
JP3631271B2 (ja) 1993-11-19 2005-03-23 ユナイテッド テクノロジーズ コーポレイション インナーシュラウド一体型ステータベーン構造
US5522705A (en) 1994-05-13 1996-06-04 United Technologies Corporation Friction damper for gas turbine engine blades
FR2738283B1 (fr) 1995-08-30 1997-09-26 Snecma Agencement de turbomachine comprenant une grille d'aubes et un carter intermediaire
US5765993A (en) * 1996-09-27 1998-06-16 Chromalloy Gas Turbine Corporation Replacement vane assembly for fan exit guide
DE10051223A1 (de) 2000-10-16 2002-04-25 Alstom Switzerland Ltd Verbindbare Statorelemente
US6821087B2 (en) 2002-01-21 2004-11-23 Honda Giken Kogyo Kabushiki Kaisha Flow-rectifying member and its unit and method for producing flow-rectifying member
FR2852884B1 (fr) 2003-03-26 2005-05-06 Hurel Hispano Procede de fabrication de pieces en composite a matrice polyimide
DE10334342A1 (de) 2003-07-29 2005-02-24 Mtu Aero Engines Gmbh Fasergelege und Verfahren zur Herstellung desselben
US7172389B2 (en) * 2004-11-16 2007-02-06 General Electric Company Method for making a repaired turbine engine stationary vane assembly and repaired assembly
US20090238863A1 (en) 2005-03-29 2009-09-24 Tokai University Educational System Liposome composition for induction of immunity
US7371046B2 (en) 2005-06-06 2008-05-13 General Electric Company Turbine airfoil with variable and compound fillet
US7300253B2 (en) 2005-07-25 2007-11-27 Siemens Aktiengesellschaft Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turbine blade or vane ring and the use of a gas turbine blade or vane ring
US7322796B2 (en) * 2005-08-31 2008-01-29 United Technologies Corporation Turbine vane construction
DE602005024425D1 (de) * 2005-12-22 2010-12-09 Techspace Aero Milmort Schaufelleitring einer Strömungsmaschine, Strömungsmaschine mit einem solchen Leitring und Leitschaufel
US7510372B2 (en) 2006-04-19 2009-03-31 United Technologies Corporation Wedge repair of mechanically retained vanes
FR2906296A1 (fr) * 2006-09-26 2008-03-28 Snecma Sa Dispositif de fixation d'une aube fixe dans un carter annulaire de turbomachine, turboreacteur incorporant le dispositif et procede de montage de l'aube.
EP1975373A1 (en) * 2007-03-06 2008-10-01 Siemens Aktiengesellschaft Guide vane duct element for a guide vane assembly of a gas turbine engine
FR2914008B1 (fr) 2007-03-21 2009-10-09 Snecma Sa Ensemble rotatif d'une soufflante de turbomachine
SE0700823L (sv) 2007-03-30 2008-10-01 Volvo Aero Corp Komponent för en gasturbinmotor, jetmotor försedd med en sådan komponent, samt en flygmaskin försedd med en sådan jetmotor
US7980817B2 (en) 2007-04-16 2011-07-19 United Technologies Corporation Gas turbine engine vane
US7931442B1 (en) 2007-05-31 2011-04-26 Florida Turbine Technologies, Inc. Rotor blade assembly with de-coupled composite platform
US20090014926A1 (en) 2007-07-09 2009-01-15 Siemens Power Generation, Inc. Method of constructing a hollow fiber reinforced structure
US8206095B2 (en) 2008-11-19 2012-06-26 Alstom Technology Ltd Compound variable elliptical airfoil fillet
US8371810B2 (en) 2009-03-26 2013-02-12 General Electric Company Duct member based nozzle for turbine
GB0905729D0 (en) * 2009-04-03 2009-05-20 Rolls Royce Plc Stator vane assembly
EP2494154B1 (en) 2009-10-27 2017-11-29 GKN Aerospace Sweden AB Gas turbine engine component
FR2956876B1 (fr) * 2010-02-26 2012-10-19 Snecma Module structural et aerodynamique d'un carter de turbomachine et structure de carter comportant une pluralite d'un tel module
FR2958323B1 (fr) 2010-03-30 2012-05-04 Snecma Etage redresseur de compresseur pour une turbomachine.
US8550776B2 (en) 2010-07-28 2013-10-08 General Electric Company Composite vane mounting
US8734101B2 (en) 2010-08-31 2014-05-27 General Electric Co. Composite vane mounting
GB201104994D0 (en) 2011-03-25 2011-05-11 Rolls Royce Plc a rotor having an annulus filler
US9915154B2 (en) * 2011-05-26 2018-03-13 United Technologies Corporation Ceramic matrix composite airfoil structures for a gas turbine engine
US20130052004A1 (en) 2011-08-25 2013-02-28 Nicholas D. Stilin Structural composite fan exit guide vane for a turbomachine
US20130149130A1 (en) * 2011-12-09 2013-06-13 General Electric Company Fan Hub Frame for Double Outlet Guide Vane
US9303520B2 (en) * 2011-12-09 2016-04-05 General Electric Company Double fan outlet guide vane with structural platforms
US9303531B2 (en) * 2011-12-09 2016-04-05 General Electric Company Quick engine change assembly for outlet guide vanes
US8733156B2 (en) 2012-07-16 2014-05-27 United Technologies Corporation PMC laminate embedded hypotube lattice
EP2696035A1 (de) 2012-08-09 2014-02-12 MTU Aero Engines GmbH Rückhaltevorrichtung für Laufschaufeln einer Strömungsmaschine und zugehöriges Montageverfahren

Also Published As

Publication number Publication date
WO2013086305A1 (en) 2013-06-13
CN104093938B (zh) 2015-11-25
EP2800877B1 (en) 2015-11-18
JP2015500431A (ja) 2015-01-05
CN104093938A (zh) 2014-10-08
BR112014013740A2 (pt) 2017-06-13
JP5926814B2 (ja) 2016-05-25
CA2858562A1 (en) 2013-06-13
CA2858562C (en) 2016-10-18
US9303531B2 (en) 2016-04-05
US20140140832A1 (en) 2014-05-22
EP2800877A1 (en) 2014-11-12

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