IN2014CN04623A - - Google Patents

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Publication number
IN2014CN04623A
IN2014CN04623A IN4623CHN2014A IN2014CN04623A IN 2014CN04623 A IN2014CN04623 A IN 2014CN04623A IN 4623CHN2014 A IN4623CHN2014 A IN 4623CHN2014A IN 2014CN04623 A IN2014CN04623 A IN 2014CN04623A
Authority
IN
India
Prior art keywords
cradles
circular hub
hub
guide vane
frame comprises
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 IN2014CN04623A publication Critical patent/IN2014CN04623A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F05D2300/6033—Ceramic matrix composites [CMC]
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Revetment (AREA)
IN4623CHN2014 2011-12-09 2012-12-07 IN2014CN04623A (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201161568976P 2011-12-09 2011-12-09
US13/652,949 US20130149130A1 (en) 2011-12-09 2012-10-16 Fan Hub Frame for Double Outlet Guide Vane
PCT/US2012/068400 WO2013086291A1 (fr) 2011-12-09 2012-12-07 Aubage directeur à double sortie d'armature de moyeu de ventilateur

Publications (1)

Publication Number Publication Date
IN2014CN04623A true IN2014CN04623A (fr) 2015-09-18

Family

ID=48572124

Family Applications (2)

Application Number Title Priority Date Filing Date
IN4623CHN2014 IN2014CN04623A (fr) 2011-12-09 2012-12-07
IN4621CHN2014 IN2014CN04621A (fr) 2011-12-09 2012-12-07

Family Applications After (1)

Application Number Title Priority Date Filing Date
IN4621CHN2014 IN2014CN04621A (fr) 2011-12-09 2012-12-07

Country Status (8)

Country Link
US (2) US20130149130A1 (fr)
EP (2) EP2798158B1 (fr)
JP (2) JP5845360B2 (fr)
CN (2) CN104105845B (fr)
BR (2) BR112014013748A2 (fr)
CA (2) CA2858556C (fr)
IN (2) IN2014CN04623A (fr)
WO (2) WO2013086315A1 (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130149130A1 (en) * 2011-12-09 2013-06-13 General Electric Company Fan Hub Frame for Double Outlet Guide Vane
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
GB201215906D0 (en) 2012-09-06 2012-10-24 Rolls Royce Plc Guide vane assembly
USD729809S1 (en) 2013-06-09 2015-05-19 Apple Inc. Component for an electronic device
US9347321B2 (en) 2014-08-01 2016-05-24 The Boeing Company Methods for optimized engine balancing based on flight data
USD777212S1 (en) * 2015-06-20 2017-01-24 General Electric Company Nozzle ring
US20170101878A1 (en) * 2015-10-08 2017-04-13 General Electric Company Low modulus insert for a component of a gas turbine engine
CN105673251A (zh) * 2016-01-13 2016-06-15 中国航空动力机械研究所 风扇增压级以及涡扇发动机
US10443447B2 (en) * 2016-03-14 2019-10-15 General Electric Company Doubler attachment system
US10443415B2 (en) 2016-03-30 2019-10-15 General Electric Company Flowpath assembly for a gas turbine engine
US10385868B2 (en) * 2016-07-05 2019-08-20 General Electric Company Strut assembly for an aircraft engine
BE1024523B1 (fr) * 2016-08-30 2018-03-29 Safran Aero Boosters S.A. Stator a aubes ajustables pour compresseur de turbomachine axiale
FR3056250B1 (fr) * 2016-09-19 2020-06-05 Safran Aircraft Engines Roue d'aube redresseuse en carter intermediaire
US10443625B2 (en) * 2016-09-21 2019-10-15 General Electric Company Airfoil singlets
US10343784B2 (en) 2017-06-07 2019-07-09 The Boeing Company Methods for optimized engine balancing based on flight data
US10239635B2 (en) 2017-06-08 2019-03-26 The Boeing Company Methods for balancing aircraft engines based on flight data
US10724390B2 (en) 2018-03-16 2020-07-28 General Electric Company Collar support assembly for airfoils
US11047251B2 (en) 2019-07-17 2021-06-29 Rolls-Royce Corporation Routing for electrical communication in gas turbine engines

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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
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
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
US5522705A (en) * 1994-05-13 1996-06-04 United Technologies Corporation Friction damper for gas turbine engine blades
US5765993A (en) * 1996-09-27 1998-06-16 Chromalloy Gas Turbine Corporation Replacement vane assembly for fan exit guide
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
EP1975373A1 (fr) * 2007-03-06 2008-10-01 Siemens Aktiengesellschaft Élément de conduit d'aube de guidage pour un ensemble d'aube de guidage d'un moteur de turbine à gaz
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
US7931442B1 (en) * 2007-05-31 2011-04-26 Florida Turbine Technologies, Inc. Rotor blade assembly with de-coupled composite platform
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
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
GB201104994D0 (en) * 2011-03-25 2011-05-11 Rolls Royce Plc a rotor having an annulus filler
US20130052004A1 (en) * 2011-08-25 2013-02-28 Nicholas D. Stilin Structural composite fan exit guide vane for a turbomachine
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
EP2696035A1 (fr) * 2012-08-09 2014-02-12 MTU Aero Engines GmbH Dispositif de retenue pour aubes mobiles d'une turbomachine et procédé de montage associé

Also Published As

Publication number Publication date
JP2015500432A (ja) 2015-01-05
IN2014CN04621A (fr) 2015-09-18
EP2798158B1 (fr) 2015-11-18
US20130149127A1 (en) 2013-06-13
EP2788587A1 (fr) 2014-10-15
EP2798158A1 (fr) 2014-11-05
US20130149130A1 (en) 2013-06-13
CN104081006B (zh) 2016-01-20
JP5926815B2 (ja) 2016-05-25
EP2788587B1 (fr) 2015-11-04
CA2858558C (fr) 2016-10-18
CN104105845A (zh) 2014-10-15
BR112014013748A2 (pt) 2017-06-13
WO2013086315A1 (fr) 2013-06-13
CN104081006A (zh) 2014-10-01
CA2858556C (fr) 2016-10-18
CN104105845B (zh) 2017-05-24
WO2013086291A1 (fr) 2013-06-13
CA2858558A1 (fr) 2013-06-13
JP5845360B2 (ja) 2016-01-20
CA2858556A1 (fr) 2013-06-13
BR112014013739A2 (pt) 2017-06-13
JP2015504998A (ja) 2015-02-16

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