BE755567A - Structure d'aube fixe, pour moteur a turbines a gaz et arrangement de reglage de temperature associe - Google Patents

Structure d'aube fixe, pour moteur a turbines a gaz et arrangement de reglage de temperature associe

Info

Publication number
BE755567A
BE755567A BE755567DA BE755567A BE 755567 A BE755567 A BE 755567A BE 755567D A BE755567D A BE 755567DA BE 755567 A BE755567 A BE 755567A
Authority
BE
Belgium
Prior art keywords
gas turbine
turbine engine
temperature adjustment
adjustment arrangement
vane structure
Prior art date
Application number
Other languages
English (en)
Inventor
R J Smuland
N A Hope
J E Sidenstick
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.)
Publication date
Publication of BE755567A publication Critical patent/BE755567A/fr

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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • F01D5/188Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • F01D5/189Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
    • 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
    • F05D2240/80Platforms for stationary or moving blades
    • F05D2240/81Cooled platforms
    • 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
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/201Heat transfer, e.g. cooling by impingement of a fluid
BE755567D 1969-12-01 Structure d'aube fixe, pour moteur a turbines a gaz et arrangement de reglage de temperature associe BE755567A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US88125469A 1969-12-01 1969-12-01

Publications (1)

Publication Number Publication Date
BE755567A true BE755567A (fr) 1971-02-15

Family

ID=25378090

Family Applications (1)

Application Number Title Priority Date Filing Date
BE755567D BE755567A (fr) 1969-12-01 Structure d'aube fixe, pour moteur a turbines a gaz et arrangement de reglage de temperature associe

Country Status (8)

Country Link
US (1) US3628880A (fr)
JP (1) JPS4826086B1 (fr)
BE (1) BE755567A (fr)
CA (1) CA941745A (fr)
DE (1) DE2042947C3 (fr)
FR (1) FR2071665A5 (fr)
GB (1) GB1322801A (fr)
IL (1) IL35196A (fr)

Families Citing this family (229)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3706508A (en) * 1971-04-16 1972-12-19 Sean Lingwood Transpiration cooled turbine blade with metered coolant flow
GB1304678A (fr) * 1971-06-30 1973-01-24
GB1355558A (en) * 1971-07-02 1974-06-05 Rolls Royce Cooled vane or blade for a gas turbine engine
GB1361256A (en) * 1971-08-25 1974-07-24 Rolls Royce Gas turbine engine blades
US3726604A (en) * 1971-10-13 1973-04-10 Gen Motors Corp Cooled jet flap vane
BE795073A (fr) * 1972-03-02 1973-05-29 Gen Electric Procede pour la fabrication d'aubes creuses
US3891348A (en) * 1972-04-24 1975-06-24 Gen Electric Turbine blade with increased film cooling
FR2185753B1 (fr) * 1972-05-26 1976-06-11 Szydlowski Joseph
GB1400285A (en) * 1972-08-02 1975-07-16 Rolls Royce Hollow cooled vane or blade for a gas turbine engine
US3800864A (en) * 1972-09-05 1974-04-02 Gen Electric Pin-fin cooling system
US3819295A (en) * 1972-09-21 1974-06-25 Gen Electric Cooling slot for airfoil blade
GB1560683A (en) * 1972-11-28 1980-02-06 Rolls Royce Turbine blade
US3921271A (en) * 1973-01-02 1975-11-25 Gen Electric Air-cooled turbine blade and method of making same
US3864058A (en) * 1973-02-05 1975-02-04 Garrett Corp Cooled aerodynamic device
US4020538A (en) * 1973-04-27 1977-05-03 General Electric Company Turbomachinery blade tip cap configuration
US3902820A (en) * 1973-07-02 1975-09-02 Westinghouse Electric Corp Fluid cooled turbine rotor blade
US3849022A (en) * 1973-07-12 1974-11-19 Gen Motors Corp Turbine blade coolant distributor
JPS5048309A (fr) * 1973-08-31 1975-04-30
GB1587401A (en) * 1973-11-15 1981-04-01 Rolls Royce Hollow cooled vane for a gas turbine engine
GB1483532A (en) * 1974-09-13 1977-08-24 Rolls Royce Stator structure for a gas turbine engine
GB1519590A (en) * 1974-11-11 1978-08-02 Rolls Royce Gas turbine engine
US4040767A (en) * 1975-06-02 1977-08-09 United Technologies Corporation Coolable nozzle guide vane
US4025226A (en) * 1975-10-03 1977-05-24 United Technologies Corporation Air cooled turbine vane
US4012167A (en) * 1975-10-14 1977-03-15 United Technologies Corporation Turbomachinery vane or blade with cooled platforms
US4017213A (en) * 1975-10-14 1977-04-12 United Technologies Corporation Turbomachinery vane or blade with cooled platforms
DE2643049A1 (de) * 1975-10-14 1977-04-21 United Technologies Corp Schaufel mit gekuehlter plattform fuer eine stroemungsmaschine
US4063851A (en) * 1975-12-22 1977-12-20 United Technologies Corporation Coolable turbine airfoil
SE395934B (sv) * 1976-01-19 1977-08-29 Stal Laval Turbin Ab Kyld-ihalig ledskovel for gasturbin
US4353679A (en) * 1976-07-29 1982-10-12 General Electric Company Fluid-cooled element
US4118146A (en) * 1976-08-11 1978-10-03 United Technologies Corporation Coolable wall
US4090810A (en) * 1977-03-23 1978-05-23 General Electric Company Liquid-cooled turbine bucket with enhanced heat transfer performance
US4292008A (en) * 1977-09-09 1981-09-29 International Harvester Company Gas turbine cooling systems
US4177004A (en) * 1977-10-31 1979-12-04 General Electric Company Combined turbine shroud and vane support structure
US4222703A (en) * 1977-12-13 1980-09-16 Pratt & Whitney Aircraft Of Canada Limited Turbine engine with induced pre-swirl at compressor inlet
US4236870A (en) * 1977-12-27 1980-12-02 United Technologies Corporation Turbine blade
US4183207A (en) * 1978-03-07 1980-01-15 Avco Corporation Oil-conducting strut for turbine engines
US4187054A (en) * 1978-04-20 1980-02-05 General Electric Company Turbine band cooling system
US4303371A (en) * 1978-06-05 1981-12-01 General Electric Company Shroud support with impingement baffle
US4314442A (en) * 1978-10-26 1982-02-09 Rice Ivan G Steam-cooled blading with steam thermal barrier for reheat gas turbine combined with steam turbine
US4384452A (en) * 1978-10-26 1983-05-24 Rice Ivan G Steam-cooled blading with steam thermal barrier for reheat gas turbine combined with steam turbine
FR2473621A1 (fr) * 1980-01-10 1981-07-17 Snecma Aube de distributeur de turbine
US4305697A (en) * 1980-03-19 1981-12-15 General Electric Company Method and replacement member for repairing a gas turbine engine vane assembly
US4693667A (en) * 1980-04-29 1987-09-15 Teledyne Industries, Inc. Turbine inlet nozzle with cooling means
WO1982001033A1 (fr) * 1980-09-24 1982-04-01 K Karstensen Systeme de refroidissement de turbine
US4312624A (en) * 1980-11-10 1982-01-26 United Technologies Corporation Air cooled hollow vane construction
GB2163218B (en) * 1981-07-07 1986-07-16 Rolls Royce Cooled vane or blade for a gas turbine engine
US4775296A (en) * 1981-12-28 1988-10-04 United Technologies Corporation Coolable airfoil for a rotary machine
US4542867A (en) * 1983-01-31 1985-09-24 United Technologies Corporation Internally cooled hollow airfoil
US4526512A (en) * 1983-03-28 1985-07-02 General Electric Co. Cooling flow control device for turbine blades
US4514144A (en) * 1983-06-20 1985-04-30 General Electric Company Angled turbulence promoter
US4515523A (en) * 1983-10-28 1985-05-07 Westinghouse Electric Corp. Cooling arrangement for airfoil stator vane trailing edge
US4712979A (en) * 1985-11-13 1987-12-15 The United States Of America As Represented By The Secretary Of The Air Force Self-retained platform cooling plate for turbine vane
US4721433A (en) * 1985-12-19 1988-01-26 United Technologies Corporation Coolable stator structure for a gas turbine engine
GB2189553B (en) * 1986-04-25 1990-05-23 Rolls Royce Cooled vane
US4798515A (en) * 1986-05-19 1989-01-17 The United States Of America As Represented By The Secretary Of The Air Force Variable nozzle area turbine vane cooling
US4721434A (en) * 1986-12-03 1988-01-26 United Technologies Corporation Damping means for a stator
WO1991009776A1 (fr) * 1989-12-29 1991-07-11 Venturi Applications, Inc. Profil d'aile ameliore par un venturi
FR2659689B1 (fr) * 1990-03-14 1992-06-05 Snecma Circuit de refroidissement interne d'une aube directrice de turbine.
US5197852A (en) * 1990-05-31 1993-03-30 General Electric Company Nozzle band overhang cooling
US5098257A (en) * 1990-09-10 1992-03-24 Westinghouse Electric Corp. Apparatus and method for minimizing differential thermal expansion of gas turbine vane structures
US5169287A (en) * 1991-05-20 1992-12-08 General Electric Company Shroud cooling assembly for gas turbine engine
US5165847A (en) * 1991-05-20 1992-11-24 General Electric Company Tapered enlargement metering inlet channel for a shroud cooling assembly of gas turbine engines
FR2692318B1 (fr) * 1992-06-11 1994-08-19 Snecma Aubage fixe de distribution des gaz chauds d'une turbo-machine.
GB9224241D0 (en) * 1992-11-19 1993-01-06 Bmw Rolls Royce Gmbh A turbine blade arrangement
US5413458A (en) * 1994-03-29 1995-05-09 United Technologies Corporation Turbine vane with a platform cavity having a double feed for cooling fluid
US5591002A (en) * 1994-08-23 1997-01-07 General Electric Co. Closed or open air cooling circuits for nozzle segments with wheelspace purge
US5634766A (en) * 1994-08-23 1997-06-03 General Electric Co. Turbine stator vane segments having combined air and steam cooling circuits
JP3824324B2 (ja) * 1994-10-31 2006-09-20 ウエスチングハウス・エレクトリック・コーポレイション 冷却式プラットホームを備えたガスタービン翼
US5468125A (en) * 1994-12-20 1995-11-21 Alliedsignal Inc. Turbine blade with improved heat transfer surface
FR2743391B1 (fr) 1996-01-04 1998-02-06 Snecma Aube refrigeree de distributeur de turbine
US5711650A (en) * 1996-10-04 1998-01-27 Pratt & Whitney Canada, Inc. Gas turbine airfoil cooling
DE19641725A1 (de) * 1996-10-10 1998-04-16 Asea Brown Boveri Gasturbine mit einer sequentiellen Verbrennung
US5738493A (en) * 1997-01-03 1998-04-14 General Electric Company Turbulator configuration for cooling passages of an airfoil in a gas turbine engine
US5752801A (en) * 1997-02-20 1998-05-19 Westinghouse Electric Corporation Apparatus for cooling a gas turbine airfoil and method of making same
JP3316415B2 (ja) * 1997-05-01 2002-08-19 三菱重工業株式会社 ガスタービン冷却静翼
US6055805A (en) * 1997-08-29 2000-05-02 United Technologies Corporation Active rotor stage vibration control
FR2771446B1 (fr) * 1997-11-27 1999-12-31 Snecma Aube de distributeur de turbine refroidie
US6092991A (en) * 1998-03-05 2000-07-25 Mitsubishi Heavy Industries, Ltd. Gas turbine blade
EP0945595A3 (fr) * 1998-03-26 2001-10-10 Mitsubishi Heavy Industries, Ltd. Aube refroidie pour turbine à gaz
US6019572A (en) * 1998-08-06 2000-02-01 Siemens Westinghouse Power Corporation Gas turbine row #1 steam cooled vane
GB2345942B (en) * 1998-12-24 2002-08-07 Rolls Royce Plc Gas turbine engine internal air system
US6254333B1 (en) 1999-08-02 2001-07-03 United Technologies Corporation Method for forming a cooling passage and for cooling a turbine section of a rotary machine
US6241467B1 (en) 1999-08-02 2001-06-05 United Technologies Corporation Stator vane for a rotary machine
US6227798B1 (en) * 1999-11-30 2001-05-08 General Electric Company Turbine nozzle segment band cooling
DE19962244A1 (de) 1999-12-22 2001-06-28 Rolls Royce Deutschland Kühlluft-Führungssystem im Hochdruck-Turbinenabschnitt eines Gasturbinen Triebwerkes
EP1136651A1 (fr) * 2000-03-22 2001-09-26 Siemens Aktiengesellschaft Système de refroidissement pour une aube de turbine à gaz
US6543993B2 (en) * 2000-12-28 2003-04-08 General Electric Company Apparatus and methods for localized cooling of gas turbine nozzle walls
US6431820B1 (en) * 2001-02-28 2002-08-13 General Electric Company Methods and apparatus for cooling gas turbine engine blade tips
US6508620B2 (en) 2001-05-17 2003-01-21 Pratt & Whitney Canada Corp. Inner platform impingement cooling by supply air from outside
DE50210878D1 (de) 2001-07-05 2007-10-25 Alstom Technology Ltd Verfahren zur Montage eines Prallblechs
DE50208671D1 (de) 2001-07-13 2006-12-21 Alstom Technology Ltd Gasturbinenteil mit Kühlluftbohrung
US6589010B2 (en) * 2001-08-27 2003-07-08 General Electric Company Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same
DE10217484B4 (de) 2001-11-02 2018-05-17 Ansaldo Energia Ip Uk Limited Leitschaufel einer thermischen Turbomaschine
FR2833035B1 (fr) * 2001-12-05 2004-08-06 Snecma Moteurs Plate-forme d'aube de distributeur pour moteur a turbine a gaz
GB0200992D0 (en) * 2002-01-17 2002-03-06 Rolls Royce Plc Gas turbine cooling system
US6892931B2 (en) * 2002-12-27 2005-05-17 General Electric Company Methods for replacing portions of turbine shroud supports
US6964557B2 (en) * 2003-02-03 2005-11-15 General Electric Company Methods and apparatus for coupling a component to a turbine engine blade
US6969233B2 (en) * 2003-02-27 2005-11-29 General Electric Company Gas turbine engine turbine nozzle segment with a single hollow vane having a bifurcated cavity
US7008185B2 (en) * 2003-02-27 2006-03-07 General Electric Company Gas turbine engine turbine nozzle bifurcated impingement baffle
US6932568B2 (en) * 2003-02-27 2005-08-23 General Electric Company Turbine nozzle segment cantilevered mount
US6887033B1 (en) * 2003-11-10 2005-05-03 General Electric Company Cooling system for nozzle segment platform edges
US7029228B2 (en) * 2003-12-04 2006-04-18 General Electric Company Method and apparatus for convective cooling of side-walls of turbine nozzle segments
US7175386B2 (en) * 2003-12-17 2007-02-13 United Technologies Corporation Airfoil with shaped trailing edge pedestals
US7114339B2 (en) * 2004-03-30 2006-10-03 United Technologies Corporation Cavity on-board injection for leakage flows
FR2872541B1 (fr) * 2004-06-30 2006-11-10 Snecma Moteurs Sa Aube fixe de turbine a refroidissement ameliore
EP1655451B1 (fr) 2004-11-09 2010-06-30 Rolls-Royce Plc Arrangement de refroidissement
GB0424668D0 (en) * 2004-11-09 2004-12-08 Rolls Royce Plc A cooling arrangement
US7217095B2 (en) * 2004-11-09 2007-05-15 United Technologies Corporation Heat transferring cooling features for an airfoil
US7258528B2 (en) * 2004-12-02 2007-08-21 Pratt & Whitney Canada Corp. Internally cooled airfoil for a gas turbine engine and method
RU2425982C2 (ru) * 2005-04-14 2011-08-10 Альстом Текнолоджи Лтд Лопатка газовой турбины
JP4867203B2 (ja) * 2005-05-31 2012-02-01 株式会社日立製作所 ガスタービン
US7588412B2 (en) * 2005-07-28 2009-09-15 General Electric Company Cooled shroud assembly and method of cooling a shroud
US7762761B2 (en) * 2005-11-30 2010-07-27 General Electric Company Methods and apparatus for assembling turbine nozzles
US7322795B2 (en) * 2006-01-27 2008-01-29 United Technologies Corporation Firm cooling method and hole manufacture
FR2899281B1 (fr) 2006-03-30 2012-08-10 Snecma Dispositif de refroidissement d'un carter de turbine d'une turbomachine
US20070258814A1 (en) * 2006-05-02 2007-11-08 Siemens Power Generation, Inc. Turbine airfoil with integral chordal support ribs
US20100322767A1 (en) * 2009-06-18 2010-12-23 Nadvit Gregory M Turbine Blade Having Platform Cooling Holes
US7534088B1 (en) 2006-06-19 2009-05-19 United Technologies Corporation Fluid injection system
US7766606B2 (en) * 2006-08-17 2010-08-03 Siemens Energy, Inc. Turbine airfoil cooling system with platform cooling channels with diffusion slots
US7722315B2 (en) * 2006-11-30 2010-05-25 General Electric Company Method and system to facilitate preferentially distributed recuperated film cooling of turbine shroud assembly
US7766609B1 (en) 2007-05-24 2010-08-03 Florida Turbine Technologies, Inc. Turbine vane endwall with float wall heat shield
US7857588B2 (en) * 2007-07-06 2010-12-28 United Technologies Corporation Reinforced airfoils
US8128365B2 (en) 2007-07-09 2012-03-06 Siemens Energy, Inc. Turbine airfoil cooling system with rotor impingement cooling
US7921654B1 (en) * 2007-09-07 2011-04-12 Florida Turbine Technologies, Inc. Cooled turbine stator vane
JP2009162119A (ja) * 2008-01-08 2009-07-23 Ihi Corp タービン翼の冷却構造
ES2374148T3 (es) * 2008-03-19 2012-02-14 Alstom Technology Ltd Pala de guía para una turbina de gas.
WO2009115384A1 (fr) * 2008-03-19 2009-09-24 Alstom Technology Ltd Aube fixe avec un élément de fixation en forme de crochet pour une turbine à gaz
US8246297B2 (en) 2008-07-21 2012-08-21 Pratt & Whitney Canada Corp. Shroud segment cooling configuration
US8240987B2 (en) * 2008-08-15 2012-08-14 United Technologies Corp. Gas turbine engine systems involving baffle assemblies
US8591166B2 (en) * 2008-12-31 2013-11-26 Rolls-Royce North American Technologies, Inc. Axial compressor vane
US8322988B1 (en) 2009-01-09 2012-12-04 Florida Turbine Technologies, Inc. Air cooled turbine airfoil with sequential impingement cooling
US8096766B1 (en) 2009-01-09 2012-01-17 Florida Turbine Technologies, Inc. Air cooled turbine airfoil with sequential cooling
US8096767B1 (en) * 2009-02-04 2012-01-17 Florida Turbine Technologies, Inc. Turbine blade with serpentine cooling circuit formed within the tip shroud
US8109724B2 (en) 2009-03-26 2012-02-07 United Technologies Corporation Recessed metering standoffs for airfoil baffle
US8348613B2 (en) * 2009-03-30 2013-01-08 United Technologies Corporation Airflow influencing airfoil feature array
US8292573B2 (en) * 2009-04-21 2012-10-23 General Electric Company Flange cooled turbine nozzle
US20100284800A1 (en) * 2009-05-11 2010-11-11 General Electric Company Turbine nozzle with sidewall cooling plenum
EP2282014A1 (fr) * 2009-06-23 2011-02-09 Siemens Aktiengesellschaft Section de canal d'écoulement annulaire pour une turbomachine
JP2011043118A (ja) * 2009-08-21 2011-03-03 Ihi Corp タービン用冷却構造及びタービン
US8794911B2 (en) * 2010-03-30 2014-08-05 United Technologies Corporation Anti-rotation slot for turbine vane
US8840369B2 (en) * 2010-09-30 2014-09-23 General Electric Company Apparatus and methods for cooling platform regions of turbine rotor blades
US8777568B2 (en) * 2010-09-30 2014-07-15 General Electric Company Apparatus and methods for cooling platform regions of turbine rotor blades
RU2547351C2 (ru) * 2010-11-29 2015-04-10 Альстом Текнолоджи Лтд Осевая газовая турбина
RU2543101C2 (ru) * 2010-11-29 2015-02-27 Альстом Текнолоджи Лтд Осевая газовая турбина
US8714911B2 (en) * 2011-01-06 2014-05-06 General Electric Company Impingement plate for turbomachine components and components equipped therewith
JP5449225B2 (ja) * 2011-02-08 2014-03-19 株式会社日立製作所 ガスタービン
GB201105105D0 (en) * 2011-03-28 2011-05-11 Rolls Royce Plc Gas turbine engine component
US8651799B2 (en) * 2011-06-02 2014-02-18 General Electric Company Turbine nozzle slashface cooling holes
EP2540969A1 (fr) * 2011-06-27 2013-01-02 Siemens Aktiengesellschaft Refroidissement par projection d'aubes ou pales de turbine
JP2011241839A (ja) * 2011-09-06 2011-12-01 Hitachi Ltd ガスタービンの静翼、及びガスタービン
US8376705B1 (en) * 2011-09-09 2013-02-19 Siemens Energy, Inc. Turbine endwall with grooved recess cavity
EP2584145A1 (fr) 2011-10-20 2013-04-24 Siemens Aktiengesellschaft Pale ou aube de guidage de turbine refroidie pour turbomachine
FR2981980B1 (fr) * 2011-10-26 2016-01-22 Snecma Procede de montage d'un aubage fixe d'une turbomachine, carter et turbomachine comportant au moins un aubage fixe monte sur ce carter
US9057271B2 (en) * 2011-11-04 2015-06-16 Siemens Energy, Inc. Splice insert repair for superalloy turbine blades
EP2626519A1 (fr) * 2012-02-09 2013-08-14 Siemens Aktiengesellschaft Ensemble pour turbine, tube de refroidissement par impact et moteur à turbine à vapeur.
US9033670B2 (en) 2012-04-11 2015-05-19 Honeywell International Inc. Axially-split radial turbines and methods for the manufacture thereof
US9115586B2 (en) 2012-04-19 2015-08-25 Honeywell International Inc. Axially-split radial turbine
CA2875816C (fr) 2012-06-15 2021-06-22 General Electric Company Aube de turbine avec circuit de refroidissement de plate-forme moulee
US9500099B2 (en) 2012-07-02 2016-11-22 United Techologies Corporation Cover plate for a component of a gas turbine engine
US8863531B2 (en) * 2012-07-02 2014-10-21 United Technologies Corporation Cooling apparatus for a mid-turbine frame
US9228450B2 (en) * 2012-07-03 2016-01-05 Solar Turbines Incorporated Nozzle particle deflector for a gas turbine engine
JP2015527530A (ja) * 2012-08-20 2015-09-17 アルストム テクノロジー リミテッドALSTOM Technology Ltd 回転機械用の内部冷却される翼
US9759072B2 (en) * 2012-08-30 2017-09-12 United Technologies Corporation Gas turbine engine airfoil cooling circuit arrangement
EP2713009B1 (fr) * 2012-09-26 2015-03-11 Alstom Technology Ltd Procédé et système de refroidissement pour refroidir des aubes d'au moins une rangée d'aubes dans une turbomachine rotative
US9863319B2 (en) * 2012-09-28 2018-01-09 United Technologies Corporation Split-zone flow metering T-tube
CN102996187A (zh) * 2012-12-06 2013-03-27 哈尔滨汽轮机厂有限责任公司 燃机涡轮首级导叶下端壁冷却系统
CN102979584A (zh) * 2012-12-06 2013-03-20 哈尔滨汽轮机厂有限责任公司 燃机涡轮首级导叶上端壁冷却系统
EP2754857A1 (fr) * 2013-01-10 2014-07-16 Alstom Technology Ltd Ensemble de refroidissement, écran thermique statorique, aube mobile et aube statorique associés pour un moteur à turbine à gaz
US9796055B2 (en) * 2013-02-17 2017-10-24 United Technologies Corporation Turbine case retention hook with insert
US9719362B2 (en) * 2013-04-24 2017-08-01 Honeywell International Inc. Turbine nozzles and methods of manufacturing the same
US9476305B2 (en) 2013-05-13 2016-10-25 Honeywell International Inc. Impingement-cooled turbine rotor
US10100737B2 (en) * 2013-05-16 2018-10-16 Siemens Energy, Inc. Impingement cooling arrangement having a snap-in plate
GB2514832A (en) * 2013-06-07 2014-12-10 Rolls Royce Deutschland & Co Kg Cooling system
CN103266922B (zh) * 2013-06-15 2014-11-12 厦门大学 一种带有级间燃烧室的涡轮静子叶片
EP3049640B1 (fr) * 2013-09-18 2022-11-09 Raytheon Technologies Corporation Protection thermique de joint d'étanchéité à l'air externe d'aube (boas)
US10280793B2 (en) 2013-09-18 2019-05-07 United Technologies Corporation Insert and standoff design for a gas turbine engine vane
US10001018B2 (en) * 2013-10-25 2018-06-19 General Electric Company Hot gas path component with impingement and pedestal cooling
US8939717B1 (en) * 2013-10-25 2015-01-27 Siemens Aktiengesellschaft Vane outer support ring with no forward hook in a compressor section of a gas turbine engine
US9206700B2 (en) * 2013-10-25 2015-12-08 Siemens Aktiengesellschaft Outer vane support ring including a strong back plate in a compressor section of a gas turbine engine
US9133716B2 (en) * 2013-12-02 2015-09-15 Siemens Energy, Inc. Turbine endwall with micro-circuit cooling
EP3092372B1 (fr) 2014-01-08 2019-06-19 United Technologies Corporation Joint de serrage pour cadre de turbine intermédiaire de turboréacteur
US10669870B2 (en) * 2014-01-28 2020-06-02 Raytheon Technologies Corporation Vane for jet engine mid-turbine frame
EP2921650B1 (fr) * 2014-03-20 2017-10-04 Ansaldo Energia Switzerland AG Aube de turbine avec congé de raccordement refroidi
EP2927430B1 (fr) * 2014-04-04 2019-08-07 United Technologies Corporation Aube statorique ayant une plate-forme refroidie pour un moteur à turbine à gaz
CN107075955A (zh) * 2014-09-04 2017-08-18 西门子公司 具有在燃气涡轮机翼型件的后部冷却腔中形成近壁冷却通道的插入件的包括散热肋的内部冷却系统
GB2530763A (en) * 2014-10-01 2016-04-06 Rolls Royce Plc A heat shield
US10711702B2 (en) * 2015-08-18 2020-07-14 General Electric Company Mixed flow turbocore
JP6587251B2 (ja) * 2015-11-27 2019-10-09 三菱日立パワーシステムズ株式会社 流路形成板、これを備える流路形成組部材及び静翼、ガスタービン、流路形成板の製造方法、並びに流路形成板の改造方法
US10221710B2 (en) 2016-02-09 2019-03-05 General Electric Company Turbine nozzle having non-axisymmetric endwall contour (EWC) and profile
US10156149B2 (en) * 2016-02-09 2018-12-18 General Electric Company Turbine nozzle having fillet, pinbank, throat region and profile
US10001014B2 (en) 2016-02-09 2018-06-19 General Electric Company Turbine bucket profile
US10196908B2 (en) 2016-02-09 2019-02-05 General Electric Company Turbine bucket having part-span connector and profile
US10125623B2 (en) 2016-02-09 2018-11-13 General Electric Company Turbine nozzle profile
US10161255B2 (en) 2016-02-09 2018-12-25 General Electric Company Turbine nozzle having non-axisymmetric endwall contour (EWC)
US10190421B2 (en) 2016-02-09 2019-01-29 General Electric Company Turbine bucket having tip shroud fillet, tip shroud cross-drilled apertures and profile
US10190417B2 (en) 2016-02-09 2019-01-29 General Electric Company Turbine bucket having non-axisymmetric endwall contour and profile
US10344619B2 (en) * 2016-07-08 2019-07-09 United Technologies Corporation Cooling system for a gaspath component of a gas powered turbine
CN105971674B (zh) * 2016-07-29 2018-04-03 上海电气燃气轮机有限公司 燃气轮机轮缘密封结构及方法
US10309242B2 (en) * 2016-08-10 2019-06-04 General Electric Company Ceramic matrix composite component cooling
DE102016222608A1 (de) * 2016-11-17 2018-05-17 MTU Aero Engines AG Dichtungsanordnung für eine Leitschaufelanordnung einer Gasturbine
EP3450685B1 (fr) * 2017-08-02 2020-04-29 United Technologies Corporation Composant de moteur à turbine à gaz
US10612466B2 (en) * 2017-09-11 2020-04-07 United Technologies Corporation Gas turbine engine active clearance control system using inlet particle separator
US20190085706A1 (en) * 2017-09-18 2019-03-21 General Electric Company Turbine engine airfoil assembly
US10822973B2 (en) * 2017-11-28 2020-11-03 General Electric Company Shroud for a gas turbine engine
US11131212B2 (en) 2017-12-06 2021-09-28 Raytheon Technologies Corporation Gas turbine engine cooling component
FR3074521B1 (fr) * 2017-12-06 2019-11-22 Safran Aircraft Engines Secteur de distributeur de turbine pour une turbomachine d'aeronef
US10648351B2 (en) * 2017-12-06 2020-05-12 United Technologies Corporation Gas turbine engine cooling component
US10655496B2 (en) 2017-12-22 2020-05-19 United Technologies Corporation Platform flow turning elements for gas turbine engine components
US10746026B2 (en) * 2018-01-05 2020-08-18 Raytheon Technologies Corporation Gas turbine engine airfoil with cooling path
US11261739B2 (en) * 2018-01-05 2022-03-01 Raytheon Technologies Corporation Airfoil with rib communication
US10697307B2 (en) * 2018-01-19 2020-06-30 Raytheon Technologies Corporation Hybrid cooling schemes for airfoils of gas turbine engines
US10808572B2 (en) * 2018-04-02 2020-10-20 General Electric Company Cooling structure for a turbomachinery component
KR102048863B1 (ko) 2018-04-17 2019-11-26 두산중공업 주식회사 인서트 지지부를 구비한 터빈 베인
US10787912B2 (en) * 2018-04-25 2020-09-29 Raytheon Technologies Corporation Spiral cavities for gas turbine engine components
US10697310B2 (en) * 2018-05-17 2020-06-30 Raytheon Technologies Corporation Multiple source impingement baffles for gas turbine engine components
RU2684298C1 (ru) * 2018-07-05 2019-04-05 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Способ охлаждения ротора турбины высокого давления (ТВД) газотурбинного двигателя (ГТД), ротор ТВД и лопатка ротора ТВД, охлаждаемые этим способом, узел аппарата закрутки воздуха ротора ТВД
RU2691867C1 (ru) * 2018-07-05 2019-06-18 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Способ охлаждения лопатки ротора турбины низкого давления (ТНД) газотурбинного двигателя и лопатка ротора ТНД, охлаждаемая этим способом
RU2691868C1 (ru) * 2018-07-05 2019-06-18 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Ротор турбины высокого давления газотурбинного двигателя (варианты)
US10822962B2 (en) * 2018-09-27 2020-11-03 Raytheon Technologies Corporation Vane platform leading edge recessed pocket with cover
US10822963B2 (en) * 2018-12-05 2020-11-03 Raytheon Technologies Corporation Axial flow cooling scheme with castable structural rib for a gas turbine engine
US20200182068A1 (en) * 2018-12-05 2020-06-11 United Technologies Corporation Axial flow cooling scheme with structural rib for a gas turbine engine
RU2716097C1 (ru) * 2019-07-30 2020-03-05 Акционерное общество "ОДК-Климов" Рабочая лопатка турбины газотурбинного двигателя и газотурбинный двигатель
WO2021193628A1 (fr) * 2020-03-25 2021-09-30 三菱パワー株式会社 Aube de turbine et procédé de fabrication d'aube de turbine
US11248479B2 (en) 2020-06-11 2022-02-15 General Electric Company Cast turbine nozzle having heat transfer protrusions on inner surface of leading edge
US11885230B2 (en) * 2021-03-16 2024-01-30 Doosan Heavy Industries & Construction Co. Ltd. Airfoil with internal crossover passages and pin array
FR3129429A1 (fr) * 2021-11-24 2023-05-26 Safran Aircraft Engines Secteur de distributeur de turbine pour une turbomachine d’aéronef
WO2023121680A1 (fr) * 2021-12-20 2023-06-29 General Electric Company Filtre à particules à tamis métallique pour profil aérodynamique de turbomachine
US11536143B1 (en) 2021-12-22 2022-12-27 Rolls-Royce North American Technologies Inc. Endwall cooling scheme
US11635000B1 (en) * 2021-12-23 2023-04-25 Rolls-Royce Corporation Endwall directional cooling

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE546821A (fr) * 1955-04-06
US3527543A (en) * 1965-08-26 1970-09-08 Gen Electric Cooling of structural members particularly for gas turbine engines
FR1503348A (fr) * 1965-12-11 1967-11-24 Daimler Benz Ag Aube pour turbines à gaz, en particulier pour réacteurs d'avions

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FR2071665A5 (fr) 1971-09-17
DE2042947B2 (de) 1973-12-20
GB1322801A (en) 1973-07-11
IL35196A (en) 1974-11-29
IL35196A0 (en) 1970-10-30
JPS4826086B1 (fr) 1973-08-06
CA941745A (en) 1974-02-12
US3628880A (en) 1971-12-21
DE2042947A1 (de) 1971-06-09
DE2042947C3 (de) 1974-07-18

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