NO20052477L - Anordning og fremgangsmate for reduksjon av varmebelastningen pa en skovel. - Google Patents

Anordning og fremgangsmate for reduksjon av varmebelastningen pa en skovel.

Info

Publication number
NO20052477L
NO20052477L NO20052477A NO20052477A NO20052477L NO 20052477 L NO20052477 L NO 20052477L NO 20052477 A NO20052477 A NO 20052477A NO 20052477 A NO20052477 A NO 20052477A NO 20052477 L NO20052477 L NO 20052477L
Authority
NO
Norway
Prior art keywords
vane
bucket
heat load
transition
reducing
Prior art date
Application number
NO20052477A
Other languages
English (en)
Other versions
NO20052477D0 (no
Inventor
Gary Zess
Joel Wagner
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
Publication of NO20052477D0 publication Critical patent/NO20052477D0/no
Publication of NO20052477L publication Critical patent/NO20052477L/no

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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/145—Means for influencing boundary layers or secondary circulations
    • 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
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
    • F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/541—Specially adapted for elastic fluid pumps
    • F04D29/542—Bladed diffusers
    • F04D29/544—Blade shapes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/14—Two-dimensional elliptical
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/18—Two-dimensional patterned
    • F05D2250/184—Two-dimensional patterned sinusoidal
    • 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
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S415/00—Rotary kinetic fluid motors or pumps
    • Y10S415/914—Device to control boundary layer

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Geometry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)

Abstract

En strømningsstyrende anordning for en gassturbinmotor er vist som omfatter: en skovl som har en forkant, en bakkant, en sugeside og en trykkside; en vegg som støter mot skovlen; og en overgang mellom skovlen og veggen. Overgangen har et forstørret område ved forkanten langs suge- og trykksidene og mot bakkanten. I tillegg til å fjerne hesteskovorteks reduserer anordningen også varmelasten på skovlen ved å rette kaldere gass fra den proksimale enden av skovlen til den varmere gassen ved midtområdet av skovlen.
NO20052477A 2002-10-23 2005-05-23 Anordning og fremgangsmate for reduksjon av varmebelastningen pa en skovel. NO20052477L (no)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/065,484 US6969232B2 (en) 2002-10-23 2002-10-23 Flow directing device
PCT/GB2003/004545 WO2004038180A1 (en) 2002-10-23 2003-10-23 Apparatus and method for reducing the heat load of an airfoil

Publications (2)

Publication Number Publication Date
NO20052477D0 NO20052477D0 (no) 2005-05-23
NO20052477L true NO20052477L (no) 2005-07-19

Family

ID=32106048

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20052477A NO20052477L (no) 2002-10-23 2005-05-23 Anordning og fremgangsmate for reduksjon av varmebelastningen pa en skovel.

Country Status (10)

Country Link
US (1) US6969232B2 (no)
EP (1) EP1556584B1 (no)
JP (1) JP2004278517A (no)
KR (1) KR20040036632A (no)
AU (1) AU2003274350A1 (no)
CA (1) CA2446035A1 (no)
NO (1) NO20052477L (no)
PL (1) PL376051A1 (no)
TW (1) TW200417682A (no)
WO (1) WO2004038180A1 (no)

Families Citing this family (101)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7217096B2 (en) * 2004-12-13 2007-05-15 General Electric Company Fillet energized turbine stage
US7134842B2 (en) * 2004-12-24 2006-11-14 General Electric Company Scalloped surface turbine stage
US7249933B2 (en) 2005-01-10 2007-07-31 General Electric Company Funnel fillet turbine stage
US7220100B2 (en) * 2005-04-14 2007-05-22 General Electric Company Crescentic ramp turbine stage
US7371046B2 (en) * 2005-06-06 2008-05-13 General Electric Company Turbine airfoil with variable and compound fillet
US7976274B2 (en) * 2005-12-08 2011-07-12 General Electric Company Methods and apparatus for assembling turbine engines
US7874794B2 (en) * 2006-03-21 2011-01-25 General Electric Company Blade row for a rotary machine and method of fabricating same
US8366399B2 (en) * 2006-05-02 2013-02-05 United Technologies Corporation Blade or vane with a laterally enlarged base
US8511978B2 (en) * 2006-05-02 2013-08-20 United Technologies Corporation Airfoil array with an endwall depression and components of the array
US7887297B2 (en) * 2006-05-02 2011-02-15 United Technologies Corporation Airfoil array with an endwall protrusion and components of the array
US7937945B2 (en) 2006-10-27 2011-05-10 Kinde Sr Ronald August Combining a series of more efficient engines into a unit, or modular units
US7758306B2 (en) * 2006-12-22 2010-07-20 General Electric Company Turbine assembly for a gas turbine engine and method of manufacturing the same
KR100847523B1 (ko) 2006-12-29 2008-07-22 엘지전자 주식회사 터보팬
US7871242B2 (en) * 2007-05-31 2011-01-18 United Technologies Corporation Single actuator controlled rotational flow balance system
JP4929193B2 (ja) * 2008-01-21 2012-05-09 三菱重工業株式会社 タービン翼列エンドウォール
JP5291355B2 (ja) * 2008-02-12 2013-09-18 三菱重工業株式会社 タービン翼列エンドウォール
EP2257709B1 (en) * 2008-02-22 2019-05-29 Horton, Inc. Hybrid flow fan apparatus
FR2928174B1 (fr) * 2008-02-28 2011-05-06 Snecma Aube avec plateforme non axisymetrique : creux et bosse sur extrados.
GB0808206D0 (en) * 2008-05-07 2008-06-11 Rolls Royce Plc A blade arrangement
FR2931214B1 (fr) * 2008-05-15 2013-07-26 Turbomeca Pale de rouet de compresseur a raccordement evolutif
US8206115B2 (en) * 2008-09-26 2012-06-26 General Electric Company Scalloped surface turbine stage with trailing edge ridges
JP5297228B2 (ja) * 2009-02-26 2013-09-25 三菱重工業株式会社 タービン翼及びガスタービン
US8105037B2 (en) * 2009-04-06 2012-01-31 United Technologies Corporation Endwall with leading-edge hump
EP2248996B1 (en) * 2009-05-04 2014-01-01 Alstom Technology Ltd Gas turbine
US9039375B2 (en) * 2009-09-01 2015-05-26 General Electric Company Non-axisymmetric airfoil platform shaping
US20110097205A1 (en) * 2009-10-28 2011-04-28 General Electric Company Turbine airfoil-sidewall integration
US9630277B2 (en) * 2010-03-15 2017-04-25 Siemens Energy, Inc. Airfoil having built-up surface with embedded cooling passage
JP5705608B2 (ja) * 2011-03-23 2015-04-22 三菱日立パワーシステムズ株式会社 回転機械の翼体の設計方法
DE102011006273A1 (de) 2011-03-28 2012-10-04 Rolls-Royce Deutschland Ltd & Co Kg Rotor einer Axialverdichterstufe einer Turbomaschine
DE102011006275A1 (de) * 2011-03-28 2012-10-04 Rolls-Royce Deutschland Ltd & Co Kg Stator einer Axialverdichterstufe einer Turbomaschine
US8926267B2 (en) 2011-04-12 2015-01-06 Siemens Energy, Inc. Ambient air cooling arrangement having a pre-swirler for gas turbine engine blade cooling
DE102011007767A1 (de) 2011-04-20 2012-10-25 Rolls-Royce Deutschland Ltd & Co Kg Strömungsmaschine
JP2012233406A (ja) 2011-04-28 2012-11-29 Hitachi Ltd ガスタービン静翼
US8864452B2 (en) * 2011-07-12 2014-10-21 Siemens Energy, Inc. Flow directing member for gas turbine engine
EP2559851A1 (en) 2011-08-19 2013-02-20 Siemens Aktiengesellschaft Exhaust diffuser and method for manufacturing an exhaust diffuser
US9017030B2 (en) * 2011-10-25 2015-04-28 Siemens Energy, Inc. Turbine component including airfoil with contour
US8992179B2 (en) * 2011-10-28 2015-03-31 General Electric Company Turbine of a turbomachine
US8967959B2 (en) 2011-10-28 2015-03-03 General Electric Company Turbine of a turbomachine
US9255480B2 (en) 2011-10-28 2016-02-09 General Electric Company Turbine of a turbomachine
US9051843B2 (en) 2011-10-28 2015-06-09 General Electric Company Turbomachine blade including a squeeler pocket
US9909425B2 (en) 2011-10-31 2018-03-06 Pratt & Whitney Canada Corporation Blade for a gas turbine engine
US8807930B2 (en) 2011-11-01 2014-08-19 United Technologies Corporation Non axis-symmetric stator vane endwall contour
DE102012207735A1 (de) * 2012-05-09 2013-11-14 Man Diesel & Turbo Se Schaufelgitter einer Strömungsmaschine
EP2662529A1 (en) * 2012-05-09 2013-11-13 Siemens Aktiengesellschaft Airfoil with PtAl bond coating and TBC, corresponding airfoil arrangement and manufacturing method
US9267386B2 (en) 2012-06-29 2016-02-23 United Technologies Corporation Fairing assembly
WO2014028056A1 (en) 2012-08-17 2014-02-20 United Technologies Corporation Contoured flowpath surface
US9212558B2 (en) 2012-09-28 2015-12-15 United Technologies Corporation Endwall contouring
US20140154068A1 (en) * 2012-09-28 2014-06-05 United Technologies Corporation Endwall Controuring
US9140128B2 (en) 2012-09-28 2015-09-22 United Technologes Corporation Endwall contouring
US9188017B2 (en) * 2012-12-18 2015-11-17 United Technologies Corporation Airfoil assembly with paired endwall contouring
US11143038B2 (en) 2013-03-04 2021-10-12 Raytheon Technologies Corporation Gas turbine engine high lift airfoil cooling in stagnation zone
JP5479624B2 (ja) * 2013-03-13 2014-04-23 三菱重工業株式会社 タービン翼及びガスタービン
US10196897B2 (en) 2013-03-15 2019-02-05 United Technologies Corporation Fan exit guide vane platform contouring
US10968747B2 (en) * 2013-03-15 2021-04-06 Raytheon Technologies Corporation Airfoil with thickened root and fan and engine incorporating same
EP3022400B1 (en) * 2013-07-15 2023-06-21 Raytheon Technologies Corporation Turbine vanes with variable fillets
GB201315078D0 (en) * 2013-08-23 2013-10-02 Siemens Ag Blade or vane arrangement for a gas turbine engine
DE102013219814B3 (de) * 2013-09-30 2014-11-27 Deutsches Zentrum für Luft- und Raumfahrt e.V. Axialverdichter
US9347320B2 (en) 2013-10-23 2016-05-24 General Electric Company Turbine bucket profile yielding improved throat
US9797258B2 (en) 2013-10-23 2017-10-24 General Electric Company Turbine bucket including cooling passage with turn
US9638041B2 (en) 2013-10-23 2017-05-02 General Electric Company Turbine bucket having non-axisymmetric base contour
US9551226B2 (en) 2013-10-23 2017-01-24 General Electric Company Turbine bucket with endwall contour and airfoil profile
US9376927B2 (en) * 2013-10-23 2016-06-28 General Electric Company Turbine nozzle having non-axisymmetric endwall contour (EWC)
US10352180B2 (en) 2013-10-23 2019-07-16 General Electric Company Gas turbine nozzle trailing edge fillet
US9528379B2 (en) 2013-10-23 2016-12-27 General Electric Company Turbine bucket having serpentine core
US9670784B2 (en) 2013-10-23 2017-06-06 General Electric Company Turbine bucket base having serpentine cooling passage with leading edge cooling
US9638212B2 (en) 2013-12-19 2017-05-02 Pratt & Whitney Canada Corp. Compressor variable vane assembly
US9631504B2 (en) * 2014-04-02 2017-04-25 Solar Turbines Incorporated Variable guide vane extended variable fillet
CN106661944B (zh) 2014-06-18 2019-03-19 西门子能源公司 用于燃气涡轮发动机的端壁构造
JP5916826B2 (ja) * 2014-09-24 2016-05-11 三菱日立パワーシステムズ株式会社 回転機械の翼体、及びガスタービン
GB201420011D0 (en) * 2014-11-11 2014-12-24 Rolls Royce Plc Gas turbine engine
GB201420010D0 (en) 2014-11-11 2014-12-24 Rolls Royce Plc Gas turbine engine
US10221708B2 (en) * 2014-12-03 2019-03-05 United Technologies Corporation Tangential on-board injection vanes
US10087767B2 (en) * 2014-12-09 2018-10-02 United Technologies Corporation Pre-diffuser with multiple radii
US10267158B2 (en) * 2014-12-22 2019-04-23 United Technologies Corporation Airfoil fillet
DE112016000685B4 (de) * 2015-02-10 2023-10-05 Mitsubishi Heavy Industries, Ltd. Turbine und gasturbine
US20160245297A1 (en) * 2015-02-23 2016-08-25 Howden Roots Llc Impeller comprising variably-dimensioned fillet to secure blades and compressor comprised thereof
US10107108B2 (en) 2015-04-29 2018-10-23 General Electric Company Rotor blade having a flared tip
US20170009589A1 (en) * 2015-07-09 2017-01-12 Siemens Energy, Inc. Gas turbine engine blade with increased wall thickness zone in the trailing edge-hub region
US10344597B2 (en) * 2015-08-17 2019-07-09 United Technologies Corporation Cupped contour for gas turbine engine blade assembly
US10125623B2 (en) 2016-02-09 2018-11-13 General Electric Company Turbine nozzle profile
US10196908B2 (en) 2016-02-09 2019-02-05 General Electric Company Turbine bucket having part-span connector and profile
US10001014B2 (en) 2016-02-09 2018-06-19 General Electric Company Turbine bucket profile
US10161255B2 (en) 2016-02-09 2018-12-25 General Electric Company Turbine nozzle having non-axisymmetric endwall contour (EWC)
US10221710B2 (en) * 2016-02-09 2019-03-05 General Electric Company Turbine nozzle having non-axisymmetric endwall contour (EWC) and profile
US10190421B2 (en) 2016-02-09 2019-01-29 General Electric Company Turbine bucket having tip shroud fillet, tip shroud cross-drilled apertures and profile
US10156149B2 (en) 2016-02-09 2018-12-18 General Electric Company Turbine nozzle having fillet, pinbank, throat region and profile
US10190417B2 (en) * 2016-02-09 2019-01-29 General Electric Company Turbine bucket having non-axisymmetric endwall contour and profile
US10408227B2 (en) * 2016-07-13 2019-09-10 Rolls-Royce Corporation Airfoil with stress-reducing fillet adapted for use in a gas turbine engine
EP3553277B1 (en) 2017-02-07 2023-06-28 IHI Corporation Airfoil of axial flow machine
US10577955B2 (en) 2017-06-29 2020-03-03 General Electric Company Airfoil assembly with a scalloped flow surface
KR20190046118A (ko) * 2017-10-25 2019-05-07 두산중공업 주식회사 터빈 블레이드
JP6982482B2 (ja) * 2017-12-11 2021-12-17 三菱パワー株式会社 可変静翼、及び圧縮機
US11767761B2 (en) * 2018-08-02 2023-09-26 Horton, Inc. Low solidity vehicle cooling fan
GB201813666D0 (en) * 2018-08-22 2018-10-03 Rolls Royce Plc Fan blade
BE1026579B1 (fr) * 2018-08-31 2020-03-30 Safran Aero Boosters Sa Aube a protuberance pour compresseur de turbomachine
US11118466B2 (en) * 2018-10-19 2021-09-14 Pratt & Whiiney Canada Corp. Compressor stator with leading edge fillet
JP7406920B2 (ja) 2019-03-20 2023-12-28 三菱重工業株式会社 タービン翼およびガスタービン
US20210079799A1 (en) * 2019-09-12 2021-03-18 General Electric Company Nozzle assembly for turbine engine
JP6776465B1 (ja) * 2020-01-27 2020-10-28 三菱パワー株式会社 タービン動翼
US11578607B2 (en) * 2020-12-15 2023-02-14 Pratt & Whitney Canada Corp. Airfoil having a spline fillet
CN115247575B (zh) * 2022-05-12 2024-05-03 中国航发四川燃气涡轮研究院 一种螺旋状涡轮叶片冷却单元及冷却结构

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2735612A (en) 1956-02-21 hausmann
FR781057A (fr) 1934-01-29 1935-05-08 Cem Comp Electro Mec Procédé et dispositif pour protéger contre les hautes températures les organes de turbo-machines plongés dans un fluide chaud en mouvement, en particulier les aubes de turbines à gaz ou à vapeur
GB504214A (en) 1937-02-24 1939-04-21 Rheinmetall Borsig Ag Werk Bor Improvements in and relating to turbo compressors
JPS5274706A (en) 1975-12-19 1977-06-23 Hitachi Ltd Turbine vane train
JPS5447907A (en) 1977-09-26 1979-04-16 Hitachi Ltd Blading structure for axial-flow fluid machine
GB2042675A (en) 1979-02-15 1980-09-24 Rolls Royce Secondary Flow Control in Axial Fluid Flow Machine
JPS55142909A (en) 1979-04-25 1980-11-07 Hitachi Ltd Turbine blade
US4739621A (en) 1984-10-11 1988-04-26 United Technologies Corporation Cooling scheme for combustor vane interface
DE59704501D1 (de) 1996-03-28 2001-10-11 Mtu Aero Engines Gmbh Schaufelblatt für Strömungsmaschinen
DE19612396C2 (de) 1996-03-28 1998-02-05 Univ Dresden Tech Schaufelblatt mit unterschiedlich ausgebildeten Profilquerschnitten
DE19650656C1 (de) 1996-12-06 1998-06-10 Mtu Muenchen Gmbh Turbomaschine mit transsonischer Verdichterstufe
US5846048A (en) 1997-05-22 1998-12-08 Mitsubishi Heavy Industries, Ltd. Gas turbine stationary blade unit
JP3316418B2 (ja) 1997-06-12 2002-08-19 三菱重工業株式会社 ガスタービン冷却動翼
US6126400A (en) 1999-02-01 2000-10-03 General Electric Company Thermal barrier coating wrap for turbine airfoil
WO2000061918A2 (en) 1999-03-22 2000-10-19 Siemens Westinghouse Power Corporation Airfoil leading edge vortex elimination device
US6419446B1 (en) 1999-08-05 2002-07-16 United Technologies Corporation Apparatus and method for inhibiting radial transfer of core gas flow within a core gas flow path of a gas turbine engine
JP2001271602A (ja) 2000-03-27 2001-10-05 Honda Motor Co Ltd ガスタービンエンジン

Also Published As

Publication number Publication date
AU2003274350A1 (en) 2004-05-13
TW200417682A (en) 2004-09-16
NO20052477D0 (no) 2005-05-23
EP1556584A1 (en) 2005-07-27
CA2446035A1 (en) 2004-04-23
KR20040036632A (ko) 2004-04-30
EP1556584B1 (en) 2016-12-07
US6969232B2 (en) 2005-11-29
PL376051A1 (en) 2005-12-12
WO2004038180A1 (en) 2004-05-06
JP2004278517A (ja) 2004-10-07
US20040081548A1 (en) 2004-04-29

Similar Documents

Publication Publication Date Title
NO20052477L (no) Anordning og fremgangsmate for reduksjon av varmebelastningen pa en skovel.
EP1936117A3 (en) Airfoil with plasma generator at leading edge for vortex reduction and corresponding operating method
EP1788192A3 (en) Gas turbine bucket with cooled platform edge and method of cooling platform leading edge
EP1795708A3 (en) Shrouded turbofan bleed duct
EP1895099A3 (en) Cascade tip baffle airfoil
ATE335917T1 (de) Turbomaschinenschaufel mit versetzter spitzenkante
PL342077A1 (en) Compressor's vane in particular for a gas turbine engine
CA2480985A1 (en) Triple circuit turbine blade
EP1712738A3 (en) Low solidity turbofan
EP3480432A3 (en) Modified structural truss for airfoils
JP2009534155A5 (no)
EP1314855A3 (en) Gas turbine engine aerofoil
EP1944465A3 (en) Gas turbine blade
NO20053711L (no) Rotorblad for et vindkraftanlegg
EP1813774A3 (en) Turbine element cooling
EP1637699A3 (en) Offset coriolis turbulator blade
EP1728990A3 (en) Auxiliary power unit supplied with air from the gas turbine
EP1770331A3 (en) Method of controlling bypass air split to gas turbine combustor
EP1445424A3 (en) Microcircuit cooling for a turbine blade tip
DK2004989T3 (da) Vindmøllevinge
EP1510165A3 (en) Silencer for vacuum cleaner
EP1688603A3 (en) Gas turbine engine assembly
EP2141327A3 (en) Rotor blade for a gas turbine engine
EP1726782A3 (en) Turbine blade trailing edge construction
ATE519036T1 (de) Verdichterschaufel

Legal Events

Date Code Title Description
FC2A Withdrawal, rejection or dismissal of laid open patent application