DE60032695D1 - Turbinenschaufel - Google Patents

Turbinenschaufel

Info

Publication number
DE60032695D1
DE60032695D1 DE60032695T DE60032695T DE60032695D1 DE 60032695 D1 DE60032695 D1 DE 60032695D1 DE 60032695 T DE60032695 T DE 60032695T DE 60032695 T DE60032695 T DE 60032695T DE 60032695 D1 DE60032695 D1 DE 60032695D1
Authority
DE
Germany
Prior art keywords
turbine blade
turbine
blade
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
DE60032695T
Other languages
English (en)
Other versions
DE60032695T2 (de
Inventor
Toby George Darkins
Mark Eugene Noe
Douglas Melton Carper
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE60032695D1 publication Critical patent/DE60032695D1/de
Publication of DE60032695T2 publication Critical patent/DE60032695T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • 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
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • 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
    • F05D2240/00—Components
    • F05D2240/80—Platforms for stationary or moving blades
    • 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
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/21—Oxide ceramics
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60032695T 1999-09-17 2000-07-14 Turbinenschaufel Expired - Lifetime DE60032695T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US399194 1999-09-17
US09/399,194 US6398501B1 (en) 1999-09-17 1999-09-17 Apparatus for reducing thermal stress in turbine airfoils

Publications (2)

Publication Number Publication Date
DE60032695D1 true DE60032695D1 (de) 2007-02-15
DE60032695T2 DE60032695T2 (de) 2007-10-31

Family

ID=23578539

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60032695T Expired - Lifetime DE60032695T2 (de) 1999-09-17 2000-07-14 Turbinenschaufel

Country Status (4)

Country Link
US (1) US6398501B1 (de)
EP (1) EP1085170B1 (de)
JP (1) JP2001132405A (de)
DE (1) DE60032695T2 (de)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6884030B2 (en) 2002-12-20 2005-04-26 General Electric Company Methods and apparatus for securing multi-piece nozzle assemblies
US7066717B2 (en) * 2004-04-22 2006-06-27 Siemens Power Generation, Inc. Ceramic matrix composite airfoil trailing edge arrangement
US7198458B2 (en) * 2004-12-02 2007-04-03 Siemens Power Generation, Inc. Fail safe cooling system for turbine vanes
US7255535B2 (en) * 2004-12-02 2007-08-14 Albrecht Harry A Cooling systems for stacked laminate CMC vane
US7153096B2 (en) * 2004-12-02 2006-12-26 Siemens Power Generation, Inc. Stacked laminate CMC turbine vane
US7435058B2 (en) * 2005-01-18 2008-10-14 Siemens Power Generation, Inc. Ceramic matrix composite vane with chordwise stiffener
US8137611B2 (en) * 2005-03-17 2012-03-20 Siemens Energy, Inc. Processing method for solid core ceramic matrix composite airfoil
US7785076B2 (en) * 2005-08-30 2010-08-31 Siemens Energy, Inc. Refractory component with ceramic matrix composite skeleton
DE102005054594A1 (de) * 2005-11-14 2007-05-16 Daubner & Stommel Gbr Rotorblatt für eine Windenergieanlage
US7600978B2 (en) * 2006-07-27 2009-10-13 Siemens Energy, Inc. Hollow CMC airfoil with internal stitch
JP5047078B2 (ja) * 2008-06-30 2012-10-10 三菱重工業株式会社 ガスタービン
US8033790B2 (en) * 2008-09-26 2011-10-11 Siemens Energy, Inc. Multiple piece turbine engine airfoil with a structural spar
US10137542B2 (en) 2010-01-14 2018-11-27 Senvion Gmbh Wind turbine rotor blade components and machine for making same
ES2510398T3 (es) 2010-01-14 2014-10-21 Neptco, Inc. Componentes de pala de rotor de aerogenerador y métodos para fabricar los mismos
US20110206522A1 (en) * 2010-02-24 2011-08-25 Ioannis Alvanos Rotating airfoil fabrication utilizing cmc
US10174627B2 (en) * 2013-02-27 2019-01-08 United Technologies Corporation Gas turbine engine thin wall composite vane airfoil
EP3059390B1 (de) * 2015-02-18 2020-03-04 Rolls-Royce Corporation Schaufelanordnung für einen gasturbinenmotor, profil und herstellungsverfahren
US11230935B2 (en) 2015-09-18 2022-01-25 General Electric Company Stator component cooling
US10738636B2 (en) 2016-12-14 2020-08-11 Rolls-Royce North American Technologies Inc. Dual wall airfoil with stiffened trailing edge
US10767502B2 (en) * 2016-12-23 2020-09-08 Rolls-Royce Corporation Composite turbine vane with three-dimensional fiber reinforcements
US11773723B2 (en) 2019-11-15 2023-10-03 Rtx Corporation Airfoil rib with thermal conductance element
US11898464B2 (en) 2021-04-16 2024-02-13 General Electric Company Airfoil for a gas turbine engine

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3017159A (en) * 1956-11-23 1962-01-16 Curtiss Wright Corp Hollow blade construction
US3628885A (en) * 1969-10-01 1971-12-21 Gen Electric Fluid-cooled airfoil
US3695778A (en) * 1970-09-18 1972-10-03 Trw Inc Turbine blade
GB1355558A (en) * 1971-07-02 1974-06-05 Rolls Royce Cooled vane or blade for a gas turbine engine
US3965963A (en) * 1973-11-16 1976-06-29 United Technologies Corporation Mold and process for casting high temperature alloys
US4073599A (en) * 1976-08-26 1978-02-14 Westinghouse Electric Corporation Hollow turbine blade tip closure
US4236870A (en) * 1977-12-27 1980-12-02 United Technologies Corporation Turbine blade
GB2041100B (en) * 1979-02-01 1982-11-03 Rolls Royce Cooled rotor blade for gas turbine engine
US4416585A (en) 1980-01-17 1983-11-22 Pratt & Whitney Aircraft Of Canada Limited Blade cooling for gas turbine engine
JPS62271902A (ja) * 1986-01-20 1987-11-26 Hitachi Ltd ガスタ−ビン冷却翼
JPH02131001U (de) * 1989-04-04 1990-10-30
JPH04219205A (ja) * 1990-03-31 1992-08-10 Ngk Insulators Ltd セラミック製高温部材
US5296308A (en) * 1992-08-10 1994-03-22 Howmet Corporation Investment casting using core with integral wall thickness control means
US5292230A (en) * 1992-12-16 1994-03-08 Westinghouse Electric Corp. Curvature steam turbine vane airfoil
US5507621A (en) 1995-01-30 1996-04-16 Rolls-Royce Plc Cooling air cooled gas turbine aerofoil
US5741117A (en) 1996-10-22 1998-04-21 United Technologies Corporation Method for cooling a gas turbine stator vane
US5820774A (en) 1996-10-28 1998-10-13 United Technologies Corporation Ceramic core for casting a turbine blade
WO1998031922A1 (de) * 1997-01-14 1998-07-23 Siemens Aktiengesellschaft Turbinenschaufel für eine strömungskraftmaschine, insbesondere eine gasturbine
JPH10212903A (ja) * 1997-01-28 1998-08-11 Mitsubishi Heavy Ind Ltd ガスタービン翼
JPH11117704A (ja) * 1997-10-13 1999-04-27 Toshiba Corp ガスタービン部品およびその製造方法
US6220817B1 (en) * 1997-11-17 2001-04-24 General Electric Company AFT flowing multi-tier airfoil cooling circuit
US6132169A (en) 1998-12-18 2000-10-17 General Electric Company Turbine airfoil and methods for airfoil cooling
US6186741B1 (en) 1999-07-22 2001-02-13 General Electric Company Airfoil component having internal cooling and method of cooling

Also Published As

Publication number Publication date
US6398501B1 (en) 2002-06-04
EP1085170B1 (de) 2007-01-03
DE60032695T2 (de) 2007-10-31
EP1085170A2 (de) 2001-03-21
JP2001132405A (ja) 2001-05-15
EP1085170A3 (de) 2003-01-02

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition