DE60026469D1 - Prallkühlung eines hinterschnittenen Bereichs bei Turbinenleitapparaten - Google Patents

Prallkühlung eines hinterschnittenen Bereichs bei Turbinenleitapparaten

Info

Publication number
DE60026469D1
DE60026469D1 DE60026469T DE60026469T DE60026469D1 DE 60026469 D1 DE60026469 D1 DE 60026469D1 DE 60026469 T DE60026469 T DE 60026469T DE 60026469 T DE60026469 T DE 60026469T DE 60026469 D1 DE60026469 D1 DE 60026469D1
Authority
DE
Germany
Prior art keywords
side wall
nozzle
wall
apertures
impingement plate
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
DE60026469T
Other languages
English (en)
Other versions
DE60026469T2 (de
Inventor
Steven Sebastian Burdgick
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
Publication of DE60026469D1 publication Critical patent/DE60026469D1/de
Application granted granted Critical
Publication of DE60026469T2 publication Critical patent/DE60026469T2/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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • 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
    • 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
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium
    • F05D2260/2322—Heat transfer, e.g. cooling characterized by the cooling medium steam

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60026469T 2000-04-11 2000-12-07 Prallkühlung eines hinterschnittenen Bereichs bei Turbinenleitapparaten Expired - Lifetime DE60026469T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/546,766 US6419445B1 (en) 2000-04-11 2000-04-11 Apparatus for impingement cooling a side wall adjacent an undercut region of a turbine nozzle segment
US546766 2000-04-11

Publications (2)

Publication Number Publication Date
DE60026469D1 true DE60026469D1 (de) 2006-05-04
DE60026469T2 DE60026469T2 (de) 2006-11-16

Family

ID=24181911

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60026469T Expired - Lifetime DE60026469T2 (de) 2000-04-11 2000-12-07 Prallkühlung eines hinterschnittenen Bereichs bei Turbinenleitapparaten

Country Status (7)

Country Link
US (1) US6419445B1 (de)
EP (1) EP1146203B1 (de)
JP (1) JP4713729B2 (de)
KR (1) KR100694921B1 (de)
AT (1) ATE319917T1 (de)
CZ (1) CZ20004034A3 (de)
DE (1) DE60026469T2 (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6832892B2 (en) 2002-12-11 2004-12-21 General Electric Company Sealing of steam turbine bucket hook leakages using a braided rope seal
US6939106B2 (en) * 2002-12-11 2005-09-06 General Electric Company Sealing of steam turbine nozzle hook leakages using a braided rope seal
US6971844B2 (en) * 2003-05-29 2005-12-06 General Electric Company Horizontal joint sealing system for steam turbine diaphragm assemblies
US6843637B1 (en) 2003-08-04 2005-01-18 General Electric Company Cooling circuit within a turbine nozzle and method of cooling a turbine nozzle
US7029228B2 (en) * 2003-12-04 2006-04-18 General Electric Company Method and apparatus for convective cooling of side-walls of turbine nozzle segments
US6994520B2 (en) * 2004-05-26 2006-02-07 General Electric Company Internal core profile for a turbine nozzle airfoil
EP1767835A1 (de) * 2005-09-22 2007-03-28 Siemens Aktiengesellschaft Hochtemperaturfeste Dichtungsanordnung, insbesondere für Gasturbinen
GB2479865B (en) * 2010-04-26 2013-07-10 Rolls Royce Plc An installation having a thermal transfer arrangement
US9039350B2 (en) 2012-01-09 2015-05-26 General Electric Company Impingement cooling system for use with contoured surfaces
US9011078B2 (en) 2012-01-09 2015-04-21 General Electric Company Turbine vane seal carrier with slots for cooling and assembly
US8944751B2 (en) 2012-01-09 2015-02-03 General Electric Company Turbine nozzle cooling assembly
US9133724B2 (en) 2012-01-09 2015-09-15 General Electric Company Turbomachine component including a cover plate
US9011079B2 (en) 2012-01-09 2015-04-21 General Electric Company Turbine nozzle compartmentalized cooling system
US8864445B2 (en) 2012-01-09 2014-10-21 General Electric Company Turbine nozzle assembly methods
US8845285B2 (en) * 2012-01-10 2014-09-30 General Electric Company Gas turbine stator assembly
US9638047B1 (en) * 2013-11-18 2017-05-02 Florida Turbine Technologies, Inc. Multiple wall impingement plate for sequential impingement cooling of an endwall
US9683444B1 (en) * 2013-11-18 2017-06-20 Florida Turbine Technologies, Inc. Multiple wall impingement plate for sequential impingement cooling of a turbine hot part
US9540956B2 (en) * 2013-11-22 2017-01-10 Siemens Energy, Inc. Industrial gas turbine exhaust system with modular struts and collars
US9644497B2 (en) 2013-11-22 2017-05-09 Siemens Energy, Inc. Industrial gas turbine exhaust system with splined profile tail cone
US9598981B2 (en) 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
US9512740B2 (en) 2013-11-22 2016-12-06 Siemens Energy, Inc. Industrial gas turbine exhaust system with area ruled exhaust path
US9745920B2 (en) * 2014-09-11 2017-08-29 General Electric Company Gas turbine nozzles with embossments in airfoil cavities
US10260356B2 (en) * 2016-06-02 2019-04-16 General Electric Company Nozzle cooling system for a gas turbine engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE794195A (fr) * 1972-01-18 1973-07-18 Bbc Sulzer Turbomaschinen Aube directrice refroidie pour des turbines a gaz
GB1519590A (en) * 1974-11-11 1978-08-02 Rolls Royce Gas turbine engine
JPS6363504U (de) * 1986-10-15 1988-04-26
US5116199A (en) * 1990-12-20 1992-05-26 General Electric Company Blade tip clearance control apparatus using shroud segment annular support ring thermal expansion
JPH04311604A (ja) * 1991-04-11 1992-11-04 Toshiba Corp タービン静翼
US5634766A (en) 1994-08-23 1997-06-03 General Electric Co. Turbine stator vane segments having combined air and steam cooling circuits
US5823741A (en) * 1996-09-25 1998-10-20 General Electric Co. Cooling joint connection for abutting segments in a gas turbine engine
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
US6126389A (en) * 1998-09-02 2000-10-03 General Electric Co. Impingement cooling for the shroud of a gas turbine

Also Published As

Publication number Publication date
JP4713729B2 (ja) 2011-06-29
KR100694921B1 (ko) 2007-03-14
EP1146203A3 (de) 2003-01-02
EP1146203B1 (de) 2006-03-08
US6419445B1 (en) 2002-07-16
EP1146203A2 (de) 2001-10-17
DE60026469T2 (de) 2006-11-16
ATE319917T1 (de) 2006-03-15
KR20010096525A (ko) 2001-11-07
CZ20004034A3 (cs) 2001-11-14
JP2001303906A (ja) 2001-10-31
US20020028134A1 (en) 2002-03-07

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