DE60112996D1 - Turbinenleitschaufelsegment - Google Patents

Turbinenleitschaufelsegment

Info

Publication number
DE60112996D1
DE60112996D1 DE60112996T DE60112996T DE60112996D1 DE 60112996 D1 DE60112996 D1 DE 60112996D1 DE 60112996 T DE60112996 T DE 60112996T DE 60112996 T DE60112996 T DE 60112996T DE 60112996 D1 DE60112996 D1 DE 60112996D1
Authority
DE
Germany
Prior art keywords
impingement
steam
cooling
vane
wall
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 - Fee Related
Application number
DE60112996T
Other languages
English (en)
Other versions
DE60112996T2 (de
Inventor
James Michael Storey
Stephen William Tesh
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 DE60112996D1 publication Critical patent/DE60112996D1/de
Application granted granted Critical
Publication of DE60112996T2 publication Critical patent/DE60112996T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using 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
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • 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
    • F01D5/187—Convection cooling
    • F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • F01D5/189—Convection 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
    • 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
    • F05D2260/205—Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
DE60112996T 2000-06-01 2001-01-31 Dampfauslassstromkonstruktion für hintere Kammern einer Strömungsfläche Expired - Fee Related DE60112996T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/585,840 US6398486B1 (en) 2000-06-01 2000-06-01 Steam exit flow design for aft cavities of an airfoil
US585840 2000-06-01

Publications (2)

Publication Number Publication Date
DE60112996D1 true DE60112996D1 (de) 2005-10-06
DE60112996T2 DE60112996T2 (de) 2006-06-08

Family

ID=24343171

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60112996T Expired - Fee Related DE60112996T2 (de) 2000-06-01 2001-01-31 Dampfauslassstromkonstruktion für hintere Kammern einer Strömungsfläche

Country Status (7)

Country Link
US (1) US6398486B1 (de)
EP (1) EP1160418B1 (de)
JP (1) JP2002004803A (de)
KR (1) KR100534813B1 (de)
AT (1) ATE303502T1 (de)
CZ (1) CZ20004488A3 (de)
DE (1) DE60112996T2 (de)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002155703A (ja) * 2000-11-21 2002-05-31 Mitsubishi Heavy Ind Ltd ガスタービン静翼−翼環間蒸気通路のシール構造
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
US6951444B2 (en) * 2002-10-22 2005-10-04 Siemens Aktiengesselschaft Turbine and a turbine vane for a turbine
FR2851286B1 (fr) * 2003-02-18 2006-07-28 Snecma Moteurs Aubes de turbine refroidie a fuite d'air de refroidissement reduite
US6742984B1 (en) 2003-05-19 2004-06-01 General Electric Company Divided insert for steam cooled nozzles and method for supporting and separating divided insert
US6830432B1 (en) 2003-06-24 2004-12-14 Siemens Westinghouse Power Corporation Cooling of combustion turbine airfoil fillets
FR2858829B1 (fr) * 2003-08-12 2008-03-14 Snecma Moteurs Aube refroidie de moteur a turbine a gaz
US7086829B2 (en) * 2004-02-03 2006-08-08 General Electric Company Film cooling for the trailing edge of a steam cooled nozzle
US7118325B2 (en) * 2004-06-14 2006-10-10 United Technologies Corporation Cooling passageway turn
US7220103B2 (en) * 2004-10-18 2007-05-22 United Technologies Corporation Impingement cooling of large fillet of an airfoil
US7488156B2 (en) * 2006-06-06 2009-02-10 Siemens Energy, Inc. Turbine airfoil with floating wall mechanism and multi-metering diffusion technique
US7621718B1 (en) 2007-03-28 2009-11-24 Florida Turbine Technologies, Inc. Turbine vane with leading edge fillet region impingement cooling
US8100632B2 (en) * 2008-12-03 2012-01-24 General Electric Company Cooling system for a turbomachine
US8353668B2 (en) * 2009-02-18 2013-01-15 United Technologies Corporation Airfoil insert having a tab extending away from the body defining a portion of outlet periphery
JP4841678B2 (ja) * 2010-04-15 2011-12-21 川崎重工業株式会社 ガスタービンのタービン静翼
GB2486488A (en) 2010-12-17 2012-06-20 Ge Aviat Systems Ltd Testing a transient voltage protection device
JP5931351B2 (ja) 2011-05-13 2016-06-08 三菱重工業株式会社 タービン静翼
EP2540969A1 (de) * 2011-06-27 2013-01-02 Siemens Aktiengesellschaft Aufprallkühlung von Turbinenschaufeln oder -flügeln
US8864445B2 (en) * 2012-01-09 2014-10-21 General Electric Company Turbine nozzle assembly methods
US9039350B2 (en) * 2012-01-09 2015-05-26 General Electric Company Impingement cooling system for use with contoured surfaces
US9567908B2 (en) 2012-04-27 2017-02-14 General Electric Company Mitigating vortex pumping effect upstream of oil seal
US9353647B2 (en) 2012-04-27 2016-05-31 General Electric Company Wide discourager tooth
EP2921650B1 (de) 2014-03-20 2017-10-04 Ansaldo Energia Switzerland AG Turbinenschaufel mit gekühlte Hohlkehle
US10053996B2 (en) * 2014-12-12 2018-08-21 United Technologies Corporation Sliding baffle inserts
US9771814B2 (en) * 2015-03-09 2017-09-26 United Technologies Corporation Tolerance resistance coverplates
EP3112592B1 (de) * 2015-07-02 2019-06-19 Ansaldo Energia Switzerland AG Gasturbinenschaufel
US10273812B2 (en) 2015-12-18 2019-04-30 Pratt & Whitney Canada Corp. Turbine rotor coolant supply system
JP6651378B2 (ja) * 2016-02-22 2020-02-19 三菱日立パワーシステムズ株式会社 インサート組品、翼、ガスタービン、および、翼の製造方法
US10370983B2 (en) * 2017-07-28 2019-08-06 Rolls-Royce Corporation Endwall cooling system
CN111535869B (zh) * 2020-04-29 2022-07-29 中国航发湖南动力机械研究所 涡轮导向器
KR102356488B1 (ko) 2020-08-21 2022-02-07 두산중공업 주식회사 터빈 베인 및 이를 포함하는 가스 터빈
CN113090335A (zh) * 2021-05-14 2021-07-09 中国航发湖南动力机械研究所 一种用于涡轮转子叶片的冲击加气膜双层壁冷却结构

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2467292A1 (fr) * 1979-10-09 1981-04-17 Snecma Dispositif de reglage du jeu entre les aubes mobiles et l'anneau de turbine
FR2681095B1 (fr) * 1991-09-05 1993-11-19 Snecma Distributeur de turbine carene.
US5145315A (en) * 1991-09-27 1992-09-08 Westinghouse Electric Corp. Gas turbine vane cooling air insert
US5253976A (en) 1991-11-19 1993-10-19 General Electric Company Integrated steam and air cooling for combined cycle gas turbines
US5320483A (en) * 1992-12-30 1994-06-14 General Electric Company Steam and air cooling for stator stage of a turbine
US5634766A (en) 1994-08-23 1997-06-03 General Electric Co. Turbine stator vane segments having combined air and steam cooling circuits
US5685693A (en) 1995-03-31 1997-11-11 General Electric Co. Removable inner turbine shell with bucket tip clearance control

Also Published As

Publication number Publication date
KR100534813B1 (ko) 2005-12-08
ATE303502T1 (de) 2005-09-15
EP1160418A2 (de) 2001-12-05
JP2002004803A (ja) 2002-01-09
DE60112996T2 (de) 2006-06-08
EP1160418B1 (de) 2005-08-31
US6398486B1 (en) 2002-06-04
CZ20004488A3 (cs) 2002-01-16
EP1160418A3 (de) 2003-09-24
KR20010109466A (ko) 2001-12-10

Similar Documents

Publication Publication Date Title
DE60112996D1 (de) Turbinenleitschaufelsegment
EP1149983A3 (de) Filmkühlung für eine im geschlossenen Kreislauf gekühlte Turbinenschaufel
ATE334300T1 (de) Turbinenleitschaufel-segment mit inneren kühlkreisläufen
KR20090127913A (ko) 가스 터빈 엔진의 안내 날개 어셈블리에 대한 안내 날개 덕트 요소
JP4879267B2 (ja) ガスタービンにおける冷却形タービン翼とそのタービン翼の利用
US6283708B1 (en) Coolable vane or blade for a turbomachine
EP1156186A3 (de) Im geschlossenen Kreislauf gekühlte Turbinenschaufel mit einer Lufttasche zur Filmkühlung
US6036436A (en) Gas turbine cooling stationary vane
US5591002A (en) Closed or open air cooling circuits for nozzle segments with wheelspace purge
EP1156187B1 (de) Turbinenleitschaufel mit Einsatz mit Bereichen zur Prallkühlung und Konvektionskühlung
EP0670954B1 (de) Verstärkte hinterkante für gusskern einer turbinenschaufel
JP4256704B2 (ja) ガスタービンエンジンのノズル組立体を冷却する方法及び装置
EP0698723A2 (de) Geschlossener Kühlkreislauf für Turbinenleitschaufel
JP2004239263A (ja) タービンブレードおよびタービンブレードの先端部の冷却方法
IT8224879A1 (it) Elemento aerodinamico raffreddabile per macchine rotative
CA2251198A1 (en) Gas turbine stationary blade
JP2010502872A (ja) 冷却形タービン動翼
EP1052374B1 (de) Kühlkreislauf für dampf- und luftgekühlte Turbinenleitschaufeln
DE60021058D1 (de) Methode um die Dicke der Seitenwand von Turbinenleitapparatsegmenten anzupassen um die Kühlung zu verbessern
ATE319917T1 (de) Prallkühlung eines hinterschnittenen bereichs bei turbinenleitapparaten
JP2019116893A (ja) 先端レール冷却通路を有するタービン構成要素
US20010005555A1 (en) Cooled heat shield
JPH11257003A (ja) インピンジメント冷却装置
ATE296942T1 (de) Prallkühlung eines hinterschnittenen bereichs bei turbinenleitapparaten
KR20000052372A (ko) 인접한 냉각 통로를 연결하는 타원형 횡단 개구를 갖는가스 터빈 부품

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee