EP1849960A3 - Aube de turbine ayant un passage interne de refroidissement - Google Patents

Aube de turbine ayant un passage interne de refroidissement Download PDF

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Publication number
EP1849960A3
EP1849960A3 EP07008241A EP07008241A EP1849960A3 EP 1849960 A3 EP1849960 A3 EP 1849960A3 EP 07008241 A EP07008241 A EP 07008241A EP 07008241 A EP07008241 A EP 07008241A EP 1849960 A3 EP1849960 A3 EP 1849960A3
Authority
EP
European Patent Office
Prior art keywords
wall surface
side wall
blade
trailing edge
cooling passage
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.)
Withdrawn
Application number
EP07008241A
Other languages
German (de)
English (en)
Other versions
EP1849960A2 (fr
Inventor
Ryou c/o Hitachi Ltd Intellectual Property Group Akiyama
Yasuhiro c/o Hitachi Ltd Intellectual Property Group Horiuchi
Shinya c/o Hitachi Ltd Intellectual Property Group Marushima
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.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
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 Hitachi Ltd filed Critical Hitachi Ltd
Publication of EP1849960A2 publication Critical patent/EP1849960A2/fr
Publication of EP1849960A3 publication Critical patent/EP1849960A3/fr
Withdrawn legal-status Critical Current

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
    • 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
    • F01D5/20Specially-shaped blade tips to seal space between tips and stator
    • 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
    • F01D9/041Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • F05D2260/221Improvement of heat transfer
    • F05D2260/2212Improvement of heat transfer by creating turbulence
    • 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
    • F05D2260/221Improvement of heat transfer
    • F05D2260/2214Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141Improvement of heat transfer by increasing the heat transfer surface using fins or ribs

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
EP07008241A 2006-04-27 2007-04-23 Aube de turbine ayant un passage interne de refroidissement Withdrawn EP1849960A3 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2006122884A JP2007292006A (ja) 2006-04-27 2006-04-27 内部に冷却通路を有するタービン翼

Publications (2)

Publication Number Publication Date
EP1849960A2 EP1849960A2 (fr) 2007-10-31
EP1849960A3 true EP1849960A3 (fr) 2010-03-10

Family

ID=38007269

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07008241A Withdrawn EP1849960A3 (fr) 2006-04-27 2007-04-23 Aube de turbine ayant un passage interne de refroidissement

Country Status (2)

Country Link
EP (1) EP1849960A3 (fr)
JP (1) JP2007292006A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107366555B (zh) * 2016-05-12 2022-03-08 通用电气公司 叶片以及涡轮转子叶片

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5436457B2 (ja) 2008-03-07 2014-03-05 アルストム テクノロジー リミテッド ガスタービンのための翼
ES2542064T3 (es) * 2008-03-28 2015-07-30 Alstom Technology Ltd Álabe de guía para una turbina de gas y turbina de gas con un álabe de guía de esta clase
JP5189406B2 (ja) 2008-05-14 2013-04-24 三菱重工業株式会社 ガスタービン翼およびこれを備えたガスタービン
EP2602439A1 (fr) * 2011-11-21 2013-06-12 Siemens Aktiengesellschaft Composant de gaz chaud pouvant être refroidi pour une turbine à gaz
US20140064983A1 (en) * 2012-08-31 2014-03-06 General Electric Company Airfoil and method for manufacturing an airfoil
US20150204237A1 (en) * 2014-01-17 2015-07-23 General Electric Company Turbine blade and method for enhancing life of the turbine blade
WO2015116338A1 (fr) 2014-01-30 2015-08-06 United Technologies Corporation Configuration d'embase de refroidissement de bord de fuite pour une surface portante de moteur à turbine à gaz
US10208604B2 (en) 2016-04-27 2019-02-19 United Technologies Corporation Cooling features with three dimensional chevron geometry
KR102114681B1 (ko) * 2018-09-21 2020-05-25 두산중공업 주식회사 핀-핀 배열을 포함하는 터빈 블레이드

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4278400A (en) * 1978-09-05 1981-07-14 United Technologies Corporation Coolable rotor blade
EP0032646A1 (fr) * 1980-01-10 1981-07-29 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Aube de distributeur de turbine
GB2112467A (en) * 1981-12-28 1983-07-20 United Technologies Corp Coolable airfoil for a rotary machine
JPH05156901A (ja) * 1991-12-02 1993-06-22 Hitachi Ltd ガスタービン冷却静翼
JPH06137102A (ja) * 1992-10-26 1994-05-17 Mitsubishi Heavy Ind Ltd ガスタービン中空動翼
US5538394A (en) * 1993-12-28 1996-07-23 Kabushiki Kaisha Toshiba Cooled turbine blade for a gas turbine
US5772397A (en) * 1996-05-08 1998-06-30 Alliedsignal Inc. Gas turbine airfoil with aft internal cooling
DE19807563A1 (de) * 1997-02-25 1998-09-24 Mitsubishi Heavy Ind Ltd Kühlkonstruktion zum Kühlen einer Montageplatte für Antriebsschaufeln einer Gasturbine
GB2349920A (en) * 1999-05-10 2000-11-15 Abb Alstom Power Ch Ag Cooling arrangement for turbine blade
EP1467065A2 (fr) * 2003-04-08 2004-10-13 United Technologies Corporation Aube de turbine
EP1538305A2 (fr) * 2003-11-19 2005-06-08 United Technologies Corporation Aube comprenant un arrangement à densité variable d'entretoises au niveau du bord de fuite
EP1674661A2 (fr) * 2004-12-23 2006-06-28 United Technologies Corporation Passage de refroidissement d'une aube de turbine
EP1715139A2 (fr) * 2005-04-22 2006-10-25 United Technologies Corporation Refroidissement du bord de fuite d'une aube de turbine

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4278400A (en) * 1978-09-05 1981-07-14 United Technologies Corporation Coolable rotor blade
EP0032646A1 (fr) * 1980-01-10 1981-07-29 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Aube de distributeur de turbine
GB2112467A (en) * 1981-12-28 1983-07-20 United Technologies Corp Coolable airfoil for a rotary machine
JPH05156901A (ja) * 1991-12-02 1993-06-22 Hitachi Ltd ガスタービン冷却静翼
JPH06137102A (ja) * 1992-10-26 1994-05-17 Mitsubishi Heavy Ind Ltd ガスタービン中空動翼
US5538394A (en) * 1993-12-28 1996-07-23 Kabushiki Kaisha Toshiba Cooled turbine blade for a gas turbine
US5772397A (en) * 1996-05-08 1998-06-30 Alliedsignal Inc. Gas turbine airfoil with aft internal cooling
DE19807563A1 (de) * 1997-02-25 1998-09-24 Mitsubishi Heavy Ind Ltd Kühlkonstruktion zum Kühlen einer Montageplatte für Antriebsschaufeln einer Gasturbine
GB2349920A (en) * 1999-05-10 2000-11-15 Abb Alstom Power Ch Ag Cooling arrangement for turbine blade
EP1467065A2 (fr) * 2003-04-08 2004-10-13 United Technologies Corporation Aube de turbine
EP1538305A2 (fr) * 2003-11-19 2005-06-08 United Technologies Corporation Aube comprenant un arrangement à densité variable d'entretoises au niveau du bord de fuite
EP1674661A2 (fr) * 2004-12-23 2006-06-28 United Technologies Corporation Passage de refroidissement d'une aube de turbine
EP1715139A2 (fr) * 2005-04-22 2006-10-25 United Technologies Corporation Refroidissement du bord de fuite d'une aube de turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107366555B (zh) * 2016-05-12 2022-03-08 通用电气公司 叶片以及涡轮转子叶片

Also Published As

Publication number Publication date
EP1849960A2 (fr) 2007-10-31
JP2007292006A (ja) 2007-11-08

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