ITMI20041779A1 - Dispositivo di protezione di uno statore di una turbina - Google Patents

Dispositivo di protezione di uno statore di una turbina

Info

Publication number
ITMI20041779A1
ITMI20041779A1 IT001779A ITMI20041779A ITMI20041779A1 IT MI20041779 A1 ITMI20041779 A1 IT MI20041779A1 IT 001779 A IT001779 A IT 001779A IT MI20041779 A ITMI20041779 A IT MI20041779A IT MI20041779 A1 ITMI20041779 A1 IT MI20041779A1
Authority
IT
Italy
Prior art keywords
stator
turbine
protection device
protection
Prior art date
Application number
IT001779A
Other languages
English (en)
Inventor
Emanuele Bigi
Riccardo Cini
Piero Iacopetti
Original Assignee
Nuovo Pignone Spa
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 Nuovo Pignone Spa filed Critical Nuovo Pignone Spa
Priority to IT001779A priority Critical patent/ITMI20041779A1/it
Publication of ITMI20041779A1 publication Critical patent/ITMI20041779A1/it
Priority to JP2007531665A priority patent/JP4958782B2/ja
Priority to EP05790086A priority patent/EP1799968A1/en
Priority to US11/575,419 priority patent/US7972106B2/en
Priority to CN201010260634.2A priority patent/CN101906995B/zh
Priority to PCT/EP2005/009886 priority patent/WO2006029843A1/en
Priority to CA2580466A priority patent/CA2580466C/en
Priority to KR1020077008605A priority patent/KR101289613B1/ko
Priority to CNA2005800311442A priority patent/CN101023244A/zh

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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • 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
    • 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
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • 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
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141—Improvement 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)
IT001779A 2004-09-17 2004-09-17 Dispositivo di protezione di uno statore di una turbina ITMI20041779A1 (it)

Priority Applications (9)

Application Number Priority Date Filing Date Title
IT001779A ITMI20041779A1 (it) 2004-09-17 2004-09-17 Dispositivo di protezione di uno statore di una turbina
JP2007531665A JP4958782B2 (ja) 2004-09-17 2005-09-13 タービンステータ用の保護装置
EP05790086A EP1799968A1 (en) 2004-09-17 2005-09-13 Shroud for a gas turbine
US11/575,419 US7972106B2 (en) 2004-09-17 2005-09-13 Protection device for a turbine stator
CN201010260634.2A CN101906995B (zh) 2004-09-17 2005-09-13 涡轮机定子保护装置
PCT/EP2005/009886 WO2006029843A1 (en) 2004-09-17 2005-09-13 Shroud for a gas turbine
CA2580466A CA2580466C (en) 2004-09-17 2005-09-13 Shroud for a gas turbine
KR1020077008605A KR101289613B1 (ko) 2004-09-17 2005-09-13 가스 터빈 스테이터용 보호 장치
CNA2005800311442A CN101023244A (zh) 2004-09-17 2005-09-13 涡轮机定子保护装置

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT001779A ITMI20041779A1 (it) 2004-09-17 2004-09-17 Dispositivo di protezione di uno statore di una turbina

Publications (1)

Publication Number Publication Date
ITMI20041779A1 true ITMI20041779A1 (it) 2004-12-17

Family

ID=35482111

Family Applications (1)

Application Number Title Priority Date Filing Date
IT001779A ITMI20041779A1 (it) 2004-09-17 2004-09-17 Dispositivo di protezione di uno statore di una turbina

Country Status (8)

Country Link
US (1) US7972106B2 (it)
EP (1) EP1799968A1 (it)
JP (1) JP4958782B2 (it)
KR (1) KR101289613B1 (it)
CN (2) CN101906995B (it)
CA (1) CA2580466C (it)
IT (1) ITMI20041779A1 (it)
WO (1) WO2006029843A1 (it)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3028883B1 (fr) 2014-11-25 2019-11-22 Safran Aircraft Engines Arbre de rotor de turbomachine comportant une surface d'echange thermique perfectionnee
EP3048262A1 (en) * 2015-01-20 2016-07-27 Alstom Technology Ltd Wall for a hot gas channel in a gas turbine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3990807A (en) * 1974-12-23 1976-11-09 United Technologies Corporation Thermal response shroud for rotating body
JP3016157B2 (ja) * 1990-11-29 2000-03-06 株式会社日立製作所 タービン静翼
US5353865A (en) * 1992-03-30 1994-10-11 General Electric Company Enhanced impingement cooled components
FR2723177B1 (fr) * 1994-07-27 1996-09-06 Snecma Chambre de combustion comportant une double paroi
US5584651A (en) * 1994-10-31 1996-12-17 General Electric Company Cooled shroud
WO2001066914A1 (fr) 2000-03-07 2001-09-13 Mitsubishi Heavy Industries, Ltd. Anneau fendu de turbine a gaz
US6402464B1 (en) * 2000-08-29 2002-06-11 General Electric Company Enhanced heat transfer surface for cast-in-bump-covered cooling surfaces and methods of enhancing heat transfer
US6779597B2 (en) * 2002-01-16 2004-08-24 General Electric Company Multiple impingement cooled structure
US7033138B2 (en) * 2002-09-06 2006-04-25 Mitsubishi Heavy Industries, Ltd. Ring segment of gas turbine
US6814538B2 (en) * 2003-01-22 2004-11-09 General Electric Company Turbine stage one shroud configuration and method for service enhancement

Also Published As

Publication number Publication date
WO2006029843A1 (en) 2006-03-23
WO2006029843A8 (en) 2006-05-18
CN101906995B (zh) 2014-03-05
US7972106B2 (en) 2011-07-05
US20090180860A1 (en) 2009-07-16
KR20070057950A (ko) 2007-06-07
KR101289613B1 (ko) 2013-07-24
JP2008513657A (ja) 2008-05-01
CA2580466A1 (en) 2006-03-23
EP1799968A1 (en) 2007-06-27
CN101023244A (zh) 2007-08-22
JP4958782B2 (ja) 2012-06-20
CA2580466C (en) 2011-05-10
CN101906995A (zh) 2010-12-08

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