JP6078353B2 - ガスタービン - Google Patents

ガスタービン Download PDF

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Publication number
JP6078353B2
JP6078353B2 JP2013010031A JP2013010031A JP6078353B2 JP 6078353 B2 JP6078353 B2 JP 6078353B2 JP 2013010031 A JP2013010031 A JP 2013010031A JP 2013010031 A JP2013010031 A JP 2013010031A JP 6078353 B2 JP6078353 B2 JP 6078353B2
Authority
JP
Japan
Prior art keywords
stage
gas turbine
blade
seal
end 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.)
Active
Application number
JP2013010031A
Other languages
English (en)
Japanese (ja)
Other versions
JP2014141910A5 (enExample
JP2014141910A (ja
Inventor
隼人 前川
隼人 前川
健治 七瀧
健治 七瀧
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.)
Mitsubishi Power Ltd
Original Assignee
Mitsubishi Hitachi Power Systems 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 Mitsubishi Hitachi Power Systems Ltd filed Critical Mitsubishi Hitachi Power Systems Ltd
Priority to JP2013010031A priority Critical patent/JP6078353B2/ja
Priority to CN201310524927.0A priority patent/CN103939149A/zh
Priority to EP13192770.9A priority patent/EP2759677A1/en
Priority to US14/078,770 priority patent/US9617867B2/en
Publication of JP2014141910A publication Critical patent/JP2014141910A/ja
Publication of JP2014141910A5 publication Critical patent/JP2014141910A5/ja
Application granted granted Critical
Publication of JP6078353B2 publication Critical patent/JP6078353B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
    • 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
    • F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/321—Application in turbines in gas turbines for a special turbine stage
    • F05D2220/3212—Application in turbines in gas turbines for a special turbine stage the first stage of a turbine
    • 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
    • F05D2300/61—Syntactic materials, i.e. hollow spheres embedded in a matrix

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
JP2013010031A 2013-01-23 2013-01-23 ガスタービン Active JP6078353B2 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2013010031A JP6078353B2 (ja) 2013-01-23 2013-01-23 ガスタービン
CN201310524927.0A CN103939149A (zh) 2013-01-23 2013-10-30 燃气轮机
EP13192770.9A EP2759677A1 (en) 2013-01-23 2013-11-13 Gas turbine
US14/078,770 US9617867B2 (en) 2013-01-23 2013-11-13 Gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2013010031A JP6078353B2 (ja) 2013-01-23 2013-01-23 ガスタービン

Publications (3)

Publication Number Publication Date
JP2014141910A JP2014141910A (ja) 2014-08-07
JP2014141910A5 JP2014141910A5 (enExample) 2015-12-17
JP6078353B2 true JP6078353B2 (ja) 2017-02-08

Family

ID=49554157

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013010031A Active JP6078353B2 (ja) 2013-01-23 2013-01-23 ガスタービン

Country Status (4)

Country Link
US (1) US9617867B2 (enExample)
EP (1) EP2759677A1 (enExample)
JP (1) JP6078353B2 (enExample)
CN (1) CN103939149A (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150040567A1 (en) * 2013-08-08 2015-02-12 General Electric Company Systems and Methods for Reducing or Limiting One or More Flows Between a Hot Gas Path and a Wheel Space of a Turbine
EP2886801B1 (en) * 2013-12-20 2019-04-24 Ansaldo Energia IP UK Limited Seal system for a gas turbine and corresponding gas turbine
JP6601677B2 (ja) 2016-02-16 2019-11-06 三菱日立パワーシステムズ株式会社 シール装置及び回転機械
JP7122274B2 (ja) * 2019-02-27 2022-08-19 三菱重工業株式会社 軸流タービン
US11415016B2 (en) 2019-11-11 2022-08-16 Rolls-Royce Plc Turbine section assembly with ceramic matrix composite components and interstage sealing features
US11591921B1 (en) 2021-11-05 2023-02-28 Rolls-Royce Plc Ceramic matrix composite vane assembly

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4588607A (en) * 1984-11-28 1986-05-13 United Technologies Corporation Method of applying continuously graded metallic-ceramic layer on metallic substrates
JPH06159099A (ja) * 1992-11-25 1994-06-07 Toshiba Corp 軸流流体機械
US5429478A (en) * 1994-03-31 1995-07-04 United Technologies Corporation Airfoil having a seal and an integral heat shield
US5522698A (en) * 1994-04-29 1996-06-04 United Technologies Corporation Brush seal support and vane assembly windage cover
JPH10252412A (ja) * 1997-03-12 1998-09-22 Mitsubishi Heavy Ind Ltd ガスタービンシール装置
DE10353810A1 (de) * 2003-11-17 2005-06-23 Rolls-Royce Deutschland Ltd & Co Kg Innendeckband für die Statorschaufeln des Verdichters einer Gasturbine
US7465152B2 (en) 2005-09-16 2008-12-16 General Electric Company Angel wing seals for turbine blades and methods for selecting stator, rotor and wing seal profiles
US20070273104A1 (en) * 2006-05-26 2007-11-29 Siemens Power Generation, Inc. Abradable labyrinth tooth seal
US20080044284A1 (en) * 2006-08-16 2008-02-21 United Technologies Corporation Segmented fluid seal assembly
US7500824B2 (en) * 2006-08-22 2009-03-10 General Electric Company Angel wing abradable seal and sealing method
US7708520B2 (en) * 2006-11-29 2010-05-04 United Technologies Corporation Gas turbine engine with concave pocket with knife edge seal
US20090238683A1 (en) * 2008-03-24 2009-09-24 United Technologies Corporation Vane with integral inner air seal
JP2010151267A (ja) * 2008-12-26 2010-07-08 Hitachi Ltd シール構造、およびこれを用いたガスタービン
JP4856257B2 (ja) * 2010-03-24 2012-01-18 川崎重工業株式会社 タービンロータのシール構造
US8979481B2 (en) * 2011-10-26 2015-03-17 General Electric Company Turbine bucket angel wing features for forward cavity flow control and related method
US9145788B2 (en) * 2012-01-24 2015-09-29 General Electric Company Retrofittable interstage angled seal

Also Published As

Publication number Publication date
US20140205445A1 (en) 2014-07-24
JP2014141910A (ja) 2014-08-07
CN103939149A (zh) 2014-07-23
US9617867B2 (en) 2017-04-11
EP2759677A1 (en) 2014-07-30

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