JP2011069366A5 - - Google Patents

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Publication number
JP2011069366A5
JP2011069366A5 JP2010212081A JP2010212081A JP2011069366A5 JP 2011069366 A5 JP2011069366 A5 JP 2011069366A5 JP 2010212081 A JP2010212081 A JP 2010212081A JP 2010212081 A JP2010212081 A JP 2010212081A JP 2011069366 A5 JP2011069366 A5 JP 2011069366A5
Authority
JP
Japan
Prior art keywords
gas turbine
sealing member
passage
fixed frame
opening
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.)
Granted
Application number
JP2010212081A
Other languages
English (en)
Japanese (ja)
Other versions
JP5840353B2 (ja
JP2011069366A (ja
Filing date
Publication date
Priority claimed from EP09171142.4A external-priority patent/EP2302173B8/en
Application filed filed Critical
Publication of JP2011069366A publication Critical patent/JP2011069366A/ja
Publication of JP2011069366A5 publication Critical patent/JP2011069366A5/ja
Application granted granted Critical
Publication of JP5840353B2 publication Critical patent/JP5840353B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2010212081A 2009-09-23 2010-09-22 ガスタービン Expired - Fee Related JP5840353B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP09171142.4A EP2302173B8 (en) 2009-09-23 2009-09-23 Gas turbine
EP09171142.4 2009-09-23

Publications (3)

Publication Number Publication Date
JP2011069366A JP2011069366A (ja) 2011-04-07
JP2011069366A5 true JP2011069366A5 (enExample) 2015-09-03
JP5840353B2 JP5840353B2 (ja) 2016-01-06

Family

ID=41820796

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2010212081A Expired - Fee Related JP5840353B2 (ja) 2009-09-23 2010-09-22 ガスタービン

Country Status (3)

Country Link
US (1) US8979479B2 (enExample)
EP (1) EP2302173B8 (enExample)
JP (1) JP5840353B2 (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5898443B2 (ja) * 2011-03-28 2016-04-06 富士フイルム株式会社 セルロースアシレートフィルム、位相差フィルム、偏光板および液晶表示装置
US9970299B2 (en) * 2015-09-16 2018-05-15 General Electric Company Mixing chambers for turbine wheel space cooling
US10132195B2 (en) 2015-10-20 2018-11-20 General Electric Company Wheel space purge flow mixing chamber
US10125632B2 (en) 2015-10-20 2018-11-13 General Electric Company Wheel space purge flow mixing chamber
US10519873B2 (en) 2016-04-06 2019-12-31 General Electric Company Air bypass system for rotor shaft cooling
US10641174B2 (en) 2017-01-18 2020-05-05 General Electric Company Rotor shaft cooling

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1351268A (fr) 1963-03-20 1964-01-31 Rolls Royce Moteur à turbine à gaz comportant un aubage de turbine refroidi
GB2081392B (en) * 1980-08-06 1983-09-21 Rolls Royce Turbomachine seal
GB2246836B (en) 1981-05-07 1992-05-13 Rolls Royce Fluid flow valve
US4456427A (en) * 1981-06-11 1984-06-26 General Electric Company Cooling air injector for turbine blades
US4882902A (en) * 1986-04-30 1989-11-28 General Electric Company Turbine cooling air transferring apparatus
US4666368A (en) * 1986-05-01 1987-05-19 General Electric Company Swirl nozzle for a cooling system in gas turbine engines
US5135354A (en) * 1990-09-14 1992-08-04 United Technologies Corporation Gas turbine blade and disk
FR2707698B1 (fr) 1993-07-15 1995-08-25 Snecma Turbomachine munie d'un moyen de soufflage d'air sur un élément de rotor.
DE10330471A1 (de) * 2003-07-05 2005-02-03 Alstom Technology Ltd Vorrichtung zum Abscheiden von Fremdpartikeln aus der den Laufschaufeln einer Turbine zuführbaren Kühlluft
GB2426289B (en) * 2005-04-01 2007-07-04 Rolls Royce Plc Cooling system for a gas turbine engine
US7189055B2 (en) * 2005-05-31 2007-03-13 Pratt & Whitney Canada Corp. Coverplate deflectors for redirecting a fluid flow
US8262342B2 (en) * 2008-07-10 2012-09-11 Honeywell International Inc. Gas turbine engine assemblies with recirculated hot gas ingestion
JP5134570B2 (ja) 2009-02-23 2013-01-30 三菱重工業株式会社 タービンの冷却構造およびガスタービン

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