JP2013253604A5 - - Google Patents

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Publication number
JP2013253604A5
JP2013253604A5 JP2013118401A JP2013118401A JP2013253604A5 JP 2013253604 A5 JP2013253604 A5 JP 2013253604A5 JP 2013118401 A JP2013118401 A JP 2013118401A JP 2013118401 A JP2013118401 A JP 2013118401A JP 2013253604 A5 JP2013253604 A5 JP 2013253604A5
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JP
Japan
Prior art keywords
fluid
rotor
upstream portion
downstream
region
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.)
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Application number
JP2013118401A
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English (en)
Japanese (ja)
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JP2013253604A (ja
JP6122346B2 (ja
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Publication date
Priority claimed from US13/489,552 external-priority patent/US9267513B2/en
Application filed filed Critical
Publication of JP2013253604A publication Critical patent/JP2013253604A/ja
Publication of JP2013253604A5 publication Critical patent/JP2013253604A5/ja
Application granted granted Critical
Publication of JP6122346B2 publication Critical patent/JP6122346B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013118401A 2012-06-06 2013-06-05 タービンエンジン圧縮機の温度を制御する方法およびタービンエンジンの圧縮機 Active JP6122346B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/489,552 2012-06-06
US13/489,552 US9267513B2 (en) 2012-06-06 2012-06-06 Method for controlling temperature of a turbine engine compressor and compressor of a turbine engine

Publications (3)

Publication Number Publication Date
JP2013253604A JP2013253604A (ja) 2013-12-19
JP2013253604A5 true JP2013253604A5 (enExample) 2016-07-14
JP6122346B2 JP6122346B2 (ja) 2017-04-26

Family

ID=48569974

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013118401A Active JP6122346B2 (ja) 2012-06-06 2013-06-05 タービンエンジン圧縮機の温度を制御する方法およびタービンエンジンの圧縮機

Country Status (5)

Country Link
US (1) US9267513B2 (enExample)
EP (1) EP2672122B1 (enExample)
JP (1) JP6122346B2 (enExample)
CN (1) CN103470318B (enExample)
RU (1) RU2013125743A (enExample)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11377957B2 (en) * 2017-05-09 2022-07-05 General Electric Company Gas turbine engine with a diffuser cavity cooled compressor
US11674396B2 (en) 2021-07-30 2023-06-13 General Electric Company Cooling air delivery assembly

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL72348C (enExample) 1948-10-15
FR2370170A1 (fr) * 1976-11-05 1978-06-02 Snecma Procede et dispositif pour la diminution du bruit des turbomachines
US4137705A (en) 1977-07-25 1979-02-06 General Electric Company Cooling air cooler for a gas turbine engine
US4576547A (en) * 1983-11-03 1986-03-18 United Technologies Corporation Active clearance control
US5697208A (en) * 1995-06-02 1997-12-16 Solar Turbines Incorporated Turbine cooling cycle
JP3758835B2 (ja) * 1997-10-22 2006-03-22 三菱重工業株式会社 空気圧縮機ディスクの冷却によるクリアランス制御方法
EP1640587B1 (de) 2004-09-22 2008-07-09 Siemens Aktiengesellschaft Kühlsystem für eine Gasturbine und Verfahren zum Kühlen einer Gasturbine
EP1795725B1 (de) 2005-10-12 2011-01-19 Alstom Technology Ltd Gasturbine mit geregelter Luftkühlung
DE102007026455A1 (de) * 2007-06-05 2008-12-11 Rolls-Royce Deutschland Ltd & Co Kg Strahltriebwerk mit Verdichterluftzirkulation und Verfahren zum Betreiben desselben
FR2933458B1 (fr) * 2008-07-01 2010-09-03 Snecma Compresseur axialo-centrifuge a systeme de pilotage
RU2539404C2 (ru) 2010-11-29 2015-01-20 Альстом Текнолоджи Лтд Осевая газовая турбина

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