JP2006250147A5 - - Google Patents

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Publication number
JP2006250147A5
JP2006250147A5 JP2006057059A JP2006057059A JP2006250147A5 JP 2006250147 A5 JP2006250147 A5 JP 2006250147A5 JP 2006057059 A JP2006057059 A JP 2006057059A JP 2006057059 A JP2006057059 A JP 2006057059A JP 2006250147 A5 JP2006250147 A5 JP 2006250147A5
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JP
Japan
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Withdrawn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
JP2006057059A
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JP2006250147A (ja
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Publication date
Priority claimed from US11/072,249 external-priority patent/US20060198726A1/en
Application filed filed Critical
Publication of JP2006250147A publication Critical patent/JP2006250147A/ja
Publication of JP2006250147A5 publication Critical patent/JP2006250147A5/ja
Withdrawn legal-status Critical Current

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JP2006057059A 2005-03-07 2006-03-03 圧縮機 Withdrawn JP2006250147A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/072,249 US20060198726A1 (en) 2005-03-07 2005-03-07 Apparatus for eliminating compressor stator vibration induced by tip leakage vortex bursting

Publications (2)

Publication Number Publication Date
JP2006250147A JP2006250147A (ja) 2006-09-21
JP2006250147A5 true JP2006250147A5 (ja) 2009-04-16

Family

ID=36570747

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2006057059A Withdrawn JP2006250147A (ja) 2005-03-07 2006-03-03 圧縮機

Country Status (4)

Country Link
US (2) US20060198726A1 (ja)
EP (1) EP1707744A3 (ja)
JP (1) JP2006250147A (ja)
CN (1) CN1831297A (ja)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7743497B2 (en) * 2005-10-06 2010-06-29 General Electric Company Method of providing non-uniform stator vane spacing in a compressor
EP2218918A1 (de) * 2009-02-13 2010-08-18 Siemens Aktiengesellschaft Axialturboverdichter für eine Gasturbine mit geringen Spaltverlusten und Diffusorverlusten
EP2218876A1 (de) * 2009-02-16 2010-08-18 Siemens Aktiengesellschaft Dichtungsring zum Abdichten eines Radialspalts in einer Gasturbine
JP5192507B2 (ja) 2010-03-19 2013-05-08 川崎重工業株式会社 ガスタービンエンジン
JP5147886B2 (ja) * 2010-03-29 2013-02-20 株式会社日立製作所 圧縮機
US9115594B2 (en) 2010-12-28 2015-08-25 Rolls-Royce Corporation Compressor casing treatment for gas turbine engine
JP5342579B2 (ja) 2011-02-28 2013-11-13 三菱重工業株式会社 回転機械の静翼ユニット、回転機械の静翼ユニットの製造方法及び回転機械の静翼ユニットの結合方法
US20130142640A1 (en) * 2011-12-02 2013-06-06 David P. Houston Alternate shroud width to provide mistuning on compressor stator clusters
US20180080454A1 (en) * 2016-09-16 2018-03-22 United Technologies Corporation Segmented stator vane
US11629606B2 (en) * 2021-05-26 2023-04-18 General Electric Company Split-line stator vane assembly

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2556161A (en) * 1944-03-21 1951-06-12 Power Jets Res & Dev Ltd Gas diffusers for air supplied to combustion chambers
US2693904A (en) * 1950-11-14 1954-11-09 A V Roe Canada Ltd Air bleed for compressors
US3265290A (en) * 1964-09-01 1966-08-09 Anthony J Cali Axial flow compressors for jet engines
US3300121A (en) * 1965-02-24 1967-01-24 Gen Motors Corp Axial-flow compressor
US3861823A (en) * 1973-01-15 1975-01-21 Caterpillar Tractor Co Compressor with retractable guide vanes
CH579218A5 (ja) * 1974-06-17 1976-08-31 Bbc Sulzer Turbomaschinen
US4022540A (en) * 1975-10-02 1977-05-10 General Electric Company Frangible airfoil structure
US4011028A (en) * 1975-10-16 1977-03-08 Anatoly Nikolaevich Borsuk Axial-flow transsonic compressor
US4008978A (en) * 1976-03-19 1977-02-22 General Motors Corporation Ceramic turbine structures
US4503668A (en) * 1983-04-12 1985-03-12 The United States Of America As Represented By The Secretary Of The Air Force Strutless diffuser for gas turbine engine
US5127797A (en) * 1990-09-12 1992-07-07 United Technologies Corporation Compressor case attachment means
US5333995A (en) * 1993-08-09 1994-08-02 General Electric Company Wear shim for a turbine engine
US5681142A (en) * 1993-12-20 1997-10-28 United Technologies Corporation Damping means for a stator assembly of a gas turbine engine
US5697208A (en) * 1995-06-02 1997-12-16 Solar Turbines Incorporated Turbine cooling cycle
US5639212A (en) * 1996-03-29 1997-06-17 General Electric Company Cavity sealed compressor
US6312219B1 (en) * 1999-11-05 2001-11-06 General Electric Company Narrow waist vane
US6338609B1 (en) * 2000-02-18 2002-01-15 General Electric Company Convex compressor casing
DE10355240A1 (de) * 2003-11-26 2005-07-07 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Fluidentnahme
JP4328269B2 (ja) * 2004-07-28 2009-09-09 株式会社日立製作所 ガスタービン装置

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