CN1831297A - 用于消除由端部泄漏涡流爆发诱发的压缩机定子振动的设备 - Google Patents
用于消除由端部泄漏涡流爆发诱发的压缩机定子振动的设备 Download PDFInfo
- Publication number
- CN1831297A CN1831297A CNA2006100594378A CN200610059437A CN1831297A CN 1831297 A CN1831297 A CN 1831297A CN A2006100594378 A CNA2006100594378 A CN A2006100594378A CN 200610059437 A CN200610059437 A CN 200610059437A CN 1831297 A CN1831297 A CN 1831297A
- Authority
- CN
- China
- Prior art keywords
- stator
- compressor
- blade
- blades
- stator blade
- 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.)
- Pending
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/08—Sealings
- F04D29/16—Sealings between pressure and suction sides
- F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
- F04D29/164—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
- F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/64—Mounting; Assembling; Disassembling of axial pumps
- F04D29/644—Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps
Applications Claiming Priority (2)
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 |
US11/072249 | 2005-03-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
CN1831297A true CN1831297A (zh) | 2006-09-13 |
Family
ID=36570747
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNA2006100594378A Pending CN1831297A (zh) | 2005-03-07 | 2006-03-07 | 用于消除由端部泄漏涡流爆发诱发的压缩机定子振动的设备 |
Country Status (4)
Country | Link |
---|---|
US (2) | US20060198726A1 (ja) |
EP (1) | EP1707744A3 (ja) |
JP (1) | JP2006250147A (ja) |
CN (1) | CN1831297A (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102207093A (zh) * | 2010-03-29 | 2011-10-05 | 株式会社日立制作所 | 压缩机 |
Families Citing this family (9)
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 |
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)
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 |
-
2005
- 2005-03-07 US US11/072,249 patent/US20060198726A1/en not_active Abandoned
-
2006
- 2006-03-03 JP JP2006057059A patent/JP2006250147A/ja not_active Withdrawn
- 2006-03-06 EP EP06251185A patent/EP1707744A3/en not_active Withdrawn
- 2006-03-07 CN CNA2006100594378A patent/CN1831297A/zh active Pending
-
2008
- 2008-05-29 US US12/155,101 patent/US20090123275A1/en not_active Abandoned
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102207093A (zh) * | 2010-03-29 | 2011-10-05 | 株式会社日立制作所 | 压缩机 |
CN102207093B (zh) * | 2010-03-29 | 2015-04-01 | 三菱日立电力系统株式会社 | 压缩机 |
US9534613B2 (en) | 2010-03-29 | 2017-01-03 | Mitsubishi Hitachi Power Systems, Ltd. | Compressor |
Also Published As
Publication number | Publication date |
---|---|
US20060198726A1 (en) | 2006-09-07 |
EP1707744A3 (en) | 2009-05-27 |
US20090123275A1 (en) | 2009-05-14 |
EP1707744A2 (en) | 2006-10-04 |
JP2006250147A (ja) | 2006-09-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C12 | Rejection of a patent application after its publication | ||
RJ01 | Rejection of invention patent application after publication |
Open date: 20060913 |