CN102758654A - 独立控制的燃气涡轮进口导叶和变距定子叶片 - Google Patents
独立控制的燃气涡轮进口导叶和变距定子叶片 Download PDFInfo
- Publication number
- CN102758654A CN102758654A CN2012101387436A CN201210138743A CN102758654A CN 102758654 A CN102758654 A CN 102758654A CN 2012101387436 A CN2012101387436 A CN 2012101387436A CN 201210138743 A CN201210138743 A CN 201210138743A CN 102758654 A CN102758654 A CN 102758654A
- Authority
- CN
- China
- Prior art keywords
- vsv
- igv
- cylinder body
- servomechanism
- body group
- 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
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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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/057—Control or regulation
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
-
- 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
- F05D2260/00—Function
- F05D2260/40—Transmission of power
- F05D2260/406—Transmission of power through hydraulic systems
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Supercharger (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
Claims (15)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/091,540 US9068470B2 (en) | 2011-04-21 | 2011-04-21 | Independently-controlled gas turbine inlet guide vanes and variable stator vanes |
US13/091,540 | 2011-04-21 | ||
US13/091540 | 2011-04-21 |
Publications (2)
Publication Number | Publication Date |
---|---|
CN102758654A true CN102758654A (zh) | 2012-10-31 |
CN102758654B CN102758654B (zh) | 2015-09-23 |
Family
ID=46084804
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201210138743.6A Expired - Fee Related CN102758654B (zh) | 2011-04-21 | 2012-04-23 | 独立控制的燃气涡轮进口导叶和变距定子叶片 |
Country Status (3)
Country | Link |
---|---|
US (1) | US9068470B2 (zh) |
EP (1) | EP2514927B1 (zh) |
CN (1) | CN102758654B (zh) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109764012A (zh) * | 2019-03-06 | 2019-05-17 | 上海电气燃气轮机有限公司 | 一种液压执行机构及燃气轮机 |
CN114576012A (zh) * | 2022-03-29 | 2022-06-03 | 华北电力科学研究院有限责任公司 | 燃气轮机进口导叶调节方法及装置 |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20120134783A1 (en) | 2010-11-30 | 2012-05-31 | General Electric Company | System and method for operating a compressor |
US8909454B2 (en) * | 2011-04-08 | 2014-12-09 | General Electric Company | Control of compression system with independently actuated inlet guide and/or stator vanes |
US20130074512A1 (en) * | 2011-09-23 | 2013-03-28 | Steven William Tillery | Inlet fluid flow and impingement angle control |
DE102012007129A1 (de) * | 2012-04-10 | 2013-10-10 | Rolls-Royce Deutschland Ltd & Co Kg | Leitschaufelverstellvorrichtung einer Gasturbine |
US9500200B2 (en) * | 2012-04-19 | 2016-11-22 | General Electric Company | Systems and methods for detecting the onset of compressor stall |
CN102966386B (zh) * | 2012-11-12 | 2016-06-08 | 国家电网公司 | 一种电液伺服控制装置 |
EP2971598B1 (en) * | 2013-03-13 | 2019-08-21 | United Technologies Corporation | Variable vane control system |
US9492780B2 (en) | 2014-01-16 | 2016-11-15 | Bha Altair, Llc | Gas turbine inlet gas phase contaminant removal |
US10001066B2 (en) * | 2014-08-28 | 2018-06-19 | General Electric Company | Rotary actuator for variable geometry vanes |
US10502136B2 (en) | 2014-10-06 | 2019-12-10 | Bha Altair, Llc | Filtration system for use in a gas turbine engine assembly and method of assembling thereof |
US10443509B2 (en) | 2014-10-31 | 2019-10-15 | General Electric Company | System and method for turbomachinery vane prognostics and diagnostics |
US20170108032A1 (en) * | 2015-10-16 | 2017-04-20 | General Electric Company | Stepped shaft assembly |
US9982686B2 (en) | 2015-11-04 | 2018-05-29 | General Electric Company | Turnbuckle dampening links |
US10215047B2 (en) | 2015-12-28 | 2019-02-26 | General Electric Company | Actuation system utilizing MEMS technology |
US10408217B2 (en) | 2016-03-15 | 2019-09-10 | General Electric Company | Controlling a compressor of a gas turbine engine |
US10400680B2 (en) | 2016-09-28 | 2019-09-03 | General Electric Company | System and method for synchronizing the operation of airfoil actuators of a gas turbine engine |
US10519964B2 (en) | 2016-12-06 | 2019-12-31 | General Electric Company | System and method for turbomachinery rotor and blade prognostics and diagnostics |
US10125779B2 (en) | 2016-12-06 | 2018-11-13 | General Electric Company | System and method for turbomachinery vane diagnostics |
US20190061918A1 (en) * | 2017-08-22 | 2019-02-28 | Hamilton Sundstrand Corporation | Electric hydraulic actuation system for a safety critical application |
US10961919B2 (en) | 2017-08-29 | 2021-03-30 | Pratt & Whitney Canada Corp | Corrected parameters control logic for variable geometry mechanisms |
DE102018211535A1 (de) * | 2018-07-11 | 2020-01-16 | MTU Aero Engines AG | Verstelleinrichtung und Verfahren zur Verstellung eines Leitgitters einer Turbomaschine |
US10704411B2 (en) | 2018-08-03 | 2020-07-07 | General Electric Company | Variable vane actuation system for a turbo machine |
GB201818075D0 (en) * | 2018-11-06 | 2018-12-19 | Rolls Royce Plc | Actuator |
GB201903062D0 (en) * | 2019-03-07 | 2019-04-24 | Rolls Royce Plc | Fuel control system |
US20220098995A1 (en) * | 2020-07-23 | 2022-03-31 | Williams International Co., L.L.C. | Gas-turbine-engine overspeed protection system |
US11725526B1 (en) | 2022-03-08 | 2023-08-15 | General Electric Company | Turbofan engine having nacelle with non-annular inlet |
EP4390064A1 (en) * | 2022-12-23 | 2024-06-26 | Rolls-Royce Deutschland Ltd & Co KG | A gas turbine engine control system and method for limiting turbine overspeed in case of a shaft failure |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5044879A (en) * | 1989-01-25 | 1991-09-03 | Rolls-Royce Plc | Variable stator vane arrangement for an axial flow compressor |
US20050147492A1 (en) * | 2003-12-30 | 2005-07-07 | Mahoney Timothy D. | Gas turbine engine electromechanical variable inlet guide vane actuation system |
EP1724472A2 (fr) * | 2005-05-17 | 2006-11-22 | Snecma | Système de commande d'étages d'aubes de stator à angle de calage variable de turbomachine |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2780064A (en) * | 1953-11-10 | 1957-02-05 | Gen Dynamics Corp | Accumulator for hydraulic systems |
US2931168A (en) * | 1955-05-24 | 1960-04-05 | Gen Electric | Variable stator engine control system |
US3973391A (en) | 1974-08-08 | 1976-08-10 | Westinghouse Electric Corporation | Control apparatus for modulating the inlet guide vanes of a gas turbine employed in a combined cycle electric power generating plant as a function of load or inlet blade path temperature |
US3914066A (en) * | 1974-09-27 | 1975-10-21 | Gen Motors Corp | Vane actuation system |
GB2206381B (en) | 1987-06-30 | 1991-10-09 | Rolls Royce Plc | A variable stator vane arrangement for a compressor |
US5102049A (en) | 1987-11-24 | 1992-04-07 | The United States Of America As Represented By The Secretary Of The Air Force | Vane control mechanism |
US5622473A (en) | 1995-11-17 | 1997-04-22 | General Electric Company | Variable stator vane assembly |
JP3600438B2 (ja) * | 1998-05-22 | 2004-12-15 | 三菱重工業株式会社 | ガスタービンの可変翼回転装置 |
US6209198B1 (en) | 1998-12-16 | 2001-04-03 | General Electric Company | Method of assembling a variable stator vane assembly |
US6226974B1 (en) | 1999-06-25 | 2001-05-08 | General Electric Co. | Method of operation of industrial gas turbine for optimal performance |
US6794766B2 (en) | 2001-06-29 | 2004-09-21 | General Electric Company | Method and operational strategy for controlling variable stator vanes of a gas turbine power generator compressor component during under-frequency events |
US6735955B2 (en) | 2001-10-10 | 2004-05-18 | Goodrich Pump & Engine Control Systems, Inc. | Control system for positioning compressor inlet guide vanes |
US7220098B2 (en) | 2003-05-27 | 2007-05-22 | General Electric Company | Wear resistant variable stator vane assemblies |
GB2402180B (en) | 2003-05-30 | 2006-09-20 | Rolls Royce Plc | Variable stator vane actuating levers |
GB0326544D0 (en) | 2003-11-14 | 2003-12-17 | Rolls Royce Plc | Variable stator vane arrangement for a compressor |
GB2412947B (en) | 2004-04-07 | 2006-06-14 | Rolls Royce Plc | Variable stator vane assemblies |
US7125222B2 (en) | 2004-04-14 | 2006-10-24 | General Electric Company | Gas turbine engine variable vane assembly |
US7278819B2 (en) | 2005-07-05 | 2007-10-09 | General Electric Company | Variable stator vane lever arm assembly and method of assembling same |
JP4699130B2 (ja) * | 2005-08-03 | 2011-06-08 | 三菱重工業株式会社 | ガスタービンの入口案内翼制御装置 |
US7445427B2 (en) | 2005-12-05 | 2008-11-04 | General Electric Company | Variable stator vane assembly and bushing thereof |
US7413401B2 (en) | 2006-01-17 | 2008-08-19 | General Electric Company | Methods and apparatus for controlling variable stator vanes |
JP2010196550A (ja) * | 2009-02-24 | 2010-09-09 | Mitsubishi Heavy Ind Ltd | 回転軸とレバーの取付構造、回転軸とレバーの取付方法、及び、流体機械 |
US8152406B1 (en) * | 2010-11-08 | 2012-04-10 | Saudi Arabian Oil Company | Crash barrier with over-pressure relief system |
-
2011
- 2011-04-21 US US13/091,540 patent/US9068470B2/en not_active Expired - Fee Related
-
2012
- 2012-04-19 EP EP12164847.1A patent/EP2514927B1/en active Active
- 2012-04-23 CN CN201210138743.6A patent/CN102758654B/zh not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5044879A (en) * | 1989-01-25 | 1991-09-03 | Rolls-Royce Plc | Variable stator vane arrangement for an axial flow compressor |
US20050147492A1 (en) * | 2003-12-30 | 2005-07-07 | Mahoney Timothy D. | Gas turbine engine electromechanical variable inlet guide vane actuation system |
EP1724472A2 (fr) * | 2005-05-17 | 2006-11-22 | Snecma | Système de commande d'étages d'aubes de stator à angle de calage variable de turbomachine |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109764012A (zh) * | 2019-03-06 | 2019-05-17 | 上海电气燃气轮机有限公司 | 一种液压执行机构及燃气轮机 |
CN109764012B (zh) * | 2019-03-06 | 2024-05-07 | 上海电气燃气轮机有限公司 | 一种液压执行机构及燃气轮机 |
CN114576012A (zh) * | 2022-03-29 | 2022-06-03 | 华北电力科学研究院有限责任公司 | 燃气轮机进口导叶调节方法及装置 |
CN114576012B (zh) * | 2022-03-29 | 2023-09-26 | 华北电力科学研究院有限责任公司 | 燃气轮机进口导叶调节方法及装置 |
Also Published As
Publication number | Publication date |
---|---|
US9068470B2 (en) | 2015-06-30 |
EP2514927B1 (en) | 2019-10-23 |
EP2514927A2 (en) | 2012-10-24 |
EP2514927A3 (en) | 2018-01-10 |
CN102758654B (zh) | 2015-09-23 |
US20120269613A1 (en) | 2012-10-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150923 Termination date: 20210423 |
|
IP01 | Partial invalidation of patent right | ||
IP01 | Partial invalidation of patent right |
Commission number: 4W106999 Conclusion of examination: The patent right for invention No. 201210138743.6 was declared partially invalid, and the patent right was maintained valid on the basis of claims 1-14 submitted by the patentee on May 28, 2018 Decision date of declaring invalidation: 20181105 Decision number of declaring invalidation: 37669 Denomination of invention: Independently controlled gas turbine inlet guide vanes and variable pitch stator vanes Granted publication date: 20150923 Patentee: General Electric Co. |