IN2012DE00979A - - Google Patents

Download PDF

Info

Publication number
IN2012DE00979A
IN2012DE00979A IN979DE2012A IN2012DE00979A IN 2012DE00979 A IN2012DE00979 A IN 2012DE00979A IN 979DE2012 A IN979DE2012 A IN 979DE2012A IN 2012DE00979 A IN2012DE00979 A IN 2012DE00979A
Authority
IN
India
Application number
Inventor
Karl Dean Minto
Original Assignee
Gen Electric
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Gen Electric filed Critical Gen Electric
Publication of IN2012DE00979A publication Critical patent/IN2012DE00979A/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/56Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16Control of working fluid flow
    • F02C9/20Control of working fluid flow by throttling; by adjusting vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • F04D27/0246Surge control by varying geometry within the pumps, e.g. by adjusting vanes
IN979DE2012 2011-04-08 2012-03-30 IN2012DE00979A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/083,056 US8909454B2 (en) 2011-04-08 2011-04-08 Control of compression system with independently actuated inlet guide and/or stator vanes

Publications (1)

Publication Number Publication Date
IN2012DE00979A true IN2012DE00979A (en) 2015-09-11

Family

ID=46022042

Family Applications (1)

Application Number Title Priority Date Filing Date
IN979DE2012 IN2012DE00979A (en) 2011-04-08 2012-03-30

Country Status (4)

Country Link
US (1) US8909454B2 (en)
EP (1) EP2508762B1 (en)
CN (1) CN102734196B (en)
IN (1) IN2012DE00979A (en)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
DE112013005424B4 (en) * 2012-12-04 2021-09-23 Trane International Inc. Chiller capacity control devices, methods and systems
US9777641B2 (en) * 2012-12-19 2017-10-03 General Electric Company System for turbomachine vane control
CN103184999B (en) * 2013-03-12 2015-06-10 河北钢铁股份有限公司邯郸分公司 Limiting critical point positioning method for guide vane executing mechanism of compressor
JP6366259B2 (en) * 2013-11-18 2018-08-01 三菱日立パワーシステムズ株式会社 Control device and control method for two-shaft gas turbine
EP2907990A1 (en) * 2014-02-18 2015-08-19 Siemens Aktiengesellschaft Method for operating a gas turbine installation, and the same
GB201407314D0 (en) 2014-04-25 2014-06-11 Rolls Royce Plc Control of a gas turbine engine
JP6364363B2 (en) * 2015-02-23 2018-07-25 三菱日立パワーシステムズ株式会社 Two-shaft gas turbine and control device and control method thereof
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
EP3225812B1 (en) * 2016-03-29 2019-02-27 Mitsubishi Hitachi Power Systems, Ltd. A two-shaft gas turbine, and the control method of opening degree of inlet guide vane of the gas turbine
US10358934B2 (en) * 2016-04-11 2019-07-23 United Technologies Corporation Method and apparatus for adjusting variable vanes
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
US10822104B2 (en) 2017-08-29 2020-11-03 Pratt & Whitney Canada Corp. Variable geometries transient control logic
US10961919B2 (en) 2017-08-29 2021-03-30 Pratt & Whitney Canada Corp Corrected parameters control logic for variable geometry mechanisms
JP2019052586A (en) * 2017-09-14 2019-04-04 株式会社Ihi Compressor control device
US11486316B2 (en) 2018-09-13 2022-11-01 Pratt & Whitney Canada Corp. Method and system for adjusting a variable geometry mechanism
US11168612B2 (en) 2018-09-21 2021-11-09 Pratt & Whitney Canada Corp. Signal processing for variable geometry mechanism control

Family Cites Families (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3779665A (en) * 1972-09-22 1973-12-18 Gen Electric Combined variable angle stator and windmill control system
DE3624951C1 (en) * 1986-02-28 1987-10-29 Mtu Muenchen Gmbh Turbocompressor with variable geometry
GB2227527B (en) * 1989-01-25 1993-06-09 Rolls Royce Plc A variable stator vane arrangement for an axial flow compressor
US5042245A (en) * 1989-02-27 1991-08-27 United Technologies Corporation Method and system for controlling variable compressor geometry
JPH04132899A (en) * 1990-09-25 1992-05-07 Mitsubishi Heavy Ind Ltd Axial blower
US5281087A (en) * 1992-06-10 1994-01-25 General Electric Company Industrial gas turbine engine with dual panel variable vane assembly
US5993152A (en) * 1997-10-14 1999-11-30 General Electric Company Nonlinear vane actuation
EP1228316A1 (en) * 1999-08-13 2002-08-07 Argo-Tech Corporation Variable capacity pump for gas turbine engines
US6466858B1 (en) * 2000-11-02 2002-10-15 General Electric Company Methods and apparatus for monitoring gas turbine engine operation
US6487847B1 (en) * 2000-11-03 2002-12-03 General Electric Company Gas turbine engine fuel control system
GB2376515B (en) * 2001-06-13 2004-09-29 Rolls Royce Plc Bleed valve assembly
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
JP2003113721A (en) 2001-10-03 2003-04-18 Mitsubishi Heavy Ind Ltd Fuel ratio control method and device for gas turbine combustor
US6823675B2 (en) * 2002-11-13 2004-11-30 General Electric Company Adaptive model-based control systems and methods for controlling a gas turbine
GB0307035D0 (en) * 2003-03-26 2003-04-30 Rolls Royce Plc Acceleration control in a multi-spool gas turbine engine
JP2005155590A (en) 2003-10-30 2005-06-16 Mitsubishi Heavy Ind Ltd Gas turbine control apparatus, gas turbine system and gas turbine control method
US7096657B2 (en) * 2003-12-30 2006-08-29 Honeywell International, Inc. Gas turbine engine electromechanical variable inlet guide vane actuation system
EP1632678A1 (en) * 2004-09-01 2006-03-08 Ford Global Technologies, LLC, A subsidary of Ford Motor Company Orthogonal swirl generator
US7762084B2 (en) * 2004-11-12 2010-07-27 Rolls-Royce Canada, Ltd. System and method for controlling the working line position in a gas turbine engine compressor
WO2006059972A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
EP1828547B1 (en) * 2004-12-01 2011-11-30 United Technologies Corporation Turbofan comprising a plurality of individually controlled inlet guide vanes and corresponding controlling method
US7690889B2 (en) * 2005-07-20 2010-04-06 United Technologies Corporation Inner diameter variable vane actuation mechanism
DE102005047942A1 (en) * 2005-10-06 2007-04-12 Daimlerchrysler Ag Supercharger for internal-combustion engine, has guiding device with adjustable and flexible ductile guidance element for guidance of flow
EP1867877A1 (en) * 2006-06-16 2007-12-19 Ansaldo Energia S.P.A. Gas turbine compressor
DE102007012119A1 (en) 2007-03-13 2008-09-18 Rolls-Royce Deutschland Ltd & Co Kg Throttling degree dependent blade adjustment in turbomachines
GB2448734A (en) * 2007-04-26 2008-10-29 Rolls Royce Plc Controlling operation of a compressor to avoid surge, stall or flutter
US20100260591A1 (en) * 2007-06-08 2010-10-14 General Electric Company Spanwise split variable guide vane and related method
US8348600B2 (en) * 2008-05-27 2013-01-08 United Technologies Corporation Gas turbine engine having controllable inlet guide vanes
GB0813413D0 (en) 2008-07-23 2008-08-27 Rolls Royce Plc A compressor variable stator vane arrangement
CH699395A1 (en) * 2008-08-21 2010-02-26 Alstom Technology Ltd Gas turbine and method of operation.
US8099944B2 (en) * 2008-10-08 2012-01-24 The Invention Science Fund I, Llc Hybrid propulsive engine including at least one independently rotatable propeller/fan
DE102009009715A1 (en) * 2009-02-19 2010-08-26 Mtu Aero Engines Gmbh Compressor with guide grille with radially variable outflow
GB0907461D0 (en) * 2009-05-01 2009-06-10 Rolls Royce Plc Control mechanism
US8516829B2 (en) * 2009-05-27 2013-08-27 General Electric Company Systems and methods for modifying the performance of a gas turbine
GB0919771D0 (en) * 2009-11-12 2009-12-30 Rolls Royce Plc Gas compression
FR2952979B1 (en) * 2009-11-20 2012-01-20 Snecma TURBOMACHINE COMPRISING A STATOR BLADE OF STATOR WITH VARIABLE SETTING AND INDEPENDENT CONTROL.
US8770912B2 (en) * 2010-04-28 2014-07-08 General Electric Company Systems, methods, and apparatus for controlling turbine guide vane positions
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
US9068470B2 (en) * 2011-04-21 2015-06-30 General Electric Company Independently-controlled gas turbine inlet guide vanes and variable stator vanes
GB201110116D0 (en) * 2011-06-16 2011-07-27 Rolls Royce Plc Surge margin control
US9297313B2 (en) * 2011-09-13 2016-03-29 General Electric Company Control apparatus for angling guide vanes of a torque converter

Also Published As

Publication number Publication date
EP2508762A3 (en) 2018-04-11
CN102734196A (en) 2012-10-17
US8909454B2 (en) 2014-12-09
US20120259528A1 (en) 2012-10-11
EP2508762A2 (en) 2012-10-10
EP2508762B1 (en) 2019-06-12
CN102734196B (en) 2016-08-24

Similar Documents

Publication Publication Date Title
BR122020015315A2 (en)
BR112013022641A2 (en)
AP3853A (en)
BR112013031251A2 (en)
BR112013027245A2 (en)
BR112013024383A2 (en)
BR112013026905A2 (en)
BR112013023185A2 (en)
BR112013022995A2 (en)
BR112013017670A2 (en)
BR112013026744A2 (en)
BR112013023927A2 (en)
BR112013027830A2 (en)
BR112013024365A2 (en)
BR112013027121A2 (en)
BR112013027452A2 (en)
AP2016009466A0 (en)
BR112013031556A2 (en)
BR112013026790A2 (en)
BR112013024588A2 (en)
IN2012DE00979A (en)
BR112013018949A2 (en)
BR112013026895A2 (en)
BR112013027761A2 (en)
BR112013021637A2 (en)