CN101892874B - 可变位置导向叶片致动系统和方法 - Google Patents

可变位置导向叶片致动系统和方法 Download PDF

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Publication number
CN101892874B
CN101892874B CN201010003821.2A CN201010003821A CN101892874B CN 101892874 B CN101892874 B CN 101892874B CN 201010003821 A CN201010003821 A CN 201010003821A CN 101892874 B CN101892874 B CN 101892874B
Authority
CN
China
Prior art keywords
variable position
position guide
turbine
guide vane
actuation system
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.)
Expired - Fee Related
Application number
CN201010003821.2A
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English (en)
Chinese (zh)
Other versions
CN101892874A (zh
Inventor
S·巴特纳加
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of CN101892874A publication Critical patent/CN101892874A/zh
Application granted granted Critical
Publication of CN101892874B publication Critical patent/CN101892874B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CN201010003821.2A 2009-01-06 2010-01-06 可变位置导向叶片致动系统和方法 Expired - Fee Related CN101892874B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/349,160 2009-01-06
US12/349,160 US8297918B2 (en) 2009-01-06 2009-01-06 Variable position guide vane actuation system and method

Publications (2)

Publication Number Publication Date
CN101892874A CN101892874A (zh) 2010-11-24
CN101892874B true CN101892874B (zh) 2015-03-11

Family

ID=41693028

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201010003821.2A Expired - Fee Related CN101892874B (zh) 2009-01-06 2010-01-06 可变位置导向叶片致动系统和方法

Country Status (4)

Country Link
US (1) US8297918B2 (https=)
EP (1) EP2204549B1 (https=)
JP (1) JP5599618B2 (https=)
CN (1) CN101892874B (https=)

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US8348600B2 (en) * 2008-05-27 2013-01-08 United Technologies Corporation Gas turbine engine having controllable inlet guide vanes
US8727697B2 (en) * 2010-03-27 2014-05-20 Rolls-Royce Corporation Variable vane actuation system and method
IT1401665B1 (it) * 2010-08-31 2013-08-02 Nuova Pignone S R L Sistema di azionamento per turbomacchina e metodo.
US8915703B2 (en) * 2011-07-28 2014-12-23 United Technologies Corporation Internally actuated inlet guide vane for fan section
US9394804B2 (en) 2012-01-24 2016-07-19 Florida Institute Of Technology Apparatus and method for rotating fluid controlling vanes in small turbine engines and other applications
US10030587B2 (en) * 2013-04-08 2018-07-24 United Technologies Corporation Annular airflow actuation system for variable cycle gas turbine engines
WO2014205816A1 (en) * 2013-06-28 2014-12-31 Siemens Aktiengesellschaft Guide vane actuator of a compressor and a compressor using it
FR3015594B1 (fr) * 2013-12-19 2018-04-06 Safran Aircraft Engines Compresseur de turbomachine, en particulier de turbopropulseur ou de turboreacteur d'avion
US9932851B2 (en) 2013-12-30 2018-04-03 Rolls-Royce North American Technologies, Inc. Active synchronizing ring
DE102014001034B4 (de) 2014-01-25 2020-01-02 MTU Aero Engines AG Strömungsmaschine
JP6194553B2 (ja) * 2014-01-27 2017-09-13 三菱日立パワーシステムズ株式会社 位置調節装置、これを備えている回転機械、及び位置調節方法
US9422859B2 (en) * 2014-03-05 2016-08-23 GM Global Technology Operations LLC Adaptable turbocharger control
FR3038666B1 (fr) * 2015-07-09 2017-07-07 Snecma Anneau de commande d'aubes a calage variable pour une turbomachine
US11073090B2 (en) * 2016-03-30 2021-07-27 General Electric Company Valved airflow passage assembly for adjusting airflow distortion in gas turbine engine
US10794219B2 (en) * 2017-09-14 2020-10-06 Rolls-Royce Corporation Axial case ring to maximize thrust bushing contact area of variable vane
GB201717091D0 (en) * 2017-10-18 2017-11-29 Rolls Royce Plc A variable vane actuation arrangement
DE102017222209A1 (de) * 2017-12-07 2019-06-13 MTU Aero Engines AG Leitschaufelanbindung sowie Strömungsmaschine
US10815802B2 (en) * 2018-12-17 2020-10-27 Raytheon Technologies Corporation Variable vane assemblies configured for non-axisymmetric actuation
US11002142B2 (en) * 2019-01-21 2021-05-11 Raytheon Technologies Corporation Thermally compensated synchronization ring of a variable stator vane assembly
US11560810B1 (en) 2021-07-20 2023-01-24 Rolls-Royce North American Technologies Inc. Variable vane actuation system and method for gas turbine engine performance management
US12270309B2 (en) 2022-10-21 2025-04-08 Rolls-Royce North American Technologies Inc. Variable stator vane assembly with magnetic actuation rotor for gas turbine engines
US12146414B2 (en) 2022-10-21 2024-11-19 Rolls-Royce North American Technologies Inc. Stator vane control system with magnetic actuation rotor for gas turbine engines
US11982193B1 (en) 2022-12-30 2024-05-14 Rolls-Royce North American Technologies Inc. Systems and methods for multi-dimensional variable vane stage rigging utilizing adjustable inclined mechanisms
US12000292B1 (en) 2022-12-30 2024-06-04 Rolls-Royce North American Technologies Inc. Systems and methods for multi-dimensional variable vane stage rigging
US12000293B1 (en) 2022-12-30 2024-06-04 Rolls-Royce North American Technologies Inc. Systems and methods for multi-dimensional variable vane stage rigging utilizing coupling mechanisms
US11834966B1 (en) 2022-12-30 2023-12-05 Rolls-Royce North American Technologies Inc. Systems and methods for multi-dimensional variable vane stage rigging utilizing adjustable alignment mechanisms
US12146415B2 (en) 2022-12-30 2024-11-19 Rolls-Royce North American Technologies Inc. Systems and methods for multi-dimensional variable vane stage rigging utilizing adjustable bracket plates

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3508839A (en) * 1968-01-15 1970-04-28 Sulzer Ag Plural-stage axial compressor
US4978280A (en) * 1987-09-26 1990-12-18 Rolls-Royce Plc Variable guide vane arrangement for a compressor
GB2264148B (en) * 1992-02-13 1995-02-08 Rolls Royce Plc Variable camber stator vane
US6106227A (en) * 1998-02-27 2000-08-22 United Technologies Corporation Roller assembly for guiding an actuating ring

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH404841A (de) * 1963-09-27 1965-12-31 Bbc Brown Boveri & Cie Turbomaschinen mit verstellbaren Schaufeln
US3861822A (en) * 1974-02-27 1975-01-21 Gen Electric Duct with vanes having selectively variable pitch
JPS5859400A (ja) 1981-10-02 1983-04-08 Hitachi Ltd 多段軸流圧縮機の静翼取付角度可変装置
CH661772A5 (de) * 1983-05-31 1987-08-14 Escher Wyss Ag Axiale turbomaschine.
JP4008404B2 (ja) * 2002-10-18 2007-11-14 三菱重工業株式会社 可変容量型排気ターボ過給機
US8435000B2 (en) * 2008-03-07 2013-05-07 Rolls-Royce Corporation Variable vane actuation system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3508839A (en) * 1968-01-15 1970-04-28 Sulzer Ag Plural-stage axial compressor
US4978280A (en) * 1987-09-26 1990-12-18 Rolls-Royce Plc Variable guide vane arrangement for a compressor
GB2264148B (en) * 1992-02-13 1995-02-08 Rolls Royce Plc Variable camber stator vane
US6106227A (en) * 1998-02-27 2000-08-22 United Technologies Corporation Roller assembly for guiding an actuating ring

Also Published As

Publication number Publication date
JP5599618B2 (ja) 2014-10-01
US20100172744A1 (en) 2010-07-08
EP2204549A3 (en) 2011-01-26
US8297918B2 (en) 2012-10-30
CN101892874A (zh) 2010-11-24
JP2010159749A (ja) 2010-07-22
EP2204549B1 (en) 2015-10-28
EP2204549A2 (en) 2010-07-07

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Granted publication date: 20150311

Termination date: 20180106