CN103133145B - 减少燃气涡轮发动机的停工时间的方法 - Google Patents

减少燃气涡轮发动机的停工时间的方法 Download PDF

Info

Publication number
CN103133145B
CN103133145B CN201210481215.0A CN201210481215A CN103133145B CN 103133145 B CN103133145 B CN 103133145B CN 201210481215 A CN201210481215 A CN 201210481215A CN 103133145 B CN103133145 B CN 103133145B
Authority
CN
China
Prior art keywords
rotor
housing
electromotor
turbine
entrance
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.)
Active
Application number
CN201210481215.0A
Other languages
English (en)
Chinese (zh)
Other versions
CN103133145A (zh
Inventor
S.舍鲁尼
J.E.阿特曼
M.布兰德斯
M.A.阿里
A.萨米姆
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 CN103133145A publication Critical patent/CN103133145A/zh
Application granted granted Critical
Publication of CN103133145B publication Critical patent/CN103133145B/zh
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/34—Turning or inching gear
    • 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
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
CN201210481215.0A 2011-11-23 2012-11-23 减少燃气涡轮发动机的停工时间的方法 Active CN103133145B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/303,338 2011-11-23
US13/303338 2011-11-23
US13/303,338 US8776530B2 (en) 2011-11-23 2011-11-23 Gas turbine engine lockout reduction

Publications (2)

Publication Number Publication Date
CN103133145A CN103133145A (zh) 2013-06-05
CN103133145B true CN103133145B (zh) 2016-08-31

Family

ID=47290663

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210481215.0A Active CN103133145B (zh) 2011-11-23 2012-11-23 减少燃气涡轮发动机的停工时间的方法

Country Status (5)

Country Link
US (1) US8776530B2 (enExample)
EP (1) EP2597274B1 (enExample)
JP (1) JP6012424B2 (enExample)
CN (1) CN103133145B (enExample)
CA (1) CA2794802C (enExample)

Families Citing this family (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013141937A1 (en) * 2011-12-30 2013-09-26 Rolls-Royce North American Technologies, Inc. Gas turbine engine tip clearance control
DE102014203318A1 (de) * 2014-02-25 2015-08-27 Siemens Aktiengesellschaft Verfahren zum Betrieb einer Gasturbine bei aktiver hydraulischer Spalteinstellung
US9708980B2 (en) * 2014-06-05 2017-07-18 General Electric Company Apparatus and system for compressor clearance control
JP6548989B2 (ja) * 2014-08-28 2019-07-24 ゼネラル・エレクトリック・カンパニイ 複合サイクル発電所熱エネルギー保存
US10502139B2 (en) 2015-01-28 2019-12-10 General Electric Company Method of starting a gas turbine engine including a cooling phase
GB201507818D0 (en) * 2015-05-07 2015-06-17 Rolls Royce Plc A gas turbine engine
US20160326915A1 (en) * 2015-05-08 2016-11-10 General Electric Company System and method for waste heat powered active clearance control
US11149642B2 (en) 2015-12-30 2021-10-19 General Electric Company System and method of reducing post-shutdown engine temperatures
US10539079B2 (en) 2016-02-12 2020-01-21 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
US10174678B2 (en) 2016-02-12 2019-01-08 United Technologies Corporation Bowed rotor start using direct temperature measurement
US10508601B2 (en) 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine
US10040577B2 (en) 2016-02-12 2018-08-07 United Technologies Corporation Modified start sequence of a gas turbine engine
US10436064B2 (en) 2016-02-12 2019-10-08 United Technologies Corporation Bowed rotor start response damping system
US10125636B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor prevention system using waste heat
US10443507B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Gas turbine engine bowed rotor avoidance system
US10508567B2 (en) 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory
US10125691B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor start using a variable position starter valve
US9664070B1 (en) 2016-02-12 2017-05-30 United Technologies Corporation Bowed rotor prevention system
US10443505B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine
EP3211184B1 (en) 2016-02-29 2021-05-05 Raytheon Technologies Corporation Bowed rotor prevention system and associated method of bowed rotor prevention
US10337405B2 (en) 2016-05-17 2019-07-02 General Electric Company Method and system for bowed rotor start mitigation using rotor cooling
US10563590B2 (en) 2016-05-19 2020-02-18 Hamilton Sundstrand Corporation System and method of gas turbine engine shaft cooling
US10787933B2 (en) 2016-06-20 2020-09-29 Raytheon Technologies Corporation Low-power bowed rotor prevention and monitoring system
US10358936B2 (en) * 2016-07-05 2019-07-23 United Technologies Corporation Bowed rotor sensor system
US10618666B2 (en) 2016-07-21 2020-04-14 United Technologies Corporation Pre-start motoring synchronization for multiple engines
US10384791B2 (en) 2016-07-21 2019-08-20 United Technologies Corporation Cross engine coordination during gas turbine engine motoring
US10221774B2 (en) 2016-07-21 2019-03-05 United Technologies Corporation Speed control during motoring of a gas turbine engine
EP3273016B1 (en) 2016-07-21 2020-04-01 United Technologies Corporation Multi-engine coordination during gas turbine engine motoring
EP3273006B1 (en) 2016-07-21 2019-07-03 United Technologies Corporation Alternating starter use during multi-engine motoring
US10823199B2 (en) 2016-08-12 2020-11-03 General Electric Company Galvanic corrosion resistant coating composition and methods for forming the same
US10787968B2 (en) 2016-09-30 2020-09-29 Raytheon Technologies Corporation Gas turbine engine motoring with starter air valve manual override
US10583933B2 (en) 2016-10-03 2020-03-10 General Electric Company Method and apparatus for undercowl flow diversion cooling
US10443543B2 (en) 2016-11-04 2019-10-15 United Technologies Corporation High compressor build clearance reduction
US10823079B2 (en) 2016-11-29 2020-11-03 Raytheon Technologies Corporation Metered orifice for motoring of a gas turbine engine
US10669945B2 (en) 2017-02-06 2020-06-02 Raytheon Technologies Corporation Starter air valve system with dual electromechanical controls
US10801359B2 (en) 2017-03-14 2020-10-13 General Electric Company Method and system for identifying rub events
US10711693B2 (en) 2017-07-12 2020-07-14 General Electric Company Gas turbine engine with an engine rotor element turning device
US10947993B2 (en) 2017-11-27 2021-03-16 General Electric Company Thermal gradient attenuation structure to mitigate rotor bow in turbine engine
US11549392B2 (en) * 2017-12-14 2023-01-10 General Electric Company Structure and method to mitigate rotor bow in turbine engine
US10760498B2 (en) 2018-01-04 2020-09-01 General Electric Company System and method for removing rotor bow in a gas turbine engine using mechanical energy storage device
GB2571992A (en) * 2018-03-16 2019-09-18 Rolls Royce Plc Gas turbine engine and method of maintaining a gas turbine engine
US10760444B2 (en) 2018-05-14 2020-09-01 Raytheon Technologies Corporation Electric heating for turbomachinery clearance control powered by hybrid energy storage system
US11111809B2 (en) 2018-05-14 2021-09-07 Raytheon Technologies Corporation Electric heating for turbomachinery clearance control
US11525370B2 (en) 2020-11-13 2022-12-13 General Electric Company Method and system for mitigating rotor bow in a turbo machine
US12060833B2 (en) * 2021-08-10 2024-08-13 Rolls-Royce North American Technologies, Inc. Gas turbine engine system with motor-generator
CN116085067A (zh) 2021-11-05 2023-05-09 通用电气公司 具有流体导管系统的燃气涡轮发动机及其操作方法
US11859500B2 (en) * 2021-11-05 2024-01-02 General Electric Company Gas turbine engine with a fluid conduit system and a method of operating the same
US12140089B2 (en) 2021-12-27 2024-11-12 Rolls-Royce North American Technologies, Inc. Gas turbine engine system with generator
US12320295B2 (en) 2021-12-27 2025-06-03 Rolls-Royce North American Technologies, Inc. Gas turbine engine system with generator
US11879411B2 (en) 2022-04-07 2024-01-23 General Electric Company System and method for mitigating bowed rotor in a gas turbine engine
US20240410314A1 (en) * 2023-06-08 2024-12-12 Raytheon Technologies Corporation Water active turbine clearance control

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2684568A (en) * 1950-02-04 1954-07-27 Senger Ulrich Apparatus for ascertaining and regulating deformation of the housing and rotor elements of an elastic fluid turbomachine
US4003200A (en) * 1972-11-14 1977-01-18 Brown Boveri-Sulzer Turbomachinery, Ltd. Method and apparatus for cooling turbomachines
US4482293A (en) * 1981-03-20 1984-11-13 Rolls-Royce Limited Casing support for a gas turbine engine
CN85101816A (zh) * 1985-04-01 1987-01-10 联合工艺公司 有效间隙控制装置

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2117842A (en) 1982-03-25 1983-10-19 Rolls Royce Means for equalising the temperatures within a gas turbine engine
US6626635B1 (en) * 1998-09-30 2003-09-30 General Electric Company System for controlling clearance between blade tips and a surrounding casing in rotating machinery
KR101346566B1 (ko) * 2008-10-08 2014-01-02 미츠비시 쥬고교 가부시키가이샤 가스 터빈 및 그 운전 방법
US8210801B2 (en) * 2009-01-29 2012-07-03 General Electric Company Systems and methods of reducing heat loss from a gas turbine during shutdown

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2684568A (en) * 1950-02-04 1954-07-27 Senger Ulrich Apparatus for ascertaining and regulating deformation of the housing and rotor elements of an elastic fluid turbomachine
US4003200A (en) * 1972-11-14 1977-01-18 Brown Boveri-Sulzer Turbomachinery, Ltd. Method and apparatus for cooling turbomachines
US4482293A (en) * 1981-03-20 1984-11-13 Rolls-Royce Limited Casing support for a gas turbine engine
CN85101816A (zh) * 1985-04-01 1987-01-10 联合工艺公司 有效间隙控制装置

Also Published As

Publication number Publication date
CN103133145A (zh) 2013-06-05
CA2794802A1 (en) 2013-05-23
EP2597274A2 (en) 2013-05-29
EP2597274B1 (en) 2019-01-09
CA2794802C (en) 2019-10-08
US8776530B2 (en) 2014-07-15
JP6012424B2 (ja) 2016-10-25
US20130125552A1 (en) 2013-05-23
JP2013108495A (ja) 2013-06-06
EP2597274A3 (en) 2017-06-07

Similar Documents

Publication Publication Date Title
CN103133145B (zh) 减少燃气涡轮发动机的停工时间的方法
JP5613393B2 (ja) ガスタービンの冷却装置及び方法
EP2587028B1 (en) Active clearance control system and method for a gas turbine engine
EP2708720B1 (en) Gas turbine and operating method thereof
US7798767B2 (en) Casing and gas turbine
US10619564B2 (en) Gas turbine and component-temperature adjustment method therefor
US9151182B2 (en) System and method for removing heat from a turbomachine
CN105579688B (zh) 燃气涡轮机、燃气涡轮机的控制装置和燃气涡轮机的运转方法
CN104769222A (zh) 位于燃气轮机发动机中的外部冷却流体喷射系统
JP3949014B2 (ja) ガスタービン装置
JP2016508569A (ja) ガスタービンエンジンのため熱保持及び熱分散システム
WO2014074368A1 (en) Air injection system for cooling a rotor in a gas turbine engine and method of cooling such rotor
EP3058182B1 (en) Sealing clearance control in turbomachines
JP2013160235A (ja) タービンの部分負荷特性を制御する方法および装置
KR101833657B1 (ko) 가스터빈의 운전방법 및 운전제어장치
CN105386876A (zh) 联合循环发电设备
CN205744015U (zh) 蒸汽涡轮温暖保持设备

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant