SA515360558B1 - نظام للتحكم في درجة حرارة حامل ريشة في محرك تربين يعمل بالغاز - Google Patents

نظام للتحكم في درجة حرارة حامل ريشة في محرك تربين يعمل بالغاز

Info

Publication number
SA515360558B1
SA515360558B1 SA515360558A SA515360558A SA515360558B1 SA 515360558 B1 SA515360558 B1 SA 515360558B1 SA 515360558 A SA515360558 A SA 515360558A SA 515360558 A SA515360558 A SA 515360558A SA 515360558 B1 SA515360558 B1 SA 515360558B1
Authority
SA
Saudi Arabia
Prior art keywords
vane carrier
control system
section
cooling air
temperature control
Prior art date
Application number
SA515360558A
Other languages
English (en)
Inventor
كوك – مون ثام
فينسينت بى لاوريلو
Original Assignee
سيمينس اكتنجسلشافت.
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 سيمينس اكتنجسلشافت. filed Critical سيمينس اكتنجسلشافت.
Publication of SA515360558B1 publication Critical patent/SA515360558B1/ar

Links

Classifications

    • 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
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • 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
    • F02C7/00Features, 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
    • F02C7/12Cooling of plants
    • F02C7/16Cooling of plants characterised by cooling medium
    • F02C7/18Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F02C7/00Features, 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
    • F02C7/12Cooling of plants
    • F02C7/16Cooling of plants characterised by cooling medium
    • F02C7/18Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F02C7/185Cooling means for reducing the temperature of the cooling air or gas

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

يتضمن نظام تحكم في درجة حرارة حامل ريشة ‏vane carrier temperature control ‎system‏ يستخدم في محرك تربين يعمل بالغاز ‏gas turbine engine‏ مصدر هواء تبريد ‏cooling air source‏ أول, مصدر هواء تبريد ثاني, ونظام تحكم في درجة حرارة الهواء ‏air ‎temperature control system‏. يقوم مصدر هواء التبريد الأول بإمداد جزء أول من هواء ‏تبريد حامل ريشة تم استخراجه من قطاع ضاغط ‏compressor‏ للمحرك ‏engine‏ إلى قطاع أول ‏لحامل ريشة ‏vane carrier‏ يحمل عديد من صفوف أرياش داخل قطاع تربين للمحرك. يقوم ‏مصدر هواء التبريد الثاني بإمداد جزء ثاني من هواء تبريد حامل ريشة مستخرج من قطاع الضاغط ‏إلى قطاع ثاني لحامل الريشة المباعد عن القطاع الأول في اتجاه محوري محدد باتجاه تدفق غاز ‏التشغيل الساخن ‏hot working gas flow‏ من خلال قطاع التربين. يقوم نظام التحكم في درجة ‏حرارة الهواء بالتحكم في درجة حرارة واحد على الأقل من أجزاء هواء تبريد حامل الريشة الأولى ‏والثانية.‏ شكل 1‏
SA515360558A 2012-12-19 2015-06-10 نظام للتحكم في درجة حرارة حامل ريشة في محرك تربين يعمل بالغاز SA515360558B1 (ar)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/719,269 US9562475B2 (en) 2012-12-19 2012-12-19 Vane carrier temperature control system in a gas turbine engine
PCT/US2013/076099 WO2014100164A1 (en) 2012-12-19 2013-12-18 Vane carrier temperature control system in a gas turbine engine

Publications (1)

Publication Number Publication Date
SA515360558B1 true SA515360558B1 (ar) 2018-09-24

Family

ID=49917293

Family Applications (1)

Application Number Title Priority Date Filing Date
SA515360558A SA515360558B1 (ar) 2012-12-19 2015-06-10 نظام للتحكم في درجة حرارة حامل ريشة في محرك تربين يعمل بالغاز

Country Status (7)

Country Link
US (1) US9562475B2 (ar)
EP (1) EP2935831A1 (ar)
JP (1) JP6165879B2 (ar)
CN (1) CN104884767B (ar)
RU (1) RU2626923C2 (ar)
SA (1) SA515360558B1 (ar)
WO (1) WO2014100164A1 (ar)

Families Citing this family (43)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2896793A1 (en) * 2014-01-21 2015-07-22 Alstom Technology Ltd Method of operating a gas turbine assembly and the gas turbine assembly
WO2015178897A1 (en) * 2014-05-21 2015-11-26 Siemens Energy, Inc. Ejector based external bleed system for a gas turbine engine
JP6368611B2 (ja) * 2014-10-03 2018-08-01 三菱日立パワーシステムズ株式会社 ガスタービン、コンバインドサイクルプラント、ガスタービンの起動方法
US10767562B2 (en) * 2014-12-10 2020-09-08 Pratt & Whitney Canada Corp. Modulated cooled P3 air for impeller
US10371055B2 (en) 2015-02-12 2019-08-06 United Technologies Corporation Intercooled cooling air using cooling compressor as starter
US11808210B2 (en) 2015-02-12 2023-11-07 Rtx Corporation Intercooled cooling air with heat exchanger packaging
US10731560B2 (en) 2015-02-12 2020-08-04 Raytheon Technologies Corporation Intercooled cooling air
US9797310B2 (en) * 2015-04-02 2017-10-24 General Electric Company Heat pipe temperature management system for a turbomachine
US10480419B2 (en) 2015-04-24 2019-11-19 United Technologies Corporation Intercooled cooling air with plural heat exchangers
US10221862B2 (en) 2015-04-24 2019-03-05 United Technologies Corporation Intercooled cooling air tapped from plural locations
US10830148B2 (en) 2015-04-24 2020-11-10 Raytheon Technologies Corporation Intercooled cooling air with dual pass heat exchanger
US10100739B2 (en) 2015-05-18 2018-10-16 United Technologies Corporation Cooled cooling air system for a gas turbine engine
US10794288B2 (en) 2015-07-07 2020-10-06 Raytheon Technologies Corporation Cooled cooling air system for a turbofan engine
KR101790146B1 (ko) 2015-07-14 2017-10-25 두산중공업 주식회사 외부 케이싱으로 우회하는 냉각공기 공급유로가 마련된 냉각시스템을 포함하는 가스터빈.
EP3168431A1 (en) * 2015-11-13 2017-05-17 General Electric Technology GmbH Heat exchangers and cooling methods for gas turbines
US10371056B2 (en) * 2015-12-10 2019-08-06 United Technologies Corporation Multi-source turbine cooling air
US10443508B2 (en) 2015-12-14 2019-10-15 United Technologies Corporation Intercooled cooling air with auxiliary compressor control
KR102052029B1 (ko) * 2016-03-01 2019-12-04 지멘스 악티엔게젤샤프트 가스 터빈 엔진에서 압축기 어셈블리로부터 하류에 있는 미드-프레임 토크 디스크들을 위한 압축기 블리드 냉각 시스템
US10196928B2 (en) * 2016-03-02 2019-02-05 General Electric Company Method and system for piping failure detection in a gas turbine bleeding air system
US10669940B2 (en) 2016-09-19 2020-06-02 Raytheon Technologies Corporation Gas turbine engine with intercooled cooling air and turbine drive
US11073085B2 (en) * 2016-11-08 2021-07-27 Raytheon Technologies Corporation Intercooled cooling air heat exchanger arrangement
US10550768B2 (en) 2016-11-08 2020-02-04 United Technologies Corporation Intercooled cooled cooling integrated air cycle machine
US10794290B2 (en) 2016-11-08 2020-10-06 Raytheon Technologies Corporation Intercooled cooled cooling integrated air cycle machine
US20180128187A1 (en) * 2016-11-08 2018-05-10 United Technologies Corporation Cooled cooling air safety through a temperature-monitoring line replaceable unit
JP6799455B2 (ja) * 2016-12-16 2020-12-16 川崎重工業株式会社 ガスタービンエンジン
US10961911B2 (en) 2017-01-17 2021-03-30 Raytheon Technologies Corporation Injection cooled cooling air system for a gas turbine engine
US10995673B2 (en) 2017-01-19 2021-05-04 Raytheon Technologies Corporation Gas turbine engine with intercooled cooling air and dual towershaft accessory gearbox
EP3379036A1 (en) * 2017-03-22 2018-09-26 Ansaldo Energia Switzerland AG Gas turbine engine and method for cooling said gas turbine engine
CN106801646A (zh) * 2017-03-23 2017-06-06 重庆大学 一种新型燃气轮机及提高燃气透平进口温度的方法
US10577964B2 (en) 2017-03-31 2020-03-03 United Technologies Corporation Cooled cooling air for blade air seal through outer chamber
US10711640B2 (en) 2017-04-11 2020-07-14 Raytheon Technologies Corporation Cooled cooling air to blade outer air seal passing through a static vane
US10934943B2 (en) 2017-04-27 2021-03-02 General Electric Company Compressor apparatus with bleed slot and supplemental flange
US10641121B2 (en) * 2017-07-24 2020-05-05 Rolls-Royce North American Technologies Inc. Gas turbine engine with rotor tip clearance control system
DE102017216119A1 (de) * 2017-09-13 2019-03-14 MTU Aero Engines AG Gasturbinenverdichtergehäuse
US10738703B2 (en) 2018-03-22 2020-08-11 Raytheon Technologies Corporation Intercooled cooling air with combined features
KR102067103B1 (ko) * 2018-04-05 2020-01-16 두산중공업 주식회사 터빈의 온도 추정 시스템
US10830145B2 (en) 2018-04-19 2020-11-10 Raytheon Technologies Corporation Intercooled cooling air fleet management system
US10808619B2 (en) 2018-04-19 2020-10-20 Raytheon Technologies Corporation Intercooled cooling air with advanced cooling system
RU2680636C1 (ru) * 2018-05-14 2019-02-25 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Система охлаждения многоконтурной газотурбинной установки
US10718233B2 (en) 2018-06-19 2020-07-21 Raytheon Technologies Corporation Intercooled cooling air with low temperature bearing compartment air
US11530650B2 (en) * 2018-07-13 2022-12-20 Raytheon Technologies Corporation Gas turbine engine with active variable turbine cooling
US11255268B2 (en) 2018-07-31 2022-02-22 Raytheon Technologies Corporation Intercooled cooling air with selective pressure dump
US11732656B2 (en) * 2021-03-31 2023-08-22 Raytheon Technologies Corporation Turbine engine with soaring air conduit

Family Cites Families (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3528250A (en) 1969-04-16 1970-09-15 Gen Motors Corp Bypass engine with afterburning and compressor bleed air heat exchanger in bypass duct
US4137705A (en) 1977-07-25 1979-02-06 General Electric Company Cooling air cooler for a gas turbine engine
US4254618A (en) 1977-08-18 1981-03-10 General Electric Company Cooling air cooler for a gas turbofan engine
JPS62182444A (ja) * 1986-02-07 1987-08-10 Hitachi Ltd ガスタ−ビン冷却空気制御方法及び装置
US5134844A (en) * 1990-07-30 1992-08-04 General Electric Company Aft entry cooling system and method for an aircraft engine
US5392614A (en) 1992-03-23 1995-02-28 General Electric Company Gas turbine engine cooling system
US5317877A (en) 1992-08-03 1994-06-07 General Electric Company Intercooled turbine blade cooling air feed system
FR2708669B1 (fr) 1993-08-05 1995-09-08 Snecma Système de ventilation des disques et du stator de turbine d'un turboréacteur.
RU2107168C1 (ru) 1995-07-12 1998-03-20 Акционерное общество открытого типа "Ленинградский Металлический завод" Система концевых уплотнений паротурбинной установки
US5581996A (en) 1995-08-16 1996-12-10 General Electric Company Method and apparatus for turbine cooling
JP2941748B2 (ja) 1997-07-15 1999-08-30 三菱重工業株式会社 ガスタービン冷却装置
US6615574B1 (en) * 2000-01-14 2003-09-09 General Electric Co. System for combining flow from compressor bleeds of an industrial gas turbine for gas turbine performance optimization
US6487863B1 (en) 2001-03-30 2002-12-03 Siemens Westinghouse Power Corporation Method and apparatus for cooling high temperature components in a gas turbine
US6550253B2 (en) 2001-09-12 2003-04-22 General Electric Company Apparatus and methods for controlling flow in turbomachinery
US6968696B2 (en) 2003-09-04 2005-11-29 Siemens Westinghouse Power Corporation Part load blade tip clearance control
US7269955B2 (en) 2004-08-25 2007-09-18 General Electric Company Methods and apparatus for maintaining rotor assembly tip clearances
DE102006010863B4 (de) * 2005-03-24 2016-12-22 General Electric Technology Gmbh Turbomaschine, insbesondere Verdichter
JP4523876B2 (ja) 2005-06-10 2010-08-11 三菱重工業株式会社 ガスタービン及び空気供給制御方法、並びに空気供給制御用コンピュータプログラム
US7708518B2 (en) * 2005-06-23 2010-05-04 Siemens Energy, Inc. Turbine blade tip clearance control
US7303372B2 (en) 2005-11-18 2007-12-04 General Electric Company Methods and apparatus for cooling combustion turbine engine components
US8495883B2 (en) * 2007-04-05 2013-07-30 Siemens Energy, Inc. Cooling of turbine components using combustor shell air
US8015826B2 (en) * 2007-04-05 2011-09-13 Siemens Energy, Inc. Engine brake for part load CO reduction
US8056345B2 (en) * 2007-06-13 2011-11-15 United Technologies Corporation Hybrid cooling of a gas turbine engine
US8033116B2 (en) * 2008-05-06 2011-10-11 General Electric Company Turbomachine and a method for enhancing power efficiency in a turbomachine
US8240153B2 (en) * 2008-05-14 2012-08-14 General Electric Company Method and system for controlling a set point for extracting air from a compressor to provide turbine cooling air in a gas turbine
JP5297114B2 (ja) * 2008-08-06 2013-09-25 三菱重工業株式会社 ガスタービン
WO2010084573A1 (ja) 2009-01-20 2010-07-29 三菱重工業株式会社 ガスタービン設備
US20110016870A1 (en) * 2009-07-23 2011-01-27 Yefim Kashler Method and apparatus for improved gas turbine efficiency and augmented power output
US20110271689A1 (en) * 2010-05-06 2011-11-10 General Electric Company Gas turbine cooling
CH705181A1 (de) * 2011-06-16 2012-12-31 Alstom Technology Ltd Verfahren zum Kühlen einer Gasturbinenanlage sowie Gasturbinenanlage zur Durchführung des Verfahrens.
US20130283814A1 (en) * 2012-04-25 2013-10-31 General Electric Company Turbine cooling system
US9261022B2 (en) * 2012-12-07 2016-02-16 General Electric Company System for controlling a cooling flow from a compressor section of a gas turbine

Also Published As

Publication number Publication date
JP6165879B2 (ja) 2017-07-19
RU2015129105A (ru) 2017-01-25
EP2935831A1 (en) 2015-10-28
WO2014100164A1 (en) 2014-06-26
JP2016503855A (ja) 2016-02-08
CN104884767B (zh) 2018-03-23
US9562475B2 (en) 2017-02-07
US20140311157A1 (en) 2014-10-23
CN104884767A (zh) 2015-09-02
RU2626923C2 (ru) 2017-08-02

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