SA515360105B1 - طريقة لتشغيل محرك توربيني غازي يتضمن نظام إعادة تدوير هواء غلاف وحدة احتراق - Google Patents

طريقة لتشغيل محرك توربيني غازي يتضمن نظام إعادة تدوير هواء غلاف وحدة احتراق

Info

Publication number
SA515360105B1
SA515360105B1 SA515360105A SA515360105A SA515360105B1 SA 515360105 B1 SA515360105 B1 SA 515360105B1 SA 515360105 A SA515360105 A SA 515360105A SA 515360105 A SA515360105 A SA 515360105A SA 515360105 B1 SA515360105 B1 SA 515360105B1
Authority
SA
Saudi Arabia
Prior art keywords
air
recirculation system
air recirculation
gas turbine
shell air
Prior art date
Application number
SA515360105A
Other languages
Arabic (ar)
English (en)
Inventor
سي. لاندروم ايفان
زهانج جيبينج
لي شينج-بانج
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 SA515360105B1 publication Critical patent/SA515360105B1/ar

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
    • 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
    • F01D25/14—Casings modified therefor
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-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
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • 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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26—Double casings; Measures against temperature strain in casings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Exhaust-Gas Circulating Devices (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
SA515360105A 2012-09-05 2015-03-03 طريقة لتشغيل محرك توربيني غازي يتضمن نظام إعادة تدوير هواء غلاف وحدة احتراق SA515360105B1 (ar)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/603,804 US8820090B2 (en) 2012-09-05 2012-09-05 Method for operating a gas turbine engine including a combustor shell air recirculation system
PCT/US2013/056720 WO2014039315A1 (en) 2012-09-05 2013-08-27 Method for operating a gas turbine engine including a combustor shell air recirculation system

Publications (1)

Publication Number Publication Date
SA515360105B1 true SA515360105B1 (ar) 2015-11-25

Family

ID=49151327

Family Applications (1)

Application Number Title Priority Date Filing Date
SA515360105A SA515360105B1 (ar) 2012-09-05 2015-03-03 طريقة لتشغيل محرك توربيني غازي يتضمن نظام إعادة تدوير هواء غلاف وحدة احتراق

Country Status (8)

Country Link
US (1) US8820090B2 (enExample)
EP (1) EP2893157A1 (enExample)
JP (1) JP6211616B2 (enExample)
CN (1) CN104619958B (enExample)
IN (1) IN2015DN00894A (enExample)
RU (1) RU2626047C2 (enExample)
SA (1) SA515360105B1 (enExample)
WO (1) WO2014039315A1 (enExample)

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US8973372B2 (en) * 2012-09-05 2015-03-10 Siemens Aktiengesellschaft Combustor shell air recirculation system in a gas turbine engine
US20140301820A1 (en) * 2013-04-03 2014-10-09 Uwe Lohse Turbine engine shutdown temperature control system with nozzle injection for a gas turbine engine
US20150107255A1 (en) * 2013-10-18 2015-04-23 General Electric Company Turbomachine combustor having an externally fueled late lean injection (lli) system
GB2526784A (en) 2014-05-26 2015-12-09 Skf Ab Micro electro optical mechanical system
US9869190B2 (en) 2014-05-30 2018-01-16 General Electric Company Variable-pitch rotor with remote counterweights
US20160061060A1 (en) * 2014-08-28 2016-03-03 General Electric Company Combined cycle power plant thermal energy conservation
US10072510B2 (en) 2014-11-21 2018-09-11 General Electric Company Variable pitch fan for gas turbine engine and method of assembling the same
US10100653B2 (en) 2015-10-08 2018-10-16 General Electric Company Variable pitch fan blade retention system
US10794281B2 (en) 2016-02-02 2020-10-06 General Electric Company Gas turbine engine having instrumented airflow path components
US11073090B2 (en) * 2016-03-30 2021-07-27 General Electric Company Valved airflow passage assembly for adjusting airflow distortion in gas turbine engine
US10753278B2 (en) 2016-03-30 2020-08-25 General Electric Company Translating inlet for adjusting airflow distortion in gas turbine engine
US11674435B2 (en) 2021-06-29 2023-06-13 General Electric Company Levered counterweight feathering system
US11795964B2 (en) 2021-07-16 2023-10-24 General Electric Company Levered counterweight feathering system
US11668206B1 (en) * 2022-03-09 2023-06-06 General Electric Company Temperature gradient control system for a compressor casing

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JPS5761123B2 (enExample) * 1974-04-26 1982-12-23 Hitachi Ltd
JPH06193407A (ja) * 1992-12-24 1994-07-12 Toshiba Corp タ−ビンケ−シング強制冷却装置
JP3234679B2 (ja) * 1993-06-25 2001-12-04 株式会社東芝 蒸気タービン冷却方法
JP3233824B2 (ja) * 1995-08-07 2001-12-04 三菱重工業株式会社 蒸気冷却燃焼器
EP1105623B1 (de) 1998-08-18 2003-05-28 Siemens Aktiengesellschaft Turbinengehäuse
RU2161715C2 (ru) * 1999-02-08 2001-01-10 Открытое акционерное общество Научно-производственное объединение "Искра" Устройство для охлаждения газотурбинной установки
DE10233113A1 (de) 2001-10-30 2003-05-15 Alstom Switzerland Ltd Turbomaschine
CN100516469C (zh) * 2003-04-07 2009-07-22 阿尔斯通技术有限公司 涡轮机
DE10352089A1 (de) 2003-11-07 2005-06-09 Alstom Technology Ltd Verfahren zum Betreiben einer Turbomaschine, und Turbomaschine
JP2006037855A (ja) * 2004-07-28 2006-02-09 Mitsubishi Heavy Ind Ltd 車室ケーシング及びガスタービン
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Also Published As

Publication number Publication date
JP6211616B2 (ja) 2017-10-11
EP2893157A1 (en) 2015-07-15
US8820090B2 (en) 2014-09-02
IN2015DN00894A (enExample) 2015-06-12
CN104619958B (zh) 2016-08-31
CN104619958A (zh) 2015-05-13
JP2015529301A (ja) 2015-10-05
RU2015107576A (ru) 2016-10-27
WO2014039315A1 (en) 2014-03-13
US20140060068A1 (en) 2014-03-06
RU2626047C2 (ru) 2017-07-21

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