CN102444477B - 用于燃气轮机系统的进口段 - Google Patents

用于燃气轮机系统的进口段 Download PDF

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Publication number
CN102444477B
CN102444477B CN201110321085.XA CN201110321085A CN102444477B CN 102444477 B CN102444477 B CN 102444477B CN 201110321085 A CN201110321085 A CN 201110321085A CN 102444477 B CN102444477 B CN 102444477B
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CN
China
Prior art keywords
bobbins
flow
gas turbine
turbine system
cooling medium
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
CN201110321085.XA
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English (en)
Chinese (zh)
Other versions
CN102444477A (zh
Inventor
S·K·维德纳
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 Company PLC
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 CN102444477A publication Critical patent/CN102444477A/zh
Application granted granted Critical
Publication of CN102444477B publication Critical patent/CN102444477B/zh
Active legal-status Critical Current
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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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/14—Preswirling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/97—Reducing windage losses

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CN201110321085.XA 2010-10-12 2011-10-12 用于燃气轮机系统的进口段 Active CN102444477B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/902,699 US8529195B2 (en) 2010-10-12 2010-10-12 Inducer for gas turbine system
US12/902699 2010-10-12

Publications (2)

Publication Number Publication Date
CN102444477A CN102444477A (zh) 2012-05-09
CN102444477B true CN102444477B (zh) 2016-09-28

Family

ID=45872521

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201110321085.XA Active CN102444477B (zh) 2010-10-12 2011-10-12 用于燃气轮机系统的进口段

Country Status (5)

Country Link
US (1) US8529195B2 (enExample)
JP (1) JP6055174B2 (enExample)
CN (1) CN102444477B (enExample)
DE (1) DE102011054388B4 (enExample)
FR (1) FR2965845B1 (enExample)

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US9435206B2 (en) 2012-09-11 2016-09-06 General Electric Company Flow inducer for a gas turbine system
GB2510004B (en) * 2013-08-19 2015-10-14 Rolls Royce Plc Axial flow machine cooling system
US9447794B2 (en) * 2013-08-27 2016-09-20 General Electric Company Inducer and diffuser configuration for a gas turbine system
US9927123B2 (en) * 2013-10-24 2018-03-27 United Technologies Corporation Fluid transport system having divided transport tube
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FR3015569B1 (fr) * 2013-12-19 2019-01-25 Safran Aircraft Engines Carter pour un ensemble propulsif
GB201408543D0 (en) 2014-05-14 2014-06-25 Rolls Royce Plc Distributor device for cooling air within an engine
CA2949547A1 (en) 2014-05-29 2016-02-18 General Electric Company Turbine engine and particle separators therefore
US11033845B2 (en) * 2014-05-29 2021-06-15 General Electric Company Turbine engine and particle separators therefore
CN104675522B (zh) * 2015-01-30 2019-10-01 北京华清燃气轮机与煤气化联合循环工程技术有限公司 一种燃气轮机涡轮气路
US10208668B2 (en) 2015-09-30 2019-02-19 Rolls-Royce Corporation Turbine engine advanced cooling system
US10352245B2 (en) 2015-10-05 2019-07-16 General Electric Company Windage shield system and method of suppressing resonant acoustic noise
US10113486B2 (en) 2015-10-06 2018-10-30 General Electric Company Method and system for modulated turbine cooling
US10196982B2 (en) * 2015-11-04 2019-02-05 General Electric Company Gas turbine engine having a flow control surface with a cooling conduit
US10830144B2 (en) 2016-09-08 2020-11-10 Rolls-Royce North American Technologies Inc. Gas turbine engine compressor impeller cooling air sinks
US10697372B2 (en) 2017-04-05 2020-06-30 General Electric Company Turbine engine conduit interface
DE102017217034A1 (de) * 2017-09-26 2019-03-28 Siemens Aktiengesellschaft Turbinengehäuse mit Stutzen sowie Verfahren zum Herstellen eines Turbinengehäuses mit Stutzen
US10982546B2 (en) * 2018-09-19 2021-04-20 General Electric Company Flow-diverting systems for gas turbine air separator
WO2020112476A1 (en) * 2018-11-30 2020-06-04 Siemens Aktiengesellschaft Secondary air system in-situ installation of a drain hole plug
WO2020149854A1 (en) * 2019-01-18 2020-07-23 Siemens Aktiengesellschaft Pre-swirler with pre-swirler plug for gas turbine engine
WO2021015861A1 (en) * 2019-07-25 2021-01-28 Siemens Energy Global GmbH & Co. KG Pre-swirler adjustability in gas turbine engine
US11421597B2 (en) * 2019-10-18 2022-08-23 Pratt & Whitney Canada Corp. Tangential on-board injector (TOBI) assembly
US11525393B2 (en) 2020-03-19 2022-12-13 Rolls-Royce Corporation Turbine engine with centrifugal compressor having impeller backplate offtake
US11598265B2 (en) * 2021-02-03 2023-03-07 Pratt & Whitney Canada Corp. Tangential on-board injector
CN113933061B (zh) * 2021-09-30 2024-04-19 中国联合重型燃气轮机技术有限公司 静叶模拟器和具有其的燃烧室试验装置
EP4174286B1 (en) * 2021-10-29 2024-12-04 ANSALDO ENERGIA S.p.A. Gas turbine assembly for power plant with improved rotor and turbine blades cooling and method for operating this gas turbine assembly
US11821365B2 (en) * 2022-01-31 2023-11-21 General Electric Company Inducer seal with integrated inducer slots
US11773773B1 (en) 2022-07-26 2023-10-03 Rolls-Royce North American Technologies Inc. Gas turbine engine centrifugal compressor with impeller load and cooling control
DE102023111513A1 (de) * 2023-05-03 2024-11-07 MTU Aero Engines AG Rotorscheibe für einen Schaufelkranz

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US6234746B1 (en) * 1999-08-04 2001-05-22 General Electric Co. Apparatus and methods for cooling rotary components in a turbine

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US6234746B1 (en) * 1999-08-04 2001-05-22 General Electric Co. Apparatus and methods for cooling rotary components in a turbine

Also Published As

Publication number Publication date
US20120087784A1 (en) 2012-04-12
CN102444477A (zh) 2012-05-09
US8529195B2 (en) 2013-09-10
DE102011054388A1 (de) 2012-04-12
FR2965845B1 (fr) 2016-03-11
JP2012082822A (ja) 2012-04-26
JP6055174B2 (ja) 2016-12-27
DE102011054388B4 (de) 2023-06-01
FR2965845A1 (fr) 2012-04-13

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SE01 Entry into force of request for substantive examination
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GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20231227

Address after: Swiss Baden

Patentee after: GENERAL ELECTRIC CO. LTD.

Address before: New York, United States

Patentee before: General Electric Co.

TR01 Transfer of patent right