KR20010076202A - 가스 터빈용 냉각 공기 유동 조절 시스템, 다단 압축기의단에서 관련 터빈으로 공기를 분출하기 위한 시스템, 및다단 압축기에서 관련 터빈으로 냉각 및/또는 퍼지 공기의제공 방법 - Google Patents

가스 터빈용 냉각 공기 유동 조절 시스템, 다단 압축기의단에서 관련 터빈으로 공기를 분출하기 위한 시스템, 및다단 압축기에서 관련 터빈으로 냉각 및/또는 퍼지 공기의제공 방법 Download PDF

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Publication number
KR20010076202A
KR20010076202A KR1020000055784A KR20000055784A KR20010076202A KR 20010076202 A KR20010076202 A KR 20010076202A KR 1020000055784 A KR1020000055784 A KR 1020000055784A KR 20000055784 A KR20000055784 A KR 20000055784A KR 20010076202 A KR20010076202 A KR 20010076202A
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KR
South Korea
Prior art keywords
air
turbine
pressure
compressor
cooling
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.)
Ceased
Application number
KR1020000055784A
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English (en)
Korean (ko)
Inventor
리언샐앨버트
북매튜데이비드
배네어스크리스토퍼알
Original Assignee
제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹
제너럴 일렉트릭 캄파니
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
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First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=23952886&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=KR20010076202(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by 제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹, 제너럴 일렉트릭 캄파니 filed Critical 제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹
Publication of KR20010076202A publication Critical patent/KR20010076202A/ko
Ceased legal-status Critical Current

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Classifications

    • 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
    • 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
    • F01D25/12—Cooling
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/301—Pressure
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/301—Pressure
    • F05D2270/3015—Pressure differential pressure

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)
KR1020000055784A 2000-01-25 2000-09-22 가스 터빈용 냉각 공기 유동 조절 시스템, 다단 압축기의단에서 관련 터빈으로 공기를 분출하기 위한 시스템, 및다단 압축기에서 관련 터빈으로 냉각 및/또는 퍼지 공기의제공 방법 Ceased KR20010076202A (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/491,599 US6393825B1 (en) 2000-01-25 2000-01-25 System for pressure modulation of turbine sidewall cavities
US09/491,599 2000-01-25

Publications (1)

Publication Number Publication Date
KR20010076202A true KR20010076202A (ko) 2001-08-11

Family

ID=23952886

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020000055784A Ceased KR20010076202A (ko) 2000-01-25 2000-09-22 가스 터빈용 냉각 공기 유동 조절 시스템, 다단 압축기의단에서 관련 터빈으로 공기를 분출하기 위한 시스템, 및다단 압축기에서 관련 터빈으로 냉각 및/또는 퍼지 공기의제공 방법

Country Status (7)

Country Link
US (2) US6393825B1 (enExample)
EP (1) EP1120559B1 (enExample)
JP (1) JP4897993B2 (enExample)
KR (1) KR20010076202A (enExample)
AT (1) ATE412821T1 (enExample)
CZ (1) CZ20003306A3 (enExample)
DE (1) DE60040646D1 (enExample)

Cited By (3)

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US9169782B2 (en) 2012-01-04 2015-10-27 General Electric Company Turbine to operate at part-load
KR101939495B1 (ko) 2017-09-21 2019-01-16 두산중공업 주식회사 압축기 및 이를 포함하는 가스 터빈
KR20190033353A (ko) 2017-09-21 2019-03-29 두산중공업 주식회사 압축기 및 이를 포함하는 가스 터빈

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EP1614858A1 (de) * 2004-07-09 2006-01-11 Siemens Aktiengesellschaft Verfahren und Vorrichtung zur Überwachung des Kühlluftsystems einer Turbine
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US8643147B2 (en) * 2007-11-01 2014-02-04 Taiwan Semiconductor Manufacturing Company, Ltd. Seal ring structure with improved cracking protection and reduced problems
JP2009243341A (ja) * 2008-03-31 2009-10-22 Ihi Corp 抽気装置
JP5297114B2 (ja) * 2008-08-06 2013-09-25 三菱重工業株式会社 ガスタービン
US8061971B2 (en) * 2008-09-12 2011-11-22 General Electric Company Apparatus and method for cooling a turbine
US8677761B2 (en) * 2009-02-25 2014-03-25 General Electric Company Systems and methods for engine turn down by controlling extraction air flows
US8355854B2 (en) * 2009-05-08 2013-01-15 General Electric Company Methods relating to gas turbine control and operation
ITTO20100824A1 (it) * 2010-10-06 2012-04-07 Ansaldo Energia Spa Metodo di controllo per raffreddare uno stadio di turbina in una turbina a gas
US9151182B2 (en) * 2011-04-22 2015-10-06 General Electric Company System and method for removing heat from a turbomachine
EP2597287A1 (de) 2011-11-28 2013-05-29 Siemens Aktiengesellschaft Verfahren zum Betrieb einer stationären Gasturbine mit einem niederkalorischen oder mittelkalorischen Brennstoff sowie stationäre Gasturbine dafür
US8769962B2 (en) 2012-01-31 2014-07-08 United Technologies Corporation Multi-circuit buffer system for a gas turbine engine
US9982886B2 (en) * 2012-07-06 2018-05-29 Honeywell International Inc. Flue gas recycle system with fixed orifices
US9328923B2 (en) 2012-10-10 2016-05-03 General Electric Company System and method for separating fluids
US9670796B2 (en) 2012-11-07 2017-06-06 General Electric Company Compressor bellmouth with a wash door
US10272475B2 (en) 2012-11-07 2019-04-30 General, Electric Company Offline compressor wash systems and methods
US9464534B2 (en) * 2012-12-14 2016-10-11 General Electric Company Turbine purge flow control system and related method of operation
US9482236B2 (en) * 2013-03-13 2016-11-01 Rolls-Royce Corporation Modulated cooling flow scheduling for both SFC improvement and stall margin increase
US9534536B2 (en) 2013-07-02 2017-01-03 General Electric Company Turbine flow modulation for part load performance
US9366194B2 (en) 2013-09-05 2016-06-14 General Electric Company Method and system for controlling gas turbine performance with a variable backflow margin
US10168716B2 (en) * 2014-10-02 2019-01-01 General Electric Company Valve position demand systems and methods
US10100730B2 (en) 2015-03-11 2018-10-16 Pratt & Whitney Canada Corp. Secondary air system with venturi
US9797310B2 (en) 2015-04-02 2017-10-24 General Electric Company Heat pipe temperature management system for a turbomachine
WO2016160023A1 (en) 2015-04-02 2016-10-06 General Electric Company Heat pipe temperature management system for wheels and buckets in a turbomachine
CA2957467A1 (en) * 2016-02-24 2017-08-24 General Electric Company Turbine engine ejector throat control
CN105750129A (zh) * 2016-04-29 2016-07-13 泉州市宏恩新能源汽车科技有限公司 空气动力学喷嘴
US10612405B2 (en) 2017-01-13 2020-04-07 United Technologies Corporation Stator outer platform sealing and retainer
US10684149B2 (en) 2018-03-09 2020-06-16 Rolls-Royce Corporation System and method of measuring turbine vane cooling air consumption during engine operation
WO2021194473A1 (en) * 2020-03-24 2021-09-30 Siemens Energy, Inc. Method for modulating a turbine cooling supply for gas turbine applications
CN113107680B (zh) * 2021-04-21 2022-04-19 南京航空航天大学 带无级可调放气活门的高超声速大内收缩比进气道及控制方法
CN113107681B (zh) * 2021-04-21 2022-02-08 南京航空航天大学 一种连续可调的进气道放气装置
US20240413711A1 (en) * 2023-06-07 2024-12-12 Hamilton Sundstrand Corporation Hybrid liquid and air cooling of high-power permanent magnet machine rotor
US12428973B2 (en) 2023-12-22 2025-09-30 Ge Infrastructure Technology Llc Mitigation of rotating stall in turbine exhaust section using segmented auxiliary struts
US12338776B1 (en) 2023-12-22 2025-06-24 Ge Infrastructure Technology Llc Fluid injection system and method for mitigating rotating stall in turbine engine

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9169782B2 (en) 2012-01-04 2015-10-27 General Electric Company Turbine to operate at part-load
KR101939495B1 (ko) 2017-09-21 2019-01-16 두산중공업 주식회사 압축기 및 이를 포함하는 가스 터빈
KR20190033353A (ko) 2017-09-21 2019-03-29 두산중공업 주식회사 압축기 및 이를 포함하는 가스 터빈
US10760421B2 (en) 2017-09-21 2020-09-01 Doosan Heavy Industries Contruction Co., Ltd Compressor and gas turbine including the same

Also Published As

Publication number Publication date
US20010018824A1 (en) 2001-09-06
EP1120559A2 (en) 2001-08-01
CZ20003306A3 (cs) 2001-09-12
JP2001207864A (ja) 2001-08-03
US6385958B2 (en) 2002-05-14
US6393825B1 (en) 2002-05-28
DE60040646D1 (de) 2008-12-11
EP1120559A3 (en) 2004-08-25
ATE412821T1 (de) 2008-11-15
JP4897993B2 (ja) 2012-03-14
EP1120559B1 (en) 2008-10-29

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