KR20010007041A - 터빈 베인 세그먼트 - Google Patents

터빈 베인 세그먼트 Download PDF

Info

Publication number
KR20010007041A
KR20010007041A KR1020000023861A KR20000023861A KR20010007041A KR 20010007041 A KR20010007041 A KR 20010007041A KR 1020000023861 A KR1020000023861 A KR 1020000023861A KR 20000023861 A KR20000023861 A KR 20000023861A KR 20010007041 A KR20010007041 A KR 20010007041A
Authority
KR
South Korea
Prior art keywords
wall
cooling
cavity
leading edge
cavities
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
KR1020000023861A
Other languages
English (en)
Korean (ko)
Inventor
이첼개리마이클
유유펭필립
Original Assignee
제이 엘. 차스킨
제너럴 일렉트릭 캄파니
버나드 스나이더
아더엠. 킹
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 제이 엘. 차스킨, 제너럴 일렉트릭 캄파니, 버나드 스나이더, 아더엠. 킹 filed Critical 제이 엘. 차스킨
Publication of KR20010007041A publication Critical patent/KR20010007041A/ko
Ceased legal-status Critical Current

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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • 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
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
KR1020000023861A 1999-05-10 2000-05-04 터빈 베인 세그먼트 Ceased KR20010007041A (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/307,719 US6406254B1 (en) 1999-05-10 1999-05-10 Cooling circuit for steam and air-cooled turbine nozzle stage
US09/307,719 1999-05-10

Publications (1)

Publication Number Publication Date
KR20010007041A true KR20010007041A (ko) 2001-01-26

Family

ID=23190921

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020000023861A Ceased KR20010007041A (ko) 1999-05-10 2000-05-04 터빈 베인 세그먼트

Country Status (5)

Country Link
US (1) US6406254B1 (enExample)
EP (1) EP1052374B1 (enExample)
JP (1) JP4393667B2 (enExample)
KR (1) KR20010007041A (enExample)
DE (1) DE60030030T2 (enExample)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10217388A1 (de) * 2002-04-18 2003-10-30 Siemens Ag Luft- und dampfgekühlte Plattform einer Turbinenschaufel
US6742984B1 (en) 2003-05-19 2004-06-01 General Electric Company Divided insert for steam cooled nozzles and method for supporting and separating divided insert
US6843637B1 (en) 2003-08-04 2005-01-18 General Electric Company Cooling circuit within a turbine nozzle and method of cooling a turbine nozzle
JP5210722B2 (ja) * 2008-06-18 2013-06-12 株式会社日立製作所 ガスタービン静翼の冷却構造および冷媒供給構造
JP5222057B2 (ja) * 2008-08-08 2013-06-26 三菱重工業株式会社 ガスタービン高温部の冷却装置
US8439628B2 (en) 2010-01-06 2013-05-14 General Electric Company Heat transfer enhancement in internal cavities of turbine engine airfoils
US8851845B2 (en) * 2010-11-17 2014-10-07 General Electric Company Turbomachine vane and method of cooling a turbomachine vane
US8979477B2 (en) * 2011-03-09 2015-03-17 General Electric Company System for cooling and purging exhaust section of gas turbine engine
CN102312684A (zh) * 2011-09-05 2012-01-11 沈阳黎明航空发动机(集团)有限责任公司 一种蒸汽、空气混合冷却透平导向叶片
PL220729B1 (pl) 2011-10-03 2015-12-31 Gen Electric Układ turbiny gazowej
US20130283814A1 (en) * 2012-04-25 2013-10-31 General Electric Company Turbine cooling system
US9500099B2 (en) * 2012-07-02 2016-11-22 United Techologies Corporation Cover plate for a component of a gas turbine engine
US9670797B2 (en) 2012-09-28 2017-06-06 United Technologies Corporation Modulated turbine vane cooling
EP3004558B1 (en) 2013-06-04 2021-08-25 Raytheon Technologies Corporation Gas turbine engine airfoil trailing edge suction side cooling
US9334803B2 (en) 2013-08-20 2016-05-10 General Electric Company Method of recovering energy in a steam-cooled gas turbine
US20170234218A1 (en) * 2016-02-16 2017-08-17 Florida Turbine Technologies, Inc. Turbine Stator Vane with Multiple Outer Diameter Pressure Feeds
US10260356B2 (en) * 2016-06-02 2019-04-16 General Electric Company Nozzle cooling system for a gas turbine engine
US20180149085A1 (en) * 2016-11-28 2018-05-31 General Electric Company Exhaust frame cooling via cooling flow reversal
US10428660B2 (en) * 2017-01-31 2019-10-01 United Technologies Corporation Hybrid airfoil cooling
US11242760B2 (en) * 2020-01-22 2022-02-08 General Electric Company Turbine rotor blade with integral impingement sleeve by additive manufacture
CN111691926B (zh) * 2020-06-24 2021-09-14 中船重工龙江广瀚燃气轮机有限公司 一种带空气流道的动力涡轮导叶组
CN115559789A (zh) * 2022-09-19 2023-01-03 中国航发湖南动力机械研究所 一种具有冷却结构的涡轮导向叶片
US12331684B2 (en) * 2023-11-07 2025-06-17 Rtx Corporation Strut microtube counterflow evaporator
CN119957317B (zh) * 2025-03-21 2025-11-21 中国航发湖南动力机械研究所 一种回转内腔供气冷却叶片及航空发动机

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3142850B2 (ja) * 1989-03-13 2001-03-07 株式会社東芝 タービンの冷却翼および複合発電プラント
US5634766A (en) 1994-08-23 1997-06-03 General Electric Co. Turbine stator vane segments having combined air and steam cooling circuits
JPH1037704A (ja) * 1996-07-19 1998-02-10 Mitsubishi Heavy Ind Ltd ガスタービンの静翼
JP3316405B2 (ja) * 1997-02-04 2002-08-19 三菱重工業株式会社 ガスタービン冷却静翼
US5827043A (en) * 1997-06-27 1998-10-27 United Technologies Corporation Coolable airfoil

Also Published As

Publication number Publication date
US20020037217A1 (en) 2002-03-28
DE60030030D1 (de) 2006-09-28
JP4393667B2 (ja) 2010-01-06
EP1052374A3 (en) 2003-12-03
EP1052374A2 (en) 2000-11-15
JP2000337102A (ja) 2000-12-05
US6406254B1 (en) 2002-06-18
EP1052374B1 (en) 2006-08-16
DE60030030T2 (de) 2007-03-08

Similar Documents

Publication Publication Date Title
KR20010007041A (ko) 터빈 베인 세그먼트
KR100534812B1 (ko) 터빈 베인 세그먼트
US6416275B1 (en) Recessed impingement insert metering plate for gas turbine nozzles
US6561757B2 (en) Turbine vane segment and impingement insert configuration for fail-safe impingement insert retention
US5480281A (en) Impingement cooling apparatus for turbine shrouds having ducts of increasing cross-sectional area in the direction of post-impingement cooling flow
US6089822A (en) Gas turbine stationary blade
JP4130540B2 (ja) ガスタービンノズル壁を局部的に冷却するための装置及び方法
US6431824B2 (en) Turbine nozzle stage having thermocouple guide tube
CA2250169C (en) Cooled stationary blade of gas turbine
EP1160418B1 (en) Turbine vane segment
US6422817B1 (en) Cooling circuit for and method of cooling a gas turbine bucket
US6468031B1 (en) Nozzle cavity impingement/area reduction insert
EP0814234B1 (en) Stationary blade for gas turbine
US20080112816A1 (en) Air-cooled component
EP1156186A2 (en) Film cooling air pocket in a closed loop cooled airfoil
JP2004060638A (ja) 静翼の冷却構造及びガスタービン
JP2001317302A (ja) 閉回路冷却される翼形部の膜冷却
US6390769B1 (en) Closed circuit steam cooled turbine shroud and method for steam cooling turbine shroud
US8641377B1 (en) Industrial turbine blade with platform cooling

Legal Events

Date Code Title Description
PA0109 Patent application

Patent event code: PA01091R01D

Comment text: Patent Application

Patent event date: 20000504

PG1501 Laying open of application
A201 Request for examination
PA0201 Request for examination

Patent event code: PA02012R01D

Patent event date: 20020504

Comment text: Request for Examination of Application

Patent event code: PA02011R01I

Patent event date: 20000504

Comment text: Patent Application

E902 Notification of reason for refusal
PE0902 Notice of grounds for rejection

Comment text: Notification of reason for refusal

Patent event date: 20040702

Patent event code: PE09021S01D

E601 Decision to refuse application
PE0601 Decision on rejection of patent

Patent event date: 20040908

Comment text: Decision to Refuse Application

Patent event code: PE06012S01D

Patent event date: 20040702

Comment text: Notification of reason for refusal

Patent event code: PE06011S01I