AR011159A1 - Metodo para convertir una transicion refrigerada por vapor en una transicion refrigerada por aire en una turbina de gas y transicionrefrigerada por vapor convertida a transicion refrigerada por aire - Google Patents

Metodo para convertir una transicion refrigerada por vapor en una transicion refrigerada por aire en una turbina de gas y transicionrefrigerada por vapor convertida a transicion refrigerada por aire

Info

Publication number
AR011159A1
AR011159A1 ARP980100779A ARP980100779A AR011159A1 AR 011159 A1 AR011159 A1 AR 011159A1 AR P980100779 A ARP980100779 A AR P980100779A AR P980100779 A ARP980100779 A AR P980100779A AR 011159 A1 AR011159 A1 AR 011159A1
Authority
AR
Argentina
Prior art keywords
transition
cooled transition
air
steam
cooled
Prior art date
Application number
ARP980100779A
Other languages
English (en)
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of AR011159A1 publication Critical patent/AR011159A1/es

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/005—Combined with pressure or heat exchangers
    • 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
    • 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
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings

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)

Abstract

Un método de convertir una transicion refrigerada por vapor en una transicion refrigerada por aire en una turbina de gas que tiene una compresoren comunicacion de fluido con un mechero, una seccion de turbina en comunicacion de fluido con el mechero, la transicion dispuesta en una vaina demechero y que tiene un circuito de refrigeracion que conecta una salida de vapor y una entrada de vapor y en donde fluye gas caliente desde el mechero através de la transicion y haciala seccion de turbina, incluye formar una salida de aire en la transicion en comunicacion de fluido con el circuito derefrigeracion y proveer una entrada de aire en la transicion en comunicacion de fluido con el circuito refrigerante. Incluye una turbina para llevar a cabodicho método y una transicion refrigerada por vapor convertible a una transicion refrigerada por aire.
ARP980100779A 1997-02-21 1998-02-20 Metodo para convertir una transicion refrigerada por vapor en una transicion refrigerada por aire en una turbina de gas y transicionrefrigerada por vapor convertida a transicion refrigerada por aire AR011159A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/803,614 US5906093A (en) 1997-02-21 1997-02-21 Gas turbine combustor transition

Publications (1)

Publication Number Publication Date
AR011159A1 true AR011159A1 (es) 2000-08-02

Family

ID=25187008

Family Applications (1)

Application Number Title Priority Date Filing Date
ARP980100779A AR011159A1 (es) 1997-02-21 1998-02-20 Metodo para convertir una transicion refrigerada por vapor en una transicion refrigerada por aire en una turbina de gas y transicionrefrigerada por vapor convertida a transicion refrigerada por aire

Country Status (7)

Country Link
US (1) US5906093A (es)
EP (1) EP1009915B1 (es)
JP (1) JP2002511121A (es)
KR (1) KR20000070976A (es)
AR (1) AR011159A1 (es)
DE (1) DE69810940T2 (es)
WO (1) WO1998037311A1 (es)

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JP3110338B2 (ja) * 1997-02-12 2000-11-20 東北電力株式会社 燃焼器の蒸気による冷却構造
JP3310900B2 (ja) * 1997-04-15 2002-08-05 三菱重工業株式会社 燃焼器尾筒の冷却構造
DE60137099D1 (de) * 2000-04-13 2009-02-05 Mitsubishi Heavy Ind Ltd Kühlstruktur für das Endstück einer Gasturbinenbrennkammer
JP2002243154A (ja) * 2001-02-16 2002-08-28 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器尾筒出口構造及びガスタービン燃焼器
JP2002309903A (ja) * 2001-04-10 2002-10-23 Mitsubishi Heavy Ind Ltd ガスタービンの蒸気配管構造
JP4008212B2 (ja) * 2001-06-29 2007-11-14 三菱重工業株式会社 フランジ付中空構造物
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US7870739B2 (en) * 2006-02-02 2011-01-18 Siemens Energy, Inc. Gas turbine engine curved diffuser with partial impingement cooling apparatus for transitions
US7827801B2 (en) * 2006-02-09 2010-11-09 Siemens Energy, Inc. Gas turbine engine transitions comprising closed cooled transition cooling channels
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US8549861B2 (en) * 2009-01-07 2013-10-08 General Electric Company Method and apparatus to enhance transition duct cooling in a gas turbine engine
US8281601B2 (en) * 2009-03-20 2012-10-09 General Electric Company Systems and methods for reintroducing gas turbine combustion bypass flow
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US8966910B2 (en) * 2011-06-21 2015-03-03 General Electric Company Methods and systems for cooling a transition nozzle
US9188009B2 (en) * 2012-10-30 2015-11-17 United Technologies Corporation Bore cavity thermal conditioning system
US9574498B2 (en) * 2013-09-25 2017-02-21 General Electric Company Internally cooled transition duct aft frame with serpentine cooling passage and conduit
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KR102403512B1 (ko) 2015-04-30 2022-05-31 삼성전자주식회사 공기 조화기의 실외기, 이에 적용되는 컨트롤 장치
DE102015212573A1 (de) * 2015-07-06 2017-01-12 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit integriertem Turbinenvorleitrad sowie Verfahren zu deren Herstellung
US10520193B2 (en) 2015-10-28 2019-12-31 General Electric Company Cooling patch for hot gas path components
US10830442B2 (en) 2016-03-25 2020-11-10 General Electric Company Segmented annular combustion system with dual fuel capability
US10563869B2 (en) 2016-03-25 2020-02-18 General Electric Company Operation and turndown of a segmented annular combustion system
US10605459B2 (en) 2016-03-25 2020-03-31 General Electric Company Integrated combustor nozzle for a segmented annular combustion system
US10641491B2 (en) 2016-03-25 2020-05-05 General Electric Company Cooling of integrated combustor nozzle of segmented annular combustion system
US10584876B2 (en) 2016-03-25 2020-03-10 General Electric Company Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system
US10641175B2 (en) 2016-03-25 2020-05-05 General Electric Company Panel fuel injector
US10584880B2 (en) 2016-03-25 2020-03-10 General Electric Company Mounting of integrated combustor nozzles in a segmented annular combustion system
US11428413B2 (en) 2016-03-25 2022-08-30 General Electric Company Fuel injection module for segmented annular combustion system
US10520194B2 (en) 2016-03-25 2019-12-31 General Electric Company Radially stacked fuel injection module for a segmented annular combustion system
US10830142B2 (en) * 2016-10-10 2020-11-10 General Electric Company Combustor aft frame cooling
US11156362B2 (en) 2016-11-28 2021-10-26 General Electric Company Combustor with axially staged fuel injection
US10690350B2 (en) 2016-11-28 2020-06-23 General Electric Company Combustor with axially staged fuel injection
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
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Also Published As

Publication number Publication date
EP1009915A1 (en) 2000-06-21
US5906093A (en) 1999-05-25
JP2002511121A (ja) 2002-04-09
EP1009915B1 (en) 2003-01-22
DE69810940T2 (de) 2003-08-28
DE69810940D1 (de) 2003-02-27
WO1998037311A1 (en) 1998-08-27
KR20000070976A (ko) 2000-11-25

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