DE60236991D1 - Befestigungsvorrichtung für Gasturbinenbrennkammer - Google Patents

Befestigungsvorrichtung für Gasturbinenbrennkammer

Info

Publication number
DE60236991D1
DE60236991D1 DE60236991T DE60236991T DE60236991D1 DE 60236991 D1 DE60236991 D1 DE 60236991D1 DE 60236991 T DE60236991 T DE 60236991T DE 60236991 T DE60236991 T DE 60236991T DE 60236991 D1 DE60236991 D1 DE 60236991D1
Authority
DE
Germany
Prior art keywords
gas turbine
fastening device
turbine combustor
combustor
fastening
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.)
Expired - Lifetime
Application number
DE60236991T
Other languages
English (en)
Inventor
Thomas L Maclean
Tod K Bosel
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 Co
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
Application granted granted Critical
Publication of DE60236991D1 publication Critical patent/DE60236991D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50Combustion chambers comprising an annular flame tube within an annular casing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60Support structures; Attaching or mounting means

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)
DE60236991T 2001-12-18 2002-12-10 Befestigungsvorrichtung für Gasturbinenbrennkammer Expired - Lifetime DE60236991D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/024,094 US6672833B2 (en) 2001-12-18 2001-12-18 Gas turbine engine frame flowpath liner support

Publications (1)

Publication Number Publication Date
DE60236991D1 true DE60236991D1 (de) 2010-08-26

Family

ID=21818838

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60236991T Expired - Lifetime DE60236991D1 (de) 2001-12-18 2002-12-10 Befestigungsvorrichtung für Gasturbinenbrennkammer

Country Status (5)

Country Link
US (1) US6672833B2 (de)
EP (1) EP1323983B1 (de)
JP (1) JP4471566B2 (de)
CN (1) CN100489398C (de)
DE (1) DE60236991D1 (de)

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US10240532B2 (en) 2012-12-29 2019-03-26 United Technologies Corporation Frame junction cooling holes
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JP6271582B2 (ja) 2012-12-29 2018-01-31 ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation ガスタービンシールアセンブリおよびシール支持体
US9828867B2 (en) 2012-12-29 2017-11-28 United Technologies Corporation Bumper for seals in a turbine exhaust case
EP2938863B1 (de) 2012-12-29 2019-09-25 United Technologies Corporation Mechanische verbindung für segmentierten hitzeschild
WO2014105602A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Heat shield for a casing
US10006306B2 (en) 2012-12-29 2018-06-26 United Technologies Corporation Turbine exhaust case architecture
WO2014105577A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Scupper channelling in gas turbine modules
JP6385955B2 (ja) 2012-12-29 2018-09-05 ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation タービンフレームアセンブリおよびタービンフレームアセンブリを設計する方法
WO2014105826A1 (en) 2012-12-29 2014-07-03 United Technologies Corporation Seal support disk and assembly
US9541006B2 (en) 2012-12-29 2017-01-10 United Technologies Corporation Inter-module flow discourager
US10054009B2 (en) 2012-12-31 2018-08-21 United Technologies Corporation Turbine exhaust case multi-piece frame
EP2938860B1 (de) 2012-12-31 2018-08-29 United Technologies Corporation Turbinenabgasgehäuse mit mehrteiligem rahmen
WO2014105682A1 (en) 2012-12-31 2014-07-03 United Technologies Corporation Turbine exhaust case multi-piece frame
US9617872B2 (en) 2013-02-14 2017-04-11 United Technologies Corporation Low profile thermally free blind liner hanger attachment for complex shapes
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US9771828B2 (en) * 2015-04-01 2017-09-26 General Electric Company Turbine exhaust frame and method of vane assembly
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EP3159505B1 (de) * 2015-10-20 2020-01-08 MTU Aero Engines GmbH Zwischengehàuse für eine gasturbine
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ES2861200T3 (es) * 2015-12-15 2021-10-06 MTU Aero Engines AG Conexión de componentes de turbomaquinaria
EP3208431B1 (de) 2016-02-16 2022-01-05 MTU Aero Engines AG Verbindungsanordnung für gehäuseelement eines turbinenzwischengehäuses
RU2715634C2 (ru) 2016-11-21 2020-03-02 Дженерал Электрик Текнолоджи Гмбх Устройство и способ для принудительного охлаждения компонентов газотурбинной установки
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Also Published As

Publication number Publication date
CN100489398C (zh) 2009-05-20
CN1427141A (zh) 2003-07-02
JP4471566B2 (ja) 2010-06-02
EP1323983A3 (de) 2004-01-07
JP2003201913A (ja) 2003-07-18
EP1323983A2 (de) 2003-07-02
US6672833B2 (en) 2004-01-06
US20030161727A1 (en) 2003-08-28
EP1323983B1 (de) 2010-07-14

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