JP3727987B2 - ガスタービン燃焼器とガスタービン段との間の移行部材 - Google Patents

ガスタービン燃焼器とガスタービン段との間の移行部材 Download PDF

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Publication number
JP3727987B2
JP3727987B2 JP32613595A JP32613595A JP3727987B2 JP 3727987 B2 JP3727987 B2 JP 3727987B2 JP 32613595 A JP32613595 A JP 32613595A JP 32613595 A JP32613595 A JP 32613595A JP 3727987 B2 JP3727987 B2 JP 3727987B2
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Japan
Prior art keywords
transition member
gas turbine
rear end
outer portion
transition
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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 - Fee Related
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JP32613595A
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English (en)
Japanese (ja)
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JPH08261017A5 (enExample
JPH08261017A (ja
Inventor
ジョン・ユジーン・バーンズ
ロジャー・オーバル・アンダーソン
チャールス・エバン・ステバー
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General Electric Co
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General Electric Co
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
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Publication of JPH08261017A5 publication Critical patent/JPH08261017A5/ja
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Publication of JP3727987B2 publication Critical patent/JP3727987B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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
    • F23R3/60Support structures; Attaching or mounting means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023Transition 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)
JP32613595A 1994-12-20 1995-12-15 ガスタービン燃焼器とガスタービン段との間の移行部材 Expired - Fee Related JP3727987B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US35949594A 1994-12-20 1994-12-20
US08/359495 1994-12-20

Publications (3)

Publication Number Publication Date
JPH08261017A JPH08261017A (ja) 1996-10-08
JPH08261017A5 JPH08261017A5 (enExample) 2005-11-04
JP3727987B2 true JP3727987B2 (ja) 2005-12-21

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ID=23414052

Family Applications (1)

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JP32613595A Expired - Fee Related JP3727987B2 (ja) 1994-12-20 1995-12-15 ガスタービン燃焼器とガスタービン段との間の移行部材

Country Status (4)

Country Link
US (1) US5761898A (enExample)
EP (1) EP0718468B1 (enExample)
JP (1) JP3727987B2 (enExample)
DE (1) DE69523545T2 (enExample)

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US10584880B2 (en) 2016-03-25 2020-03-10 General Electric Company Mounting of integrated combustor nozzles in 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
US11156362B2 (en) 2016-11-28 2021-10-26 General Electric Company Combustor with axially staged fuel injection
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Also Published As

Publication number Publication date
JPH08261017A (ja) 1996-10-08
US5761898A (en) 1998-06-09
DE69523545D1 (de) 2001-12-06
DE69523545T2 (de) 2002-05-29
EP0718468B1 (en) 2001-10-31
EP0718468A1 (en) 1996-06-26

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