JP6186133B2 - タービンシステムの移行ダクト用の重畳シール - Google Patents

タービンシステムの移行ダクト用の重畳シール Download PDF

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Publication number
JP6186133B2
JP6186133B2 JP2013034084A JP2013034084A JP6186133B2 JP 6186133 B2 JP6186133 B2 JP 6186133B2 JP 2013034084 A JP2013034084 A JP 2013034084A JP 2013034084 A JP2013034084 A JP 2013034084A JP 6186133 B2 JP6186133 B2 JP 6186133B2
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JP
Japan
Prior art keywords
turbine system
outer leg
transition duct
transition
seal
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 - Fee Related
Application number
JP2013034084A
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English (en)
Japanese (ja)
Other versions
JP2013231426A5 (enExample
JP2013231426A (ja
Inventor
ジェームズ・スコット・フラナガン
ロニー・レイ・ペンテコスト
ケヴィン・ウエストン・マクマハン
ダニエル・ジャクソン・ディラード
ジェフリー・スコット・ルベグ
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
Publication of JP2013231426A publication Critical patent/JP2013231426A/ja
Publication of JP2013231426A5 publication Critical patent/JP2013231426A5/ja
Application granted granted Critical
Publication of JP6186133B2 publication Critical patent/JP6186133B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • F23R3/002—Wall structures
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • 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
    • F05D2240/00—Components
    • F05D2240/55—Seals
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/18—Two-dimensional patterned
    • F05D2250/183—Two-dimensional patterned zigzag
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/501—Elasticity

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)
JP2013034084A 2012-04-30 2013-02-25 タービンシステムの移行ダクト用の重畳シール Expired - Fee Related JP6186133B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/459,533 2012-04-30
US13/459,533 US9038394B2 (en) 2012-04-30 2012-04-30 Convolution seal for transition duct in turbine system

Publications (3)

Publication Number Publication Date
JP2013231426A JP2013231426A (ja) 2013-11-14
JP2013231426A5 JP2013231426A5 (enExample) 2016-04-07
JP6186133B2 true JP6186133B2 (ja) 2017-08-23

Family

ID=47826934

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013034084A Expired - Fee Related JP6186133B2 (ja) 2012-04-30 2013-02-25 タービンシステムの移行ダクト用の重畳シール

Country Status (5)

Country Link
US (1) US9038394B2 (enExample)
EP (1) EP2660427B1 (enExample)
JP (1) JP6186133B2 (enExample)
CN (1) CN103375261B (enExample)
RU (1) RU2013108685A (enExample)

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US10082085B2 (en) * 2013-12-17 2018-09-25 Rolls-Royce North American Technologies Inc. Seal for gas turbine engines
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WO2015199693A1 (en) * 2014-06-26 2015-12-30 Siemens Energy, Inc. Converging flow joint insert system at an intersection between adjacent transition duct bodljs
US9771813B2 (en) * 2014-06-26 2017-09-26 Siemens Energy, Inc. Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine
US20160033134A1 (en) * 2014-08-01 2016-02-04 General Electric Company Seal in combustor nozzle of gas turbine engine
US10132175B2 (en) 2014-10-07 2018-11-20 Siemens Energy, Inc. Arrangement for a gas turbine combustion engine
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US9810434B2 (en) * 2016-01-21 2017-11-07 Siemens Energy, Inc. Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine
US10227883B2 (en) * 2016-03-24 2019-03-12 General Electric Company Transition duct assembly

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Also Published As

Publication number Publication date
CN103375261B (zh) 2016-09-07
RU2013108685A (ru) 2014-09-10
CN103375261A (zh) 2013-10-30
JP2013231426A (ja) 2013-11-14
EP2660427A1 (en) 2013-11-06
EP2660427B1 (en) 2017-02-22
US9038394B2 (en) 2015-05-26
US20130283818A1 (en) 2013-10-31

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