BE892362A - Systeme a combustion catalytique pour turbine a gaz fixe - Google Patents

Systeme a combustion catalytique pour turbine a gaz fixe

Info

Publication number
BE892362A
BE892362A BE0/207469A BE207469A BE892362A BE 892362 A BE892362 A BE 892362A BE 0/207469 A BE0/207469 A BE 0/207469A BE 207469 A BE207469 A BE 207469A BE 892362 A BE892362 A BE 892362A
Authority
BE
Belgium
Prior art keywords
gas turbine
combustion system
catalytic combustion
fixed gas
fixed
Prior art date
Application number
BE0/207469A
Other languages
English (en)
Inventor
P E Scheihing
J A Laurelli
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 BE892362A publication Critical patent/BE892362A/fr

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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00—Manufacture
    • F05B2230/60—Assembly methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00—Manufacture
    • F05B2230/60—Assembly methods
    • F05B2230/604—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins
    • F05B2230/606—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins using maintaining alignment while permitting differential dilatation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
BE0/207469A 1981-03-05 1982-03-04 Systeme a combustion catalytique pour turbine a gaz fixe BE892362A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/240,716 US4413470A (en) 1981-03-05 1981-03-05 Catalytic combustion system for a stationary combustion turbine having a transition duct mounted catalytic element

Publications (1)

Publication Number Publication Date
BE892362A true BE892362A (fr) 1982-09-06

Family

ID=22907656

Family Applications (1)

Application Number Title Priority Date Filing Date
BE0/207469A BE892362A (fr) 1981-03-05 1982-03-04 Systeme a combustion catalytique pour turbine a gaz fixe

Country Status (13)

Country Link
US (1) US4413470A (fr)
JP (1) JPS5924331B2 (fr)
AU (1) AU559236B2 (fr)
BE (1) BE892362A (fr)
BR (1) BR8201077A (fr)
CA (1) CA1167264A (fr)
CH (1) CH647063A5 (fr)
GB (1) GB2094172B (fr)
IN (1) IN155659B (fr)
IT (1) IT8219961A0 (fr)
MX (1) MX155529A (fr)
NL (1) NL8200671A (fr)
ZA (1) ZA82974B (fr)

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TW534945B (en) * 2000-11-13 2003-06-01 Catalytica Energy Sys Inc Thermally tolerant support structure for a catalytic combustion catalyst
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US6775989B2 (en) 2002-09-13 2004-08-17 Siemens Westinghouse Power Corporation Catalyst support plate assembly and related methods for catalytic combustion
US7093837B2 (en) * 2002-09-26 2006-08-22 Siemens Westinghouse Power Corporation Turbine spring clip seal
ITMI20031673A1 (it) * 2003-08-28 2005-02-28 Nuovo Pignone Spa Sistema di fissaggio di un tubo di fiamma o "liner".
US7065873B2 (en) 2003-10-28 2006-06-27 Capstone Turbine Corporation Recuperator assembly and procedures
US7147050B2 (en) 2003-10-28 2006-12-12 Capstone Turbine Corporation Recuperator construction for a gas turbine engine
US8015818B2 (en) * 2005-02-22 2011-09-13 Siemens Energy, Inc. Cooled transition duct for a gas turbine engine
US7377116B2 (en) * 2005-04-28 2008-05-27 Siemens Power Generation, Inc. Gas turbine combustor barrier structures for spring clips
US7513098B2 (en) 2005-06-29 2009-04-07 Siemens Energy, Inc. Swirler assembly and combinations of same in gas turbine engine combustors
US7421842B2 (en) * 2005-07-18 2008-09-09 Siemens Power Generation, Inc. Turbine spring clip seal
US7681403B2 (en) 2006-04-13 2010-03-23 General Electric Company Forward sleeve retainer plate and method
US8141370B2 (en) * 2006-08-08 2012-03-27 General Electric Company Methods and apparatus for radially compliant component mounting
US7665960B2 (en) * 2006-08-10 2010-02-23 United Technologies Corporation Turbine shroud thermal distortion control
US7930891B1 (en) 2007-05-10 2011-04-26 Florida Turbine Technologies, Inc. Transition duct with integral guide vanes
JP5010521B2 (ja) * 2008-03-28 2012-08-29 三菱重工業株式会社 燃焼器尾筒案内治具及びガスタービンの燃焼器の取り外し方法、並びに製造方法
US20100050649A1 (en) * 2008-09-04 2010-03-04 Allen David B Combustor device and transition duct assembly
US9074005B2 (en) * 2009-01-02 2015-07-07 Washington State University Compositions and methods for modulating plant disease resistance and immunity
US20110271688A1 (en) * 2010-05-06 2011-11-10 General Electric Company Reduced Pressure Loss Transition Support
US8448444B2 (en) 2011-02-18 2013-05-28 General Electric Company Method and apparatus for mounting transition piece in combustor
AU2012359391A1 (en) * 2011-12-27 2014-07-17 Kawasaki Jukogyo Kabushiki Kaisha Catalytic combustor in gas turbine engine
US9416969B2 (en) 2013-03-14 2016-08-16 Siemens Aktiengesellschaft Gas turbine transition inlet ring adapter
US20150159873A1 (en) * 2013-12-10 2015-06-11 General Electric Company Compressor discharge casing assembly
US10215418B2 (en) * 2014-10-13 2019-02-26 Ansaldo Energia Ip Uk Limited Sealing device for a gas turbine combustor
EP3088691B1 (fr) * 2015-04-27 2019-06-19 Ansaldo Energia Switzerland AG Procédé de démontage d'une turbine à gaz
RU2626180C2 (ru) * 2015-10-01 2017-07-24 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Выносная камера сгорания
US10520193B2 (en) 2015-10-28 2019-12-31 General Electric Company Cooling patch for hot gas path components
JP6563312B2 (ja) * 2015-11-05 2019-08-21 川崎重工業株式会社 ガスタービンエンジンの抽気構造
US10641491B2 (en) 2016-03-25 2020-05-05 General Electric Company Cooling of integrated combustor nozzle of segmented annular combustion system
US10830442B2 (en) 2016-03-25 2020-11-10 General Electric Company Segmented annular combustion system with dual fuel capability
US11428413B2 (en) 2016-03-25 2022-08-30 General Electric Company Fuel injection module for 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
US10605459B2 (en) 2016-03-25 2020-03-31 General Electric Company Integrated combustor nozzle for a segmented annular combustion system
US10563869B2 (en) 2016-03-25 2020-02-18 General Electric Company Operation and turndown of a segmented annular combustion system
US10584880B2 (en) 2016-03-25 2020-03-10 General Electric Company Mounting of integrated combustor nozzles in a segmented annular combustion system
US10641176B2 (en) 2016-03-25 2020-05-05 General Electric Company Combustion system with panel fuel injector
US10520194B2 (en) 2016-03-25 2019-12-31 General Electric Company Radially stacked fuel injection module for a segmented annular combustion system
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
RU2698542C1 (ru) * 2018-11-15 2019-08-28 Публичное Акционерное Общество "Одк-Сатурн" Узел промежуточного корпуса газотурбинного двигателя
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
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
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages

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DE2216644A1 (de) * 1972-04-07 1973-10-11 Kali Chemie Ag Elastische halterung fuer keramische monolithische katalysatorkoerper
US4004888A (en) * 1972-04-07 1977-01-25 Kali-Chemie Aktiengesellschaft Exhaust gas cleaning arrangement with a resiliently supported monolithic ceramic catalyzer
DE7541252U (de) * 1975-12-24 1976-04-29 Paul Gillet Gmbh, 6732 Edenkoben Vorrichtung zum reinigen der abgase von brennkraftmaschinen
US4072007A (en) * 1976-03-03 1978-02-07 Westinghouse Electric Corporation Gas turbine combustor employing plural catalytic stages
US4155980A (en) * 1976-06-19 1979-05-22 Zeuna-Starker Kg Apparatus for catalytic purifying the effluent gases of internal combustion engines
CH643050A5 (de) * 1979-10-01 1984-05-15 Proizv Ob Nevsky Z Im V I Gasturbinentriebwerk mit ringbrennkammer.

Also Published As

Publication number Publication date
CH647063A5 (fr) 1984-12-28
US4413470A (en) 1983-11-08
GB2094172A (en) 1982-09-15
IN155659B (fr) 1985-02-16
JPS5924331B2 (ja) 1984-06-08
AU8043082A (en) 1982-09-09
MX155529A (es) 1988-03-24
BR8201077A (pt) 1983-01-11
NL8200671A (nl) 1982-10-01
ZA82974B (en) 1983-03-30
AU559236B2 (en) 1987-03-05
JPS57161423A (en) 1982-10-05
GB2094172B (en) 1984-12-19
IT8219961A0 (it) 1982-03-04
CA1167264A (fr) 1984-05-15

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Legal Events

Date Code Title Description
RE Patent lapsed

Owner name: WESTINGHOUSE ELECTRIC CORP.

Effective date: 19900331