MX164478B - Mejoras en camara de combustion de turbina de gas con tomas de aire - Google Patents

Mejoras en camara de combustion de turbina de gas con tomas de aire

Info

Publication number
MX164478B
MX164478B MX17785A MX1778589A MX164478B MX 164478 B MX164478 B MX 164478B MX 17785 A MX17785 A MX 17785A MX 1778589 A MX1778589 A MX 1778589A MX 164478 B MX164478 B MX 164478B
Authority
MX
Mexico
Prior art keywords
combustion chamber
gas turbine
air intakes
turbine combustion
intakes
Prior art date
Application number
MX17785A
Other languages
English (en)
Inventor
Stephen Eugene Mumford
Jan Peer Smed
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 MX164478B publication Critical patent/MX164478B/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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/045—Air inlet arrangements using pipes
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
MX17785A 1988-10-07 1989-10-02 Mejoras en camara de combustion de turbina de gas con tomas de aire MX164478B (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/255,577 US4887432A (en) 1988-10-07 1988-10-07 Gas turbine combustion chamber with air scoops

Publications (1)

Publication Number Publication Date
MX164478B true MX164478B (es) 1992-08-19

Family

ID=22968936

Family Applications (1)

Application Number Title Priority Date Filing Date
MX17785A MX164478B (es) 1988-10-07 1989-10-02 Mejoras en camara de combustion de turbina de gas con tomas de aire

Country Status (6)

Country Link
US (1) US4887432A (es)
EP (1) EP0363624B1 (es)
JP (1) JP2554175B2 (es)
CA (1) CA1315994C (es)
DE (1) DE68904280T2 (es)
MX (1) MX164478B (es)

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FR2826102B1 (fr) * 2001-06-19 2004-01-02 Snecma Moteurs Perfectionnements apportes aux chambres de combustion de turbine a gaz
US7421843B2 (en) * 2005-01-15 2008-09-09 Siemens Power Generation, Inc. Catalytic combustor having fuel flow control responsive to measured combustion parameters
GB0601413D0 (en) * 2006-01-25 2006-03-08 Rolls Royce Plc Wall elements for gas turbine engine combustors
FR2899315B1 (fr) * 2006-03-30 2012-09-28 Snecma Configuration d'ouvertures de dilution dans une paroi de chambre de combustion de turbomachine
US8047008B2 (en) * 2008-03-31 2011-11-01 General Electric Company Replaceable orifice for combustion tuning and related method
US20100223930A1 (en) * 2009-03-06 2010-09-09 General Electric Company Injection device for a turbomachine
US20100236248A1 (en) * 2009-03-18 2010-09-23 Karthick Kaleeswaran Combustion Liner with Mixing Hole Stub
US20100269513A1 (en) * 2009-04-23 2010-10-28 General Electric Company Thimble Fan for a Combustion System
RU2519014C2 (ru) * 2010-03-02 2014-06-10 Дженерал Электрик Компани Диффузор для камеры сгорания турбины (варианты) и камера сгорания турбины
US9010123B2 (en) * 2010-07-26 2015-04-21 Honeywell International Inc. Combustors with quench inserts
US8590864B2 (en) * 2010-10-21 2013-11-26 Woodward Fst, Inc. Semi-tubular vane air swirler
EP2463582B1 (en) * 2010-12-10 2019-06-19 Rolls-Royce plc A combustion chamber
US9249679B2 (en) * 2011-03-15 2016-02-02 General Electric Company Impingement sleeve and methods for designing and forming impingement sleeve
US9062884B2 (en) 2011-05-26 2015-06-23 Honeywell International Inc. Combustors with quench inserts
US9360215B2 (en) 2012-04-02 2016-06-07 United Technologies Corporation Combustor having a beveled grommet
US20130283806A1 (en) * 2012-04-26 2013-10-31 General Electric Company Combustor and a method for repairing the combustor
FR2991028B1 (fr) * 2012-05-25 2014-07-04 Snecma Virole de chambre de combustion de turbomachine
DE102012015449A1 (de) * 2012-08-03 2014-02-20 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit Mischluftöffnungen und Luftleitelementen in modularer Bauweise
US9328923B2 (en) * 2012-10-10 2016-05-03 General Electric Company System and method for separating fluids
EP2735796B1 (en) * 2012-11-23 2020-01-01 Ansaldo Energia IP UK Limited Wall of a hot gas path component of a gas turbine and method for enhancing operational behaviour of a gas turbine
US20140208771A1 (en) * 2012-12-28 2014-07-31 United Technologies Corporation Gas turbine engine component cooling arrangement
WO2014197045A2 (en) 2013-03-12 2014-12-11 United Technologies Corporation Active cooling of grommet bosses for a combustor panel of a gas turbine engine
WO2015047509A2 (en) * 2013-08-30 2015-04-02 United Technologies Corporation Vena contracta swirling dilution passages for gas turbine engine combustor
US11112115B2 (en) * 2013-08-30 2021-09-07 Raytheon Technologies Corporation Contoured dilution passages for gas turbine engine combustor
US10648666B2 (en) 2013-09-16 2020-05-12 United Technologies Corporation Angled combustor liner cooling holes through transverse structure within a gas turbine engine combustor
WO2015108584A2 (en) * 2013-10-24 2015-07-23 United Technologies Corporation Passage geometry for gas turbine engine combustor
EP3077640B1 (en) * 2013-12-06 2021-06-02 Raytheon Technologies Corporation Combustor quench aperture cooling
WO2015100346A1 (en) 2013-12-23 2015-07-02 United Technologies Corporation Multi-streamed dilution hole configuration for a gas turbine engine
WO2015147938A2 (en) 2014-01-03 2015-10-01 United Technologies Corporation A cooled grommet for a combustor wall assembly
EP2927595B1 (en) * 2014-04-02 2019-11-13 United Technologies Corporation Grommet assembly and method of design
EP2957833B1 (en) 2014-06-17 2018-10-24 Rolls-Royce Corporation Combustor assembly with chutes
EP2993404B1 (en) * 2014-09-08 2019-03-13 Ansaldo Energia Switzerland AG Dilution gas or air mixer for a combustor of a gas turbine
US20160178199A1 (en) * 2014-12-17 2016-06-23 United Technologies Corporation Combustor dilution hole active heat transfer control apparatus and system
US20160209035A1 (en) * 2015-01-16 2016-07-21 Solar Turbines Incorporated Combustion hole insert with integrated film restarter
DE102016207066A1 (de) * 2016-04-26 2017-10-26 Rolls-Royce Deutschland Ltd & Co Kg Brennkammerschindel einer Gasturbine
US11181273B2 (en) * 2016-09-27 2021-11-23 Siemens Energy Global GmbH & Co. KG Fuel oil axial stage combustion for improved turbine combustor performance
US20180283695A1 (en) * 2017-04-03 2018-10-04 United Technologies Corporation Combustion panel grommet
US20180283689A1 (en) * 2017-04-03 2018-10-04 General Electric Company Film starters in combustors of gas turbine engines
US11137140B2 (en) * 2017-10-04 2021-10-05 Raytheon Technologies Corporation Dilution holes with ridge feature for gas turbine engines
US11255543B2 (en) * 2018-08-07 2022-02-22 General Electric Company Dilution structure for gas turbine engine combustor
US11085639B2 (en) * 2018-12-27 2021-08-10 Rolls-Royce North American Technologies Inc. Gas turbine combustor liner with integral chute made by additive manufacturing process
US11079111B2 (en) * 2019-04-29 2021-08-03 Solar Turbines Incorporated Air tube
CN116265810A (zh) * 2021-12-16 2023-06-20 通用电气公司 利用成形冷却栅栏的旋流器反稀释

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Also Published As

Publication number Publication date
JPH02187520A (ja) 1990-07-23
CA1315994C (en) 1993-04-13
DE68904280T2 (de) 1993-05-06
US4887432A (en) 1989-12-19
EP0363624A1 (en) 1990-04-18
DE68904280D1 (de) 1993-02-18
JP2554175B2 (ja) 1996-11-13
EP0363624B1 (en) 1993-01-07

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