IT7923668A0 - Sistema di controllo di combustione. - Google Patents

Sistema di controllo di combustione.

Info

Publication number
IT7923668A0
IT7923668A0 IT7923668A IT2366879A IT7923668A0 IT 7923668 A0 IT7923668 A0 IT 7923668A0 IT 7923668 A IT7923668 A IT 7923668A IT 2366879 A IT2366879 A IT 2366879A IT 7923668 A0 IT7923668 A0 IT 7923668A0
Authority
IT
Italy
Prior art keywords
control system
combustion control
combustion
control
Prior art date
Application number
IT7923668A
Other languages
English (en)
Other versions
IT1121814B (it
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT7923668A0 publication Critical patent/IT7923668A0/it
Application granted granted Critical
Publication of IT1121814B publication Critical patent/IT1121814B/it

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
    • F23R3/26—Controlling the air flow
    • 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
    • F05B2200/00—Mathematical features
    • F05B2200/10—Basic functions
    • F05B2200/15—Inverse
IT23668/79A 1978-06-29 1979-06-18 Sistema di controllo di combustione IT1121814B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/920,191 US4255927A (en) 1978-06-29 1978-06-29 Combustion control system

Publications (2)

Publication Number Publication Date
IT7923668A0 true IT7923668A0 (it) 1979-06-18
IT1121814B IT1121814B (it) 1986-04-23

Family

ID=25443326

Family Applications (1)

Application Number Title Priority Date Filing Date
IT23668/79A IT1121814B (it) 1978-06-29 1979-06-18 Sistema di controllo di combustione

Country Status (6)

Country Link
US (1) US4255927A (it)
JP (1) JPS5517095A (it)
BE (1) BE877332A (it)
FR (1) FR2432091A1 (it)
GB (1) GB2024402A (it)
IT (1) IT1121814B (it)

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US4628687A (en) * 1984-05-15 1986-12-16 A/S Kongsberg Vapenfabrikk Gas turbine combustor with pneumatically controlled flow distribution
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US5628182A (en) * 1993-07-07 1997-05-13 Mowill; R. Jan Star combustor with dilution ports in can portions
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JP3116081B2 (ja) * 1994-07-29 2000-12-11 科学技術庁航空宇宙技術研究所長 空気配分制御ガスタービン燃焼器
US5964087A (en) * 1994-08-08 1999-10-12 Tort-Oropeza; Alejandro External combustion engine
US5924276A (en) * 1996-07-17 1999-07-20 Mowill; R. Jan Premixer with dilution air bypass valve assembly
US6070406A (en) * 1996-11-26 2000-06-06 Alliedsignal, Inc. Combustor dilution bypass system
US6220035B1 (en) * 1997-09-15 2001-04-24 Alliedsignal Inc. Annular combustor tangential injection flame stabilizer
US6082093A (en) * 1998-05-27 2000-07-04 Solar Turbines Inc. Combustion air control system for a gas turbine engine
US6095793A (en) * 1998-09-18 2000-08-01 Woodward Governor Company Dynamic control system and method for catalytic combustion process and gas turbine engine utilizing same
US6925809B2 (en) 1999-02-26 2005-08-09 R. Jan Mowill Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities
US6253538B1 (en) 1999-09-27 2001-07-03 Pratt & Whitney Canada Corp. Variable premix-lean burn combustor
WO2001040713A1 (en) 1999-12-03 2001-06-07 Mowill Rolf Jan Cooled premixer exit nozzle for gas turbine combustor and method of operation therefor
US6814568B2 (en) * 2000-07-27 2004-11-09 Foster Wheeler Usa Corporation Superatmospheric combustor for combusting lean concentrations of a burnable gas
US6449956B1 (en) * 2001-04-09 2002-09-17 General Electric Company Bypass air injection method and apparatus for gas turbines
EP1319896A3 (en) 2001-12-14 2004-05-12 R. Jan Mowill Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities
DE10308384A1 (de) * 2003-02-27 2004-09-09 Alstom Technology Ltd Betriebsverfahren für eine Gasturbine
GB0319329D0 (en) * 2003-08-16 2003-09-17 Rolls Royce Plc Variable geometry combustor
GB2405197B (en) * 2003-08-16 2005-09-28 Rolls Royce Plc Fuel injector
JP2005171795A (ja) * 2003-12-09 2005-06-30 Mitsubishi Heavy Ind Ltd ガスタービン燃焼装置
US7047723B2 (en) * 2004-04-30 2006-05-23 Martling Vincent C Apparatus and method for reducing the heat rate of a gas turbine powerplant
WO2006110870A2 (en) * 2005-04-12 2006-10-19 Zilkha Biomass Energy Llc Integrated biomass energy system
US7752850B2 (en) * 2005-07-01 2010-07-13 Siemens Energy, Inc. Controlled pilot oxidizer for a gas turbine combustor
US7870739B2 (en) * 2006-02-02 2011-01-18 Siemens Energy, Inc. Gas turbine engine curved diffuser with partial impingement cooling apparatus for transitions
US7631504B2 (en) * 2006-02-21 2009-12-15 General Electric Company Methods and apparatus for assembling gas turbine engines
US8915086B2 (en) * 2006-08-07 2014-12-23 General Electric Company System for controlling combustion dynamics and method for operating the same
US7921653B2 (en) * 2007-11-26 2011-04-12 General Electric Company Internal manifold air extraction system for IGCC combustor and method
EP2078898A1 (de) * 2008-01-11 2009-07-15 Siemens Aktiengesellschaft Brenner und Verfahren zur Verringerung von selbstinduzierten Flammenschwingungen
GB0815761D0 (en) * 2008-09-01 2008-10-08 Rolls Royce Plc Swirler for a fuel injector
US8099941B2 (en) * 2008-12-31 2012-01-24 General Electric Company Methods and systems for controlling a combustor in turbine engines
US8281596B1 (en) * 2011-05-16 2012-10-09 General Electric Company Combustor assembly for a turbomachine
US20120308947A1 (en) * 2011-06-06 2012-12-06 General Electric Company Combustor having a pressure feed
US8959888B2 (en) * 2011-11-28 2015-02-24 Siemens Energy, Inc. Device to lower NOx in a gas turbine engine combustion system
US9010082B2 (en) * 2012-01-03 2015-04-21 General Electric Company Turbine engine and method for flowing air in a turbine engine
US20130276450A1 (en) * 2012-04-24 2013-10-24 General Electric Company Combustor apparatus for stoichiometric combustion
US9052115B2 (en) * 2012-04-25 2015-06-09 General Electric Company System and method for supplying a working fluid to a combustor
US9631815B2 (en) * 2012-12-28 2017-04-25 General Electric Company System and method for a turbine combustor
US9376961B2 (en) * 2013-03-18 2016-06-28 General Electric Company System for controlling a flow rate of a compressed working fluid to a combustor fuel injector
US9500367B2 (en) * 2013-11-11 2016-11-22 General Electric Company Combustion casing manifold for high pressure air delivery to a fuel nozzle pilot system
GB201414662D0 (en) * 2014-08-19 2014-10-01 Rolls Royce Plc Method of operation of a gas turbine engine
GB201414661D0 (en) * 2014-08-19 2014-10-01 Rolls Royce Plc Gas turbine engine and method of operation
EP3037725B1 (en) * 2014-12-22 2018-10-31 Ansaldo Energia Switzerland AG Mixer for admixing a dilution air to the hot gas flow
US20170191373A1 (en) 2015-12-30 2017-07-06 General Electric Company Passive flow modulation of cooling flow into a cavity
US10337411B2 (en) 2015-12-30 2019-07-02 General Electric Company Auto thermal valve (ATV) for dual mode passive cooling flow modulation
US10337739B2 (en) 2016-08-16 2019-07-02 General Electric Company Combustion bypass passive valve system for a gas turbine
US10712007B2 (en) 2017-01-27 2020-07-14 General Electric Company Pneumatically-actuated fuel nozzle air flow modulator
US10738712B2 (en) 2017-01-27 2020-08-11 General Electric Company Pneumatically-actuated bypass valve
GB201808070D0 (en) 2018-05-18 2018-07-04 Rolls Royce Plc Burner

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US2625011A (en) * 1948-07-31 1953-01-13 Armstrong Siddeley Motors Ltd Igniter for liquid fuel combustion chambers
US2858671A (en) * 1953-01-05 1958-11-04 Phillips Petroleum Co Pressure ratio control of gas turbine bypass during acceleration of turbojet engine
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US3691761A (en) * 1967-11-10 1972-09-19 Squire Ronald Jackson Apparatus for regulation of airflow to flame tubes for gas turbine engines
US3731484A (en) * 1967-11-10 1973-05-08 Lucas Ltd Joseph Apparatus for regulation of airflow to flame tubes for gas turbine engines
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US3975900A (en) * 1972-02-18 1976-08-24 Engelhard Minerals & Chemicals Corporation Method and apparatus for turbine system combustor temperature
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Also Published As

Publication number Publication date
BE877332A (fr) 1979-10-15
JPS5517095A (en) 1980-02-06
IT1121814B (it) 1986-04-23
US4255927A (en) 1981-03-17
FR2432091A1 (fr) 1980-02-22
GB2024402A (en) 1980-01-09

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