DE69016943T2 - Steuervorrichtung einer Gasturbine mit optimiertem Zündzeitpunkt. - Google Patents

Steuervorrichtung einer Gasturbine mit optimiertem Zündzeitpunkt.

Info

Publication number
DE69016943T2
DE69016943T2 DE69016943T DE69016943T DE69016943T2 DE 69016943 T2 DE69016943 T2 DE 69016943T2 DE 69016943 T DE69016943 T DE 69016943T DE 69016943 T DE69016943 T DE 69016943T DE 69016943 T2 DE69016943 T2 DE 69016943T2
Authority
DE
Germany
Prior art keywords
control device
gas turbine
ignition timing
optimized ignition
optimized
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
DE69016943T
Other languages
English (en)
Other versions
DE69016943D1 (de
Inventor
Stephen Eugene Mumford
William Lawrence Mccarty
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.)
CBS Corp
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
Application granted granted Critical
Publication of DE69016943D1 publication Critical patent/DE69016943D1/de
Publication of DE69016943T2 publication Critical patent/DE69016943T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
DE69016943T 1989-11-20 1990-10-19 Steuervorrichtung einer Gasturbine mit optimiertem Zündzeitpunkt. Expired - Fee Related DE69016943T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/439,112 US5103629A (en) 1989-11-20 1989-11-20 Gas turbine control system having optimized ignition air flow control

Publications (2)

Publication Number Publication Date
DE69016943D1 DE69016943D1 (de) 1995-03-23
DE69016943T2 true DE69016943T2 (de) 1995-07-06

Family

ID=23743341

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69016943T Expired - Fee Related DE69016943T2 (de) 1989-11-20 1990-10-19 Steuervorrichtung einer Gasturbine mit optimiertem Zündzeitpunkt.

Country Status (7)

Country Link
US (1) US5103629A (de)
EP (1) EP0429840B1 (de)
JP (1) JPH03179134A (de)
KR (1) KR0159930B1 (de)
AU (1) AU630514B2 (de)
CA (1) CA2030268A1 (de)
DE (1) DE69016943T2 (de)

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JP3327772B2 (ja) * 1996-05-24 2002-09-24 三菱重工業株式会社 燃焼器の火炎検知器の掃除方法及び装置
US6334398B1 (en) * 2000-04-28 2002-01-01 Tokyo Electron Limited Variable gap stop which can be used in a semiconductor processing device
US6513318B1 (en) 2000-11-29 2003-02-04 Hybrid Power Generation Systems Llc Low emissions gas turbine engine with inlet air heating
DE10119625B4 (de) * 2001-04-20 2004-04-08 Wobben, Aloys, Dipl.-Ing. Verfahren zur Steuerung einer Windenergieanlage
US6516263B1 (en) 2001-08-02 2003-02-04 Honeywell Power Systems Inc. Adaptive flame-out prevention
US6762512B2 (en) * 2002-05-10 2004-07-13 Siemens Westinghourse Power Corporation Methods for starting a combustion turbine and combustion turbine generator configured to implement same methods
US6923003B2 (en) * 2002-09-13 2005-08-02 Siemens Westinghouse Power Corporation Power generating apparatus having combustion turbine inlet air flow temperature sensor for sensing a drybulb temperature and related methods
US6775988B2 (en) 2002-09-13 2004-08-17 Siemens Westinghouse Power Corproation Combustion turbine having inlet air flow temperature sensor and related methods
US7310950B2 (en) * 2002-09-13 2007-12-25 Siemens Power Generation, Inc. Inlet airflow cooling control for a power generating system
US20040114666A1 (en) * 2002-12-17 2004-06-17 Hardwicke Canan Uslu Temperature sensing structure, method of making the structure, gas turbine engine and method of controlling temperature
US7386982B2 (en) * 2004-10-26 2008-06-17 General Electric Company Method and system for detecting ignition failure in a gas turbine engine
US7185538B2 (en) * 2004-11-12 2007-03-06 Honeywell International Inc. Methods and systems for sensing air vehicle airspeed
US7191084B2 (en) * 2005-04-20 2007-03-13 General Electric Company Method and apparatus for gas turbine engine ignition systems
CN101598067B (zh) * 2009-07-10 2013-09-18 哈尔滨东安发动机（集团）有限公司 燃气轮机自动起动的控制方法
US8925328B2 (en) * 2009-10-26 2015-01-06 Siemens Energy, Inc. Gas turbine starting process
US20120006032A1 (en) * 2010-07-06 2012-01-12 General Electric Company Systems, methods, and apparatus for confirming ignition in a gas turbine
US8355819B2 (en) 2010-10-05 2013-01-15 General Electric Company Method, apparatus and system for igniting wide range of turbine fuels
US9058029B2 (en) * 2011-03-31 2015-06-16 Brad Radl System and method for creating a graphical control programming environment
FR2980236B1 (fr) * 2011-09-20 2017-02-03 Ge Energy Products France Snc Procede et systeme de commande d'arret d'une turbine a gaz.
US20130167549A1 (en) * 2011-12-29 2013-07-04 Chad M. Holcomb Compressor guide vane and pilot control for gas turbine engine
CN104204569B (zh) * 2012-04-04 2017-08-25 开利公司 多轴磁轴承和对具有主动开关拓扑的磁轴承的控制
US20140102113A1 (en) * 2012-06-15 2014-04-17 General Electric Company Exhaust heat recovery for a gas turbine system
US9353691B2 (en) * 2012-12-18 2016-05-31 General Electric Company Fuel routing system of a gas turbine engine and method of routing fuel
US9850823B2 (en) * 2013-12-26 2017-12-26 Siemens Aktiengesellschaft Control system and method for controlling a gas turbine engine during transients
US9507365B2 (en) 2014-06-24 2016-11-29 Woodward, Inc. Adaptive PID control system for industrial turbines
US10508601B2 (en) 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine
US10174678B2 (en) 2016-02-12 2019-01-08 United Technologies Corporation Bowed rotor start using direct temperature measurement
US9664070B1 (en) 2016-02-12 2017-05-30 United Technologies Corporation Bowed rotor prevention system
US10436064B2 (en) 2016-02-12 2019-10-08 United Technologies Corporation Bowed rotor start response damping system
US10508567B2 (en) 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory
US10125691B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor start using a variable position starter valve
US10125636B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor prevention system using waste heat
US10443505B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine
US10040577B2 (en) 2016-02-12 2018-08-07 United Technologies Corporation Modified start sequence of a gas turbine engine
US10443507B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Gas turbine engine bowed rotor avoidance system
US10539079B2 (en) 2016-02-12 2020-01-21 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
US10598047B2 (en) 2016-02-29 2020-03-24 United Technologies Corporation Low-power bowed rotor prevention system
US10787933B2 (en) 2016-06-20 2020-09-29 Raytheon Technologies Corporation Low-power bowed rotor prevention and monitoring system
US10358936B2 (en) 2016-07-05 2019-07-23 United Technologies Corporation Bowed rotor sensor system
US10384791B2 (en) 2016-07-21 2019-08-20 United Technologies Corporation Cross engine coordination during gas turbine engine motoring
US10618666B2 (en) 2016-07-21 2020-04-14 United Technologies Corporation Pre-start motoring synchronization for multiple engines
EP3273006B1 (de) 2016-07-21 2019-07-03 United Technologies Corporation Verwendung eines alternierenden anlassers während des anfahrens mit mehreren motoren
US10221774B2 (en) 2016-07-21 2019-03-05 United Technologies Corporation Speed control during motoring of a gas turbine engine
EP3273016B1 (de) 2016-07-21 2020-04-01 United Technologies Corporation Koordination während des anlassens eines gasturbinenmotors
US10787968B2 (en) 2016-09-30 2020-09-29 Raytheon Technologies Corporation Gas turbine engine motoring with starter air valve manual override
US10443543B2 (en) 2016-11-04 2019-10-15 United Technologies Corporation High compressor build clearance reduction
US10823079B2 (en) 2016-11-29 2020-11-03 Raytheon Technologies Corporation Metered orifice for motoring of a gas turbine engine
KR102123573B1 (ko) * 2018-12-20 2020-06-16 (주)고려엔지니어링 점화 장치 상태 감시 시스템
CN111963323B (zh) * 2020-07-29 2022-08-02 东方电气自动控制工程有限公司 一种燃气轮机升速过程中的燃料控制方法
CN111927636A (zh) * 2020-07-31 2020-11-13 中国航发贵阳发动机设计研究所 一种航空发动机起动过程涡轮后温度限制方法

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GB1090143A (en) * 1965-04-07 1967-11-08 Hawker Siddeley Dynamics Ltd Improvements in or relating to electrical control systems for engines
US3470691A (en) * 1968-06-17 1969-10-07 Avco Corp Automatic starting and protection system for a gas turbine
CA961920A (en) * 1970-10-20 1975-01-28 John F. Reuther System and method for operating industrial gas turbine apparatus and gas turbine electric power plants preferably with a digital computer control system
GB1415681A (en) * 1972-06-24 1975-11-26 Rolls Royce Flame-out control in gas turbine engine
US4019315A (en) * 1973-06-20 1977-04-26 Westinghouse Electric Corporation Gas turbine power plant control apparatus including a temperature reset starting control system and an ignition pressure control system
US4245462A (en) * 1978-11-29 1981-01-20 The Bendix Corporation Starting system for a turbine engine
JPS6125896A (ja) * 1984-07-17 1986-02-04 松下電器産業株式会社 ペン式多色記録装置の色換え装置

Also Published As

Publication number Publication date
KR0159930B1 (ko) 1998-12-15
AU6496590A (en) 1991-05-23
CA2030268A1 (en) 1991-05-21
KR910010042A (ko) 1991-06-28
US5103629A (en) 1992-04-14
EP0429840B1 (de) 1995-02-15
JPH03179134A (ja) 1991-08-05
EP0429840A1 (de) 1991-06-05
DE69016943D1 (de) 1995-03-23
AU630514B2 (en) 1992-10-29

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee