HK1057387A1 - Exciter circuit with ferro-resonant transformer network for an ignition system of a turbine engine - Google Patents

Exciter circuit with ferro-resonant transformer network for an ignition system of a turbine engine

Info

Publication number
HK1057387A1
HK1057387A1 HK03108533A HK03108533A HK1057387A1 HK 1057387 A1 HK1057387 A1 HK 1057387A1 HK 03108533 A HK03108533 A HK 03108533A HK 03108533 A HK03108533 A HK 03108533A HK 1057387 A1 HK1057387 A1 HK 1057387A1
Authority
HK
Hong Kong
Prior art keywords
ferro
turbine engine
ignition system
resonant transformer
exciter circuit
Prior art date
Application number
HK03108533A
Other languages
English (en)
Inventor
John Joseph Costello
Original Assignee
Champion Aerospace Inc
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 Champion Aerospace Inc filed Critical Champion Aerospace Inc
Publication of HK1057387A1 publication Critical patent/HK1057387A1/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02PIGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P3/00Other installations
    • F02P3/06Other installations having capacitive energy storage
    • F02P3/08Layout of circuits
    • F02P3/0876Layout of circuits the storage capacitor being charged by means of an energy converter (DC-DC converter) or of an intermediate storage inductance
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/26Starting; Ignition
    • F02C7/264Ignition
    • F02C7/266Electric
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02PIGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P15/00Electric spark ignition having characteristics not provided for in, or of interest apart from, groups F02P1/00 - F02P13/00 and combined with layout of ignition circuits
    • F02P15/001Ignition installations adapted to specific engine types
    • F02P15/003Layout of ignition circuits for gas turbine plants
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
HK03108533A 2001-10-10 2003-11-21 Exciter circuit with ferro-resonant transformer network for an ignition system of a turbine engine HK1057387A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/974,074 US6603216B2 (en) 2001-10-10 2001-10-10 Exciter circuit with ferro-resonant transformer network for an ignition system of a turbine engine

Publications (1)

Publication Number Publication Date
HK1057387A1 true HK1057387A1 (en) 2004-04-02

Family

ID=25521555

Family Applications (1)

Application Number Title Priority Date Filing Date
HK03108533A HK1057387A1 (en) 2001-10-10 2003-11-21 Exciter circuit with ferro-resonant transformer network for an ignition system of a turbine engine

Country Status (5)

Country Link
US (1) US6603216B2 (xx)
JP (1) JP4084159B2 (xx)
FR (1) FR2830691B1 (xx)
GB (1) GB2382106B (xx)
HK (1) HK1057387A1 (xx)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE50110759D1 (de) * 2001-09-25 2006-09-28 Abb Schweiz Ag Energieerzeugungseinrichtung
NO322439B1 (no) * 2004-02-03 2006-10-09 Magtech As Fremgangsmåte for spenningsregulering av en krets med en kapasitiv last
US7095601B2 (en) * 2004-08-20 2006-08-22 Hamilton Sundstrand Corporation High energy primary spark ignition system for a gas turbine engine
US7509812B2 (en) * 2004-08-20 2009-03-31 Hamilton Sundstrand Corporation Dual ignition system for a gas turbine engine
US20060071640A1 (en) * 2004-09-30 2006-04-06 Nanotechnologies, Inc. Fast-recovery circuitry and method for a capacitor charging power supply
US7637094B2 (en) * 2005-12-16 2009-12-29 General Electric Company Cooling apparatus for a gas turbine engine igniter lead
DE102006007832A1 (de) * 2006-02-17 2007-08-30 Rolls-Royce Deutschland Ltd & Co Kg Zündanlage für ein Gasturbinentriebwerk
US7965529B2 (en) * 2008-05-13 2011-06-21 Eaton Corporation Voltage source inverter and medium voltage pre-charge circuit therefor
US8266885B2 (en) * 2008-12-23 2012-09-18 General Electric Company Method and systems for adaptive ignition energy
US8117904B2 (en) * 2009-03-31 2012-02-21 Ford Global Technologies, Llc System and method for evaluating an integrated coil on plug ignition system
US20110186096A1 (en) * 2010-02-02 2011-08-04 Gas Turbine Efficiency Sweden Ab Aircraft maintenance unit
DE102010045174B4 (de) * 2010-09-04 2012-06-21 Borgwarner Beru Systems Gmbh Schaltungsanordnung für eine HF-Zündung von Verbrennungsmotoren
US20130181688A1 (en) * 2010-10-06 2013-07-18 Raven Energy Alternatives, Llc System and method for variable speed generation of controlled high-voltage dc power
DE102012200633A1 (de) * 2012-01-17 2013-07-18 Man Diesel & Turbo Se Kapazitives Zündsystem
FR2988435B1 (fr) * 2012-03-23 2016-03-18 Snecma Boitier d'allumage pour turboreacteur a segregation d'allumage
US9593660B2 (en) 2014-03-12 2017-03-14 Unison Industries, Llc Method and apparatus of charging an engine ignition system
US9399954B2 (en) 2014-03-17 2016-07-26 Unison Industries, Llc Ignition exciter discharge switch
US10581284B2 (en) * 2014-12-16 2020-03-03 Samsung Electronics Co., Ltd. Wireless charger and wireless power receiver
US10590887B2 (en) 2016-05-20 2020-03-17 Alphaport, Inc. Spark exciter operational unit
US10473033B2 (en) * 2016-10-19 2019-11-12 Honeywell International Inc. Gas turbine engine
US10801414B2 (en) 2017-01-24 2020-10-13 Honeywell International Inc. Gas turbine engine including a rectifierless electronic control unit and method for supplying power to same
US11682535B2 (en) 2021-03-12 2023-06-20 Essex Industries, Inc. Rocker switch
EP4309200A1 (en) 2021-03-15 2024-01-24 Essex Industries, Inc. Five-position switch
CN114151260A (zh) * 2021-11-08 2022-03-08 四川泛华航空仪表电器有限公司 一种具有状态控制和bit功能的点火装置
US20230340934A1 (en) * 2022-04-25 2023-10-26 Hamilton Sundstrand Corporation Engine ignition systems

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3448732A (en) * 1966-09-06 1969-06-10 August C Weiss Capacitor-discharge electronic ignition system and a method for adjusting the circuit
US3906919A (en) * 1974-04-24 1975-09-23 Ford Motor Co Capacitor discharge ignition system with controlled spark duration
US5245252A (en) 1988-11-15 1993-09-14 Frus John R Apparatus and method for providing ignition to a turbine engine
US5053913A (en) * 1989-02-17 1991-10-01 Unison Industries Limited Partnership Capacitive discharge ignition exciter using scr discharge switches
US5473502A (en) * 1992-09-22 1995-12-05 Simmonds Precision Engine Systems Exciter with an output current multiplier
DE69324981D1 (de) * 1992-09-22 1999-06-24 Unison Ind Lp Erregerkreise und Methoden mit Schutzmassnahmen für Halbleiterschalter
US5488536A (en) * 1993-04-01 1996-01-30 Simmonds Precision Engine Systems, Inc. Exciter circuit using gated switches
CA2128036C (en) * 1993-07-15 2003-11-04 Howard Vincent Bonavia Ignition system using multiple gated switches with variable discharge energy levels and rates
US5656966A (en) 1994-03-09 1997-08-12 Cooper Industries, Inc. Turbine engine ignition exciter circuit including low voltage lockout control
US5654868A (en) * 1995-10-27 1997-08-05 Sl Aburn, Inc. Solid-state exciter circuit with two drive pulses having indendently adjustable durations
US6081074A (en) * 1996-08-30 2000-06-27 Unison Industries, Inc. Method and apparatus for offsetting power draw in a multiple channel system
US5862033A (en) 1997-02-13 1999-01-19 Unison Industries Limited Partnership Exciter circuit
US6104143A (en) * 1999-10-01 2000-08-15 Peabody Engneering Corporation Exciter circuit with solid switch device separated from discharge path
US6758199B2 (en) * 2001-04-05 2004-07-06 Mide Technology Corporation Tuned power ignition system

Also Published As

Publication number Publication date
GB0223241D0 (en) 2002-11-13
GB2382106B (en) 2005-04-13
FR2830691B1 (fr) 2006-11-17
US6603216B2 (en) 2003-08-05
JP2003124024A (ja) 2003-04-25
FR2830691A1 (fr) 2003-04-11
US20030067284A1 (en) 2003-04-10
JP4084159B2 (ja) 2008-04-30
GB2382106A (en) 2003-05-21

Similar Documents

Publication Publication Date Title
GB2382106B (en) Exciter circuit with ferro-resonant transformer network for an ignition system of a turbine engine
GB2336663B (en) Gas-turbine engine combustion system
GB2380692B (en) A system and method for adjusting an air/fuel ratio of an engine
GB2374123B (en) Gas turbine engine system
GB2375513B (en) A mounting arrangement for a gas turbine engine
GB2383409B (en) A method for operating an internal combustion engine
GB2383279B (en) A method and system for an engine
SG121725A1 (en) Dianostic method and system for turbine engines
GB2339307B (en) Method for operating an internal combustion engine
GB9607010D0 (en) Gas turbine engine combustion equipment
GB2379499B (en) Gas turbine engine combustor
GB0025878D0 (en) Gas turbine engine combustion system
GB2380429B (en) A system and method for adjusting the air/fuel ratio of an engine
GB2383278B (en) A method and system for an engine
GB2396880B (en) Method and system for producing an oil and gas mixture through a well
GB2339468B (en) Gas-turbine engine combustion system
GB0225101D0 (en) A method and system for an engine
GB9820226D0 (en) Gas turbine engine casing
GB2366599B (en) Gas turbine engine system
GB2337136B (en) Equipment for regulating an engine
GB0103821D0 (en) Gas turbine engine system
AU2002347660A1 (en) Combustion engine and ignition circuit for a combustion engine
GB2360836B (en) Gas turbine engine combustion system
NO992628L (no) Anordning for etterfylling av en kjölekrets for en undervannsmotor
GB9800782D0 (en) Gas turbine engine

Legal Events

Date Code Title Description
PC Patent ceased (i.e. patent has lapsed due to the failure to pay the renewal fee)

Effective date: 20141008