JP2017137862A5 - - Google Patents

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Publication number
JP2017137862A5
JP2017137862A5 JP2017009199A JP2017009199A JP2017137862A5 JP 2017137862 A5 JP2017137862 A5 JP 2017137862A5 JP 2017009199 A JP2017009199 A JP 2017009199A JP 2017009199 A JP2017009199 A JP 2017009199A JP 2017137862 A5 JP2017137862 A5 JP 2017137862A5
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JP
Japan
Prior art keywords
coil
trigger
voltage
solid
circuit
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Application number
JP2017009199A
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English (en)
Japanese (ja)
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JP6888961B2 (ja
JP2017137862A (ja
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Publication of JP2017137862A publication Critical patent/JP2017137862A/ja
Publication of JP2017137862A5 publication Critical patent/JP2017137862A5/ja
Application granted granted Critical
Publication of JP6888961B2 publication Critical patent/JP6888961B2/ja
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Anticipated expiration legal-status Critical

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JP2017009199A 2016-01-21 2017-01-23 航空機点火システムに用いられる固体スパーク装置 Active JP6888961B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201662281494P 2016-01-21 2016-01-21
US62/281,494 2016-01-21

Publications (3)

Publication Number Publication Date
JP2017137862A JP2017137862A (ja) 2017-08-10
JP2017137862A5 true JP2017137862A5 (enExample) 2019-10-10
JP6888961B2 JP6888961B2 (ja) 2021-06-18

Family

ID=57906441

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2017009199A Active JP6888961B2 (ja) 2016-01-21 2017-01-23 航空機点火システムに用いられる固体スパーク装置

Country Status (4)

Country Link
US (1) US10030584B2 (enExample)
EP (1) EP3196444B1 (enExample)
JP (1) JP6888961B2 (enExample)
CN (1) CN106988892B (enExample)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3072762B1 (fr) * 2017-10-23 2019-11-08 Airbus Operations (S.A.S.) Systeme d'allumage d'une turbomachine d'aeronef
CN108019284B (zh) * 2017-11-08 2019-11-15 陕西航空电气有限责任公司 飞机发动机点火装置高压放电触发电路
US11913310B2 (en) 2019-03-27 2024-02-27 Hunting Titan, Inc. Solid state dual fire circuit
CN110821681B (zh) * 2019-11-11 2023-01-17 陕西航空电气有限责任公司 一种航空发动机双放电管点火电路限流电阻的定值方法
US11519335B1 (en) 2021-08-27 2022-12-06 Unison Industries, Llc Turbine engine ignition system and method

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2448302A1 (de) * 1973-10-15 1975-04-17 Teledyne Ind Funkenenergiespeicherkondensator- ladeeinrichtung
JPS58117357A (ja) * 1981-12-29 1983-07-12 Kioritz Corp 補器用電力取り出し可能な内燃機関電子点火装置
US5245252A (en) * 1988-11-15 1993-09-14 Frus John R Apparatus and method for providing ignition to a turbine engine
US5754011A (en) * 1995-07-14 1998-05-19 Unison Industries Limited Partnership Method and apparatus for controllably generating sparks in an ignition system or the like
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
JP5683777B2 (ja) 2007-08-20 2015-03-11 チャンピオン・エアロスペース・インコーポレイテッドＣｈａｍｐｉｏｎ Ａｅｒｏｓｐａｃｅ Ｉｎｃ． 高電圧航空機イグニションシステム用スイッチング組立体、およびスイッチング組立体
CN201212441Y (zh) * 2008-05-17 2009-03-25 浙江长进机电有限公司 具备自动限速功能的电容放电式通用汽油机点火系统
CN202772800U (zh) * 2012-06-21 2013-03-06 上海浩亚机电有限公司 一种交流调压器电路
CN202931657U (zh) * 2012-07-29 2013-05-08 绍兴市奇鑫照明技术有限公司 用于无极灯上的镇流器电路
CN202747393U (zh) * 2012-07-30 2013-02-20 咸阳西燃机电设备有限公司 全固态高能电点火装置

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