Invention Grant
- Patent Title: Ignition unit for turbojet engine
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Application No.: US14386656Application Date: 2013-03-22
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Publication No.: US09915207B2Publication Date: 2018-03-13
- Inventor: Christian Schaeffer , David Gino Stifanic , Bertrand Boedot
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1252648 20120323
- International Application: PCT/EP2013/056119 WO 20130322
- International Announcement: WO2013/139974 WO 20130926
- Main IPC: F02C7/266
- IPC: F02C7/266 ; F02P15/00 ; F02P15/02 ; F02P3/08 ; F02P5/15

Abstract:
An ignition unit for a turbojet engine, including: an electrical power supply, a single control channel to receive a control signal from a computer, a main sparkplug ignition channel to energize at least one main sparkplug of a main combustion chamber, and an afterburner sparkplug ignition channel to energize at least one afterburner sparkplug of an afterburner chamber. The ignition unit is configured, in response to pulsed controls on the single control channel, to selectively activate the main sparkplug ignition channel or the afterburner sparkplug ignition channel.
Public/Granted literature
- US20150033699A1 IGNITION UNIT FOR TURBOJET ENGINE Public/Granted day:2015-02-05
Information query
IPC分类: