AIRCRAFT IGNITION SYSTEM AND METHOD OF OPERATING THE SAME
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United States of America Patent
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Issued Date -
May 9, 2013
app pub date -
Apr 27, 2012
filing date -
Apr 27, 2011
priority date (Note) -
Abandoned
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Abstract
An aircraft ignition system having a power circuit, a control circuit, and a discharge circuit and coupled to the spark plugs of an aircraft engine. The power circuit may include two independent power sources; e.g., alternator power (such as a permanent magnet alternator) and power from aircraft or DC power bus. The control circuit may control one or more aspects of the discharge circuit, e.g., the ignition timing. And the discharge circuit may trigger a capacitive discharge ignition event to the spark plugs.
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