METHOD OF CONTROLLING AIRCRAFT ENGINE CAPACITIVE IGNITION SYSTEM Russian patent published in 2012 - IPC F23Q23/00 F02P17/00 

Abstract RU 2463523 C1

FIELD: engines and pumps.

SUBSTANCE: proposed method comprises measuring time interval between reservoir capacitor discharge current sequential pulses that follows to ignition plug. Time interval exceeding preset magnitude allows deciding on ignition system integrity. Note here that measured is the time interval between discharge current pulses caused solely by commutation of power accumulated at reservoir capacitor that exceeds check magnitude.

EFFECT: higher validity of control, condition-based operation.

2 dwg

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RU2463522C1

RU 2 463 523 C1

Authors

Murysev Andrej Nikolaevich

Krasnov Aleksandr Vladimirovich

Raspopov Evgenij Viktorovich

Dates

2012-10-10Published

2011-02-04Filed