Electricity: electrical systems and devices – Igniting systems – For electric spark ignition
Reexamination Certificate
2006-10-31
2006-10-31
Sircus, Brian (Department: 2836)
Electricity: electrical systems and devices
Igniting systems
For electric spark ignition
C361S256000, C361S257000
Reexamination Certificate
active
07130180
ABSTRACT:
A partitioned exciter system for use with an igniter in an aircraft engine. The exciter has low-energy charging circuit and a high-energy discharge circuit that are remotely located from each other and that are connected by a low-energy coaxial cable. The charging circuit can be located within the aircraft fuselage and the discharge circuit mounted at the engine. The discharge circuit contains passive components that do not need special environmental protection, and the remotely located charging circuit can utilize existing electrical circuitry protection measures already in place in the fuselage to protect against lightning and other potentially-damaging environmental factors. Also disclosed is a housing arrangement for the discharge circuit that allows it to be directly attached to the igniter.
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Srtandard Handbook for Electrical Engineers, 1968, McGraw Hill, Inc., pp. 13-2, 13-3.
Champion Aerospace Inc.
Kitov Z
Reising Ethington Barnes Kisselle P.C.
Sircus Brian
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