Auxiliary ignition system and method for aircraft engines

Details Auxiliary ignition system and method for aircraft engines Auxiliary ignition system and method for aircraft engines

1993-03-31

1994-07-26

Dolinar, Andrew M.

Internal-combustion engines

Combustion chamber means combined with air-fuel mixture...

1231795, 123639, 123640, F02P 108

Patent

active

053319354

ABSTRACT:
An auxiliary ignition system comprising a first magneto having a normal operating mode and a start-up mode, and a second magneto having a normal operating mode and a start-up mode. A primary starter switch is operably wired to the first and second magnetos. Engagement of the primary starter switch activates the second magneto start-up mode and the first magneto start-up mode. Auxiliary ignition switches are operably connected to the primary starter switch wiring such that engagement of the auxiliary ignition switches after engagement of the starter switch causes the first and second magnetos to initiate engine ignition in their respective normal operating mode.

REFERENCES:
patent: 1862116 (1932-06-01), Hicks
patent: 2380707 (1945-07-01), Sawyer
Teledyne Continental Motors, "The ABC's of the TCM Shower of Sparks Ignition System", Oct. 1990.

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