Breakerless ignition system for internal combustion aircraft eng

Internal-combustion engines – High tension ignition system – Retrofit conversion ignition unit

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123424, 123617, F02P 306

Patent

active

055136176

ABSTRACT:
A breakerless ignition system for internal combustion aircraft engines which includes a pair of separately activated Hall effect and amplifier combinations for controlling the timing and the delivery of electrical energy to the spark plugs of the engine in a predetermined sequence.

REFERENCES:
patent: 3765390 (1973-10-01), Loudon et al.
patent: 3906920 (1975-09-01), Hemphill
patent: 4138976 (1979-02-01), Crall
patent: 4235213 (1980-11-01), Jellissen
Article entitled "Magnetos: What Are They" from Light Plane Maintenance of Mar. 1992.
Article entitled "Breaker Point Pointers" from Light Plane Maintenance of Mar. 1992.

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