Capacitor discharge ignition system

Electric lamp and discharge devices: systems – Periodic switch in the supply circuit – Silicon controlled rectifier ignition

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Details

315209R, 315247, 315278, 315279, 123148E, 315241R, H05B 3702, H05B 3904, H05B 4136

Patent

active

040271986

ABSTRACT:
A capacitor discharge ignition system for a jet engine which has a relatively high power factor at the transformer input without exceeding the one ampere current rating required in jet ignition systems at the desired power level. A specially designed power transformer (10 ) has a capacitor (3) connected across closely coupled primary and tertiary windings (11 and 12).

REFERENCES:
patent: 2473917 (1949-06-01), Steinert et al.
patent: 2791726 (1957-05-01), Feinberg
patent: 2864035 (1958-12-01), Davis
patent: 3080505 (1963-03-01), Eppert
patent: 3427501 (1969-02-01), Laub et al.
patent: 3450972 (1969-06-01), Linkroum
patent: 3780347 (1973-12-01), Riesland
patent: 3890562 (1975-06-01), West

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