Fuel control apparatus for a diesel engine

Internal-combustion engines – Starting device – For airplane

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123139ST, F02N 1700

Patent

active

041471482

ABSTRACT:
A fuel control apparatus for a diesel engine is provided with a control lever which reciprocates between two positions under control of a motor shaft which rotates in one direction only. The control lever connects to a fuel control lever which is moved from a fuel shut-off position to a starting fuel increasing position and then to a normal fuel supply position in accordance with the movement of the control lever. Motor control is effected by relay control in accordance with the positions of a key switch, a pattern switch rotating angularly with the motor shaft, and a switch which determines whether the engine is rotating or at rest.

REFERENCES:
patent: 2879754 (1959-03-01), Von Kienlin et al.
patent: 3311102 (1967-03-01), Voigt
patent: 3533391 (1970-10-01), Lockmuller
patent: 3545418 (1970-12-01), Ballou
patent: 3614945 (1971-10-01), Schlagmuller et al.
patent: 3690768 (1972-09-01), Nagasawa
patent: 3699941 (1972-10-01), Hughes et al.
patent: 3786794 (1974-01-01), Davis
patent: 3792693 (1974-02-01), Luchaco

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