Start system for internal combustion engines

Internal-combustion engines – Starting device – For airplane

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Details

123180R, 261 34A, F02N 1700

Patent

active

045094713

ABSTRACT:
A carburetor for an internal combustion engine which includes a supplemental fuel chamber and fuel injector valve, manually or remotely actuated, to inject a charge of fuel into the fuel induction chamber of an associated engine and provide a continuing fuel supply to the engine, over and above, the normal carburetor system, to allow the engine to reach a warm-up stage and prevent stalling out until such stage is reached where normal carburetion can take over. Automatic refill and vent valves permit fuel recharge of the supplemental fuel chamber to insure readiness of the chamber for starting at all times.

REFERENCES:
patent: 1974585 (1934-09-01), Prentiss
patent: 2977948 (1961-04-01), Kittler
patent: 3957929 (1976-05-01), Gural et al.
patent: 4216175 (1980-08-01), Schauer
patent: 4285887 (1981-08-01), Akiya
patent: 4390480 (1983-06-01), Noisier

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