Internal combustion engine system

Internal-combustion engines – Starting device – For airplane

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Details

123179H, 123180R, 123122E, 123122F, F02N 1700, F02M 3100

Patent

active

042023084

ABSTRACT:
An engine system includes a starting aid which is mounted in the air inlet manifold of the engine and is supplied with fuel from a fuel chamber to assist starting of the engine. The engine includes a fuel injection nozzle which is supplied with fuel at high pressure by means of a pump. The leakage fuel from the nozzle is utilized to recharge the chamber with fuel during running of the engine and the chamber is provided with an overflow connection back to a source of fuel.

REFERENCES:
patent: 2905165 (1959-09-01), Hall
patent: 2995890 (1961-08-01), Dolza
patent: 3091282 (1963-05-01), Curzon
patent: 3353520 (1967-11-01), Haag
patent: 3379184 (1968-04-01), Wolf
patent: 3620424 (1971-11-01), Grigsby
patent: 3767173 (1973-10-01), Ishii
patent: 3872851 (1975-03-01), Matsumoto et al.
patent: 3943901 (1976-03-01), Takahashi et al.

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