Internal-combustion engines – Starting device – For airplane
Patent
1974-07-24
1976-05-18
Myhre, Charles J.
Internal-combustion engines
Starting device
For airplane
261 39D, 261 39B, F02N 1700
Patent
active
039570266
ABSTRACT:
A carburetor for an internal combustion engine is provided with auxiliary fuel means for continuously regulating the fuel air ratio from a first, cold start condition to a second, normal run condition. The auxiliary fuel means includes a vacuum operated metering system to provide the additional fuel required for starting and running the engine untile the engine reaches normal operating temperature, and a combination shut-off valve and air bleed. In the preferred embodiment, the air bleed is actuated by manifold pressure overcoming the closing force of a thermostatic coil, and is open whenever the engine starts. The air bleed increases air input to the auxiliary fuel supply, thereby reducing fuel richness after start. A temperature sensitive element such as a bimetal coil is utilized to operate the shut-off valve and completely closes the auxiliary fuel means input to the engine at some predetermined temperature.
REFERENCES:
patent: 2074471 (1937-03-01), Holley et al.
patent: 2264996 (1942-12-01), Messinger
patent: 2675792 (1954-04-01), Brown et al.
patent: 3249345 (1966-05-01), Gast
patent: 3278171 (1966-10-01), Carlson
patent: 3642256 (1972-02-01), Phelps
patent: 3706444 (1972-12-01), Masaki et al.
Hardwick Ralph G.
Winkley Jerry H.
Liles James D.
Myhre Charles J.
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