Internal-combustion engines – Starting device – For airplane
Patent
1973-12-10
1976-04-13
Burns, Wendell E.
Internal-combustion engines
Starting device
For airplane
123122G, F02N 1700, F02M 3900
Patent
active
039497232
ABSTRACT:
An intake conduit or manifold for air for combustion engines has an auxiliary burning chamber provided in one of its walls which communicates with the interior of the intake conduit. A valve can establish or terminate communication between the chamber and the conduit in a sense permitting some of the air from the latter to flow into the former. An injector injects vaporized fuel into the burning chamber and a spark plug ignites the fuel so that the heat of combustion is transmitted to air flowing through the intake manifold to thereby preheat such air.
REFERENCES:
patent: 1235255 (1917-07-01), Stewart
patent: 1424394 (1922-08-01), Doolittle
patent: 1602790 (1926-10-01), Tibbetts
patent: 1617605 (1927-02-01), Peterson
patent: 3656465 (1972-04-01), Frankle
Burns Wendell E.
Cox Ronald B.
Robert & Bosch GmbH
Striker Michael J.
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