Internal-combustion engines – Starting device – For airplane
Patent
1980-12-22
1983-05-17
Cuchlinski, Jr., William A.
Internal-combustion engines
Starting device
For airplane
F02N 1700
Patent
active
043835066
ABSTRACT:
An engine rotation speed control system which comprises an actuator for prescribing the recovery position of a throttle valve, a recovery position sensor for detecting that the throttle valve is returned to the recovery position, an idle speed control unit for controlling the engine to a predetermined idling speed, and a negative pressure restricting unit for controlling the throttle actuator such that reduction in intake negative pressure to below a predetermined negative pressure is prevented. When the throttle valve returns to the recovery position with the engine speed in excess of an upper limit of the idling speed, the actuator is controlled by the negative pressure restricting unit. When the engine speed falls below the upper limit, the idle speed control unit is actuated. Upon engine starting the actuator is set such that the opening degree of the throttle valve suitable for the engine starting is obtained before the starter starts operating.
REFERENCES:
patent: 3081846 (1963-03-01), Lift
patent: 3266473 (1966-08-01), Rhodes
patent: 3621824 (1971-11-01), Burnia et al.
patent: 3964457 (1976-06-01), Coscia
patent: 4212272 (1980-07-01), Hawk
Atago Takeshi
Manaka Toshio
Cuchlinski Jr. William A.
Hitachi , Ltd.
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