Internal-combustion engines – Starting device – For airplane
Patent
1985-08-27
1987-06-02
Wolfe, Jr., Willis R.
Internal-combustion engines
Starting device
For airplane
123179H, 123145A, 219497, 219509, F02P 1902, G05D 2319
Patent
active
046694307
ABSTRACT:
Electrical energy being supplied to an electrical heater, typically a glow plug within an internal combustion engine (ICE), is easily and simply controlled by controlling the duty cycle or ON/OFF duration of a switch (10) serially connected between the glow plug (11) and a supply voltage source, for example a vehicular battery (U.sub.Batt). An operational amplifier (15) controls the duty cycle of the switch (10) by comparing a periodically varying voltage (37a) derived from a stabilized frequency or pulse generator (30) with battery voltage (U.sub.Batt) and, at the cross-over points, respectively changing the switching condition of the switch. Upon drop in battery voltage, the switch will be longer in an ON position than at a higher battery voltage, so that the average voltage, over a plurality of cycles, across the glow plug (11), will have a value (U.sub.KEM) which will result in a predetermined temperature thereof.
REFERENCES:
patent: 4300491 (1981-11-01), Hara et al.
patent: 4307689 (1981-12-01), Raeske et al.
patent: 4458639 (1984-07-01), Abe et al.
patent: 4516543 (1985-05-01), Abe et al.
Reinold Martin
Schmidt Peter
Robert & Bosch GmbH
Wolfe, Jr. Willis R.
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