Internal-combustion engines – Starting device – For airplane
Patent
1983-02-16
1984-10-09
Lall, Parshotam S.
Internal-combustion engines
Starting device
For airplane
123198DB, 123491, F02N 1700
Patent
active
044754930
ABSTRACT:
An electronic control (10) for generating control, diagnostic, and fault signals for a diesel engine (12) with a turbocharger (22) and an injection pump (14). The control (10) provides an injection pump control (78), a turbocharger control (80), a fault monitor (82) and a sequencing control (84). These controllers are embodied as a stored program of a microprocessor controlled processor, timing, and memory module (228). The module (228) communicates with an input section receiving analog and discrete inputs via a serial input data line (CRUIN) and further communicates with an output section generating analog and discrete outputs via a serial output data line (CRUOUT).
REFERENCES:
patent: 3656465 (1972-04-01), Frankle
patent: 3913543 (1975-10-01), Richard
patent: 4231073 (1980-10-01), Suchko
patent: 4264898 (1981-04-01), Barman et al.
patent: 4312310 (1982-01-01), Chivilo' et al.
patent: 4328773 (1982-05-01), Woodward
patent: 4338896 (1982-07-01), Papasideris
Fujawa Charles S.
Masteller Sara B.
Decker Ken C.
Lall Parshotam S.
The Bendix Corporation
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