Helicopter rotor and engine control

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Details

364131, 244 1713, G06F 1516

Patent

active

048071293

ABSTRACT:
A Helicopter rotor and engine control apparatus in which the computers used to control the engines and the rotors are linked to exchange performance data and act together to improve the aircraft performance.

REFERENCES:
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patent: 4207168 (1981-05-01), Murphy et al.
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patent: 4488236 (1984-12-01), Morrison et al.
patent: 4493465 (1985-01-01), Howlett et al.
patent: 4504905 (1985-03-01), Burrage
patent: 4590549 (1986-05-01), Burrage et al.
patent: 4628455 (1986-12-01), Skutecki

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