FIELD: aircraft engineering.
SUBSTANCE: proposed device (1) comprises control means (3) to actuate protection function and to automatically control engines (M1 to M4) for them to run at maximum power when starting conditions are satisfied. It comprises also means (8) to suppress protective function initiated only with simultaneous outage of all engines at a time. Note that all engines are arranged on common wing of aircraft.
EFFECT: flight safety, expanded performances.
11 cl, 9 dwg
