Detection of engine failure in a multi-engine aircraft

Details Detection of engine failure in a multi-engine aircraft Detection of engine failure in a multi-engine aircraft

1986-04-10

1989-03-28

Lall, Parshotam S.

Boots, shoes, and leggings

36443102, 731173, 60 30091, G08B 2100

Patent

active

048170461

ABSTRACT:
Primary logic (116-128) for engine failure detection in a multi-engine aircraft is based on thresholds for engine torque (Q), gas generator speed (NG), power turbine inner stage temperature (T5), power turbine speed (NF), throttle setting (PLA), and throttle manipulation (PLADOT).

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patent: 4500966 (1985-02-01), Zagranski et al.
patent: 4546353 (1985-10-01), Stockton
patent: 4619110 (1986-10-01), Moore

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