Engine failure monitor for a multi-engine aircraft having partia

Details Engine failure monitor for a multi-engine aircraft having partia Engine failure monitor for a multi-engine aircraft having partia

1992-10-29

1994-11-08

Harvey, Jack B.

Boots, shoes, and leggings

36443101, 36443102, 36442403, 364508, 731173, G01B 700

Patent

active

053633172

ABSTRACT:
An engine failure monitor 50 for use with a multi-engine aircraft having at least two engines detects conditions indicative of a partial (700) or total (400) engine failure, including turbine shaft failures (600). In response to an engine failure, suitable inputs (134, 138, 712) are provided to an electronic engine control for operating the remaining engine. Additionally, indications indicative of the engine failure (132, 710) are provided to the cockpit.

REFERENCES:
patent: 4500966 (1985-02-01), Zagranski et al.
patent: 4811255 (1989-03-01), Kelly, III
patent: 4817046 (1989-03-01), Rice et al.
patent: 5189620 (1993-02-01), Parsons et al.
patent: 5233542 (1993-08-01), Hohnen et al.

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