Partial engine and driveshaft failure detection monitor for...

Details Partial engine and driveshaft failure detection monitor for... Partial engine and driveshaft failure detection monitor for...

G - Physics

01

M

G01M 15/00 (2006.01) B64D 31/00 (2006.01) B64D 31/12 (2006.01) B64D 45/00 (2006.01) G07C 3/00 (2006.01)

Patent

CA 2143871

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 in- puts (134, 138, 712) are provided to an electronic engine control for operating the remaining engine. Additionally, indications in- dicative of the engine failure (132, 710) are provided to the cock- pit.

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