Failure detector and indicator for aircraft flap actuation syste

Machine element or mechanism – Gearing – Plural power paths to and/or from gearing

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244 42D, 64 30E, 74337, 74388R, 74412TA, 74520, 74664, F16H 3706, F16H 552, F16H 3500, B64C 900

Patent

active

039357546

ABSTRACT:
Detecting and indicating the failure of the primary drive train of a flap actuator system that includes primary and secondary drive trains driven by a common power supply is disclosed. When the primary drive trains fails, a free motion zone formed between the common power supply and the secondary drive train is crossed. Crossing of the free motion zone causes the position of an electro-mechanical sensor (or sensors) to change. The change in position of the electro-mechanical sensor(s) creates or changes the value of an electrical signal or signals to provide an indication of the failure of the primary drive train.

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patent: 3830349 (1974-08-01), Williams

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