Horizontal stabilizer drive

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

Patent

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Details

64 28R, 74469, 74713, 244213, F16H 144, F16D 900, G05G 700

Patent

active

042481058

ABSTRACT:
A mechanical power transmission apparatus, of the differential gear type, for actuating an airplane control surface requiring two independent actuator inputs to a single control surface. Asymmetric loading to the control surface is accommodated by a mechanical fuse link. The fuse link is provided by employing a shear pin to attach the pinion gear to the pinion shaft, designed to fail at a predetermined differential torque between the two driven bevel gears. Positive disengagement of the gears is provided following fuse link release.

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