FIELD: aviation.
SUBSTANCE: invention relates to aircraft landing gear wheels. Electromechanical disc brake comprises brake disc mounted on chassis wheel. On brake disc from magnetic material poles are oriented radially in plane of brake disc and perpendicular to disc rotation axis. On main support chassis electromagnet is fixed with split poles at ends of its magnetic conductor. Between split electromagnet poles is arranged in slots with minimum air gap a brake disc, next to split electromagnet poles there are position sensors for poles of brake disc, connected by their outputs to inputs of control device. Control device is connected by its output to input of switching device, which connects electromagnet winding to power supply. Other input of control device is connected to output of brake force control device. Device for disc retainer comprises pin of disc retainer.
EFFECT: higher reliability and wear resistance of brake.
1 cl, 8 dwg
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Authors
Dates
2016-06-10—Published
2015-05-18—Filed