FIELD: machine building.
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 the main support chassis electromagnet is fixed at the ends of which there are poles, between which there is brake disc. In circumferential direction near core poles of electromagnet brake disc pole position sensors are connected by their outputs to inputs of the control device connected by its output to the input of switching device, which connects electromagnet winding to power supply, control device is connected to another input of the output of the brake force control. Retainer device disc containing pin retainer disc is attached to the main aircraft undercarriage support near the brake disc.
EFFECT: higher reliability of disc brakes.
1 cl, 11 dwg
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Authors
Dates
2016-07-10—Published
2015-05-07—Filed