FIELD: transportation.
SUBSTANCE: multi-disc cylindrical electromechanical aircraft brake contains rotating and non-rotating brake disс
s. On the rotating and non-rotating brake discs made of a magnetic material, alternating and arranged relative to each other with the minimum working air gap, the poles are made, oriented radially in the brake discs plane. On the main landing gear axis the axial electromagnet is fixed, the poles of which are perpendicular to the brake discs plane and are arranged with the minimum air gap to the working cylinder of a magnetic material. In a plane parallel to the rotating brake disc, the position sensors of the rotating brake disc poles are located, connected by their outputs to the inputs of the control device connected by its output to the switching device input. The brake force control device output is connected to the other input of the control device.
EFFECT: increasing the reliability of multi-disc brakes and reducing the maintenance costs.
17 dwg
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Authors
Dates
2017-03-09—Published
2015-11-23—Filed