FIELD: electricity.
SUBSTANCE: method includes the current measuring stage, at least in one electrical connection, in which the nominal current flows, for the certain flight conditions of the aircraft; the measured current value wireless transmitting stage, the measured current receipt stage, comparison stage of the measured current with the reference nominal current, determined for the indicated electrical connection, for the indicated specific flight conditions; and the diagnostics stage of the electrical connection good condition after the comparison stage. The system comprises at least one current sensor, coupled to at least one electrical connection, adapted to provide circulation of the nominal current for the specific flight conditions of the aircraft, the mentioned current sensor is configured to measure the current, the mentioned current sensor comprises the measured current value wireless transmitting facilities, the maintenance computing device, comprising the wireless receiving data facilities, the maintenance computing device is adapted to compare the measured current with the reference nominal current, specified for the mentioned electrical connections for the specific aircraft flight conditions, in order to determine the electrical connection good condition.
EFFECT: increase of the rapid response.
12 cl, 4 dwg
Authors
Dates
2017-12-21—Published
2013-10-21—Filed