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
Title | Year | Author | Number |
---|---|---|---|
SYSTEM AND METHOD FOR DETECTING ERRONEOUS PRESSURE MEASUREMENTS IN AIR SIGNAL SYSTEM WITH NON-PROTRUDING PRESSURE RECEIVERS USING PRESSURE DIAGRAMS BETWEEN ADJACENT PRESSURE SAMPLING HOLES | 2019 |
|
RU2771090C1 |
DEVICE TO DETECT AND REMOVE ICE OR FLUID LAYER | 2007 |
|
RU2453475C2 |
TWO-CHANNEL ARCHITECTURE | 2015 |
|
RU2679706C2 |
METHOD OF CONTROLLING NETWORK OF ELECTRIC POWER SUPPLY OF AIR VEHICLE | 2013 |
|
RU2646012C2 |
METHOD TO CONTROL UNMANNED AIR VEHICLE AND DEVICE FOR IT | 2015 |
|
RU2637838C2 |
MONITORING STATE OF SERVO DRIVE IN AIRCRAFT | 2016 |
|
RU2710513C1 |
AIRCRAFT AIRFRAME AND THE LANDING GEAR TECHNICAL CONDITION MONITORING METHOD AND DEVICE AND DEVICE FOR ITS IMPLEMENTATION | 2017 |
|
RU2678540C1 |
FLYING VEHICLE ANGULAR ORIENTATION DETECTOR CONTROL DEVICE | 2003 |
|
RU2241247C1 |
STABILISATION OF DC ELECTRIC NETWORK | 2012 |
|
RU2597866C2 |
METHOD FOR CONTROLLING STATE OF AIRCRAFT CONSTRUCTION | 2014 |
|
RU2545150C1 |
Authors
Dates
2017-12-21—Published
2013-10-21—Filed