发明名称 METHOD OF CONTROLLING AIRCRAFT STRUCTURE STATE AND DEVICE TO THIS END
摘要 FIELD: transport. ^ SUBSTANCE: micro radars are arranged, for example, on aircraft undercarriage legs so that directional pattern of each micro radar covers strictly definite part of "its" tire. Radar signal is irradiated toward each tire in running before take-off and from undercarriage extension in landing to shutdown of engines and signal reflected from tires is received to analyse selected harmonics of reflected signal to define state of every tire. If tire displays faulty state alarm signal is generated. Proposed device comprises onboard first detector, data acquisition device, onboard device, emergent state signaling unit and power supply. Additionally it incorporates second detector, unit of pickups, alarm indicator. Note here that 1st, 2nd and 3rd inputs of second detector are connected with 1st, 2nd and 3rd outputs of the unit of pickups, outputs of second detector are connected with the group of third inputs of data acquisition device with its 2nd output connected with alarm indicator output. Unit of pickups consists of undercarriage limit switches unit, motion sensor and altimeter. ^ EFFECT: higher quality of control. ^ 4 cl, 2 dwg
申请公布号 RU2443991(C1) 申请公布日期 2012.02.27
申请号 RU20100127964 申请日期 2010.07.07
申请人 MUZHICHEK SERGEJ MIKHAJLOVICH;EFANOV VASILIJ VASIL'EVICH;EFIMOV ALEKSANDR VITAL'EVICH 发明人 MUZHICHEK SERGEJ MIKHAJLOVICH;EFANOV VASILIJ VASIL'EVICH;EFIMOV ALEKSANDR VITAL'EVICH
分类号 G01M17/02;G01S13/88 主分类号 G01M17/02
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