发明名称 RADAR FOR LIGHT-WEIGHT ENGINE AIRPLANE
摘要 FIELD: radio engineering. ^ SUBSTANCE: radar can be used for view forwarding of front semi-sphere (lower and upper) of light-weight maneuver airplanes and helicopters to prevent collision against other flying vehicles, high-voltage power lines, towers, pipes and etcetera. Radar is made of three parts: aerial which has first and second phased aerial sub-arrays and control computing unit. Any sub-array has N irradiators, phase commutator, ferrite circulator, first self-excited oscillator and low noise amplifier. Control computing unit has adder, receiver, microcontroller, second self-excited oscillator, and LCD indicator and alarm unit. ^ EFFECT: improved safety of flight. ^ 4 cl, 4 dwg
申请公布号 RU2258244(C2) 申请公布日期 2005.08.10
申请号 RU20020120557 申请日期 2002.07.29
申请人 发明人 IVANOV V.EH.;BUKREEV A.S.;DUDIN D.N.;GODLEVSKIJ V.U.;STEPANOV V.L.;ABUZJAROV F.N.;SAZHIN S.D.
分类号 G01S13/93;G01S13/42 主分类号 G01S13/93
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