发明名称 DETECTOR FOR INDICATING ICE FORMATION ON THE WING OF AN AIRCRAFT
摘要 <p>A detector indicating ice formation on the wing of an aircraft or any planear surface, based on a thread-like or a tape-like transducer, through which a supersonic signal is transmitted at one end. The attenuation of the signal having passed through the thread is measured with a receiver at the opposite end while the thread is simultaneously being heated such that ice that may surround it melts again, the attenuation thus resuming its initial level.</p>
申请公布号 WO1995021766(A1) 申请公布日期 1995.08.17
申请号 FI1994000059 申请日期 1994.02.14
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