发明名称 Ultrasonic angular measurement system
摘要 An ultrasonic angular measurement system is disclosed. The system is comprised of three parts, a control box used to collect and process data, an ultrasonic transducer, and a reflector block. The reflector block is configured so that it intercepts transmitted pulses received over a wide range of angles back to the transducer. All the components are self contained within a transportable housing which is attached to the aircraft deck during measurement of tip-off angle. The range of angle measurement is permitted because of the use of the unique reflector block which comprises a plurality of reflector segments for reflecting ultrasonic pulses transmitted at various ranges of angles.
申请公布号 US6070832(A) 申请公布日期 2000.06.06
申请号 US19940193684 申请日期 1994.02.08
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE 发明人 REDD, JUSTIN D.
分类号 B64D1/12;G01S15/42;(IPC1-7):B64D1/12;G01S15/02 主分类号 B64D1/12
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