发明名称 AIRCRAFT ROTOR OUTPUT CALIBRATION SYSTEM
摘要 PURPOSE: A system for calibrating the output of an aircraft rotor is provided to accurately adjust the posture of an aircraft and diagnose the malfunction of the aircraft by measuring the actual output of a rotor using an air flow sensor. CONSTITUTION: A system for calibrating the output of an aircraft rotor comprises an air flow sensor (130). The air flow sensor measures the intensity of an air flow caused by the rotation of a rotary blade (120). The rotary blade is rotated by a rotor (110). The air flow sensor is located under the rotary blade to be separated from the bottom of the rotary blade.
申请公布号 KR20130097279(A) 申请公布日期 2013.09.03
申请号 KR20120018803 申请日期 2012.02.24
申请人 NAVIONICS KOREA CO., LTD. 发明人 PARK SI MONG;LEE, JU HEON
分类号 B64C27/54;B64C13/16;B64D43/02 主分类号 B64C27/54
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