发明名称 ULTRASONIC AIRSPEED SENSOR FOR AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To provide an airspeed measuring device for an aircraft capable of measuring a low speed area by improving a sensor probe of an ultrasonic anemometer suitable for measuring a gentle wind and having no movable part. SOLUTION: A plurality of ultrasonic transmitters-receivers are equipped in axially different positions on three support bars mounted to an airframe parallel or having slight open angles so that their axes are positioned on the respective vertexes of a triangle toward the front direction of the aircraft. Plural sets of ultrasonic transmit-receive routes are formed by a combination of the ultrasonic transmitters-receivers on the adjacent support bars, and three- dimensional information on airspeed is obtained from time information of propagation in plural sets of the ultrasonic transmit-receive routes of specified distance.
申请公布号 JP2001278196(A) 申请公布日期 2001.10.10
申请号 JP20000090200 申请日期 2000.03.29
申请人 NATL AEROSPACE LAB 发明人 INOKUCHI HAMAKI
分类号 G01P5/00;B64B1/06;B64D43/02;(IPC1-7):B64D43/02 主分类号 G01P5/00
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