发明名称 COLLISION AVOIDANCE SYSTEM FOR USE IN AIRCRAFT
摘要 A collision avoidance system includes a forward terrain collision peak and selector channel indicator (92), a ground proximity peak selector (90), an aircraft collision threshold circuit (82), and a ground proximity threshold circuit (96) together with split range gates (84, 98, 104). Microwave transmission is accomplished using a pulse modulator (54) and Gunn or IMPATT diode power amplifier/oscillator (56). The warning alarm signal comes from t he audible alarm and color light flicker generator (72).
申请公布号 CA2362139(A1) 申请公布日期 2000.08.31
申请号 CA20002362139 申请日期 2000.02.23
申请人 FLIGHT SAFETY TECHNOLOGIES, INC. 发明人 REES, FRANK LEONARD
分类号 G01S7/02;G01S7/04;G01S13/18;G01S13/76;G01S13/93;G01S13/94;(IPC1-7):G01S13/00 主分类号 G01S7/02
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