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 the audible alarm and color light flicker generator (72).
申请公布号 CA2362139(C) 申请公布日期 2005.02.22
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
代理机构 代理人
主权项
地址