发明名称 VARNINGSINSTRUMENT VID FLYGFARKOST
摘要 In a warning system for aircraft that generates a warning signal when the aircraft is descending during a take-off or missed approach phase of operation, the warning is inhibited for a predetermined loss of altitude in order to allow the aircraft to descend a short distance without triggering a nuisance warning. Specifically, a circuit is provided to integrate a signal representing the aircraft's rate of descent until the integrated signal is equal to a predetermined drop in altitude whereupon the warning signal is triggered.
申请公布号 SE415831(B) 申请公布日期 1980.11.03
申请号 SE19760000147 申请日期 1976.01.09
申请人 * SUNDSTRAND DATA CONTRONL INC 发明人 C D * BATEMAN;H R * MULLER
分类号 B64D45/04;G01C5/00;G01C21/00;G01C21/20;G01S13/91;G05D1/06;G08G5/04;(IPC1-7):64D45/04 主分类号 B64D45/04
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