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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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