发明名称 AIRCRAFT TAKEOFF ACCELERATION INDICATOR SYSTEM
摘要 An aircraft instrument system that informs the pilot of whether, during the takeoff roll, the aircraft's acceleration rate is sufficient to ensure that V1 speed will be achieved at the expected time (and thus distance), and, if not, how far in distance the aircraft is lagging behind the required acceleration schedule.
申请公布号 CA2253899(A1) 申请公布日期 1998.10.22
申请号 CA19972253899 申请日期 1997.10.22
申请人 MILLARD, WAYNE C.;MILLARD, CARL W. 发明人 MILLARD, WAYNE C.;MILLARD, CARL W.
分类号 B64D43/02;G01C23/00;(IPC1-7):G01C23/00 主分类号 B64D43/02
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