发明名称 AIRCRAFT TAKEOOF ACCELERATION INDICATOR SYSTEM
摘要 <p>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.</p>
申请公布号 WO1998047056(A1) 申请公布日期 1998.10.22
申请号 CA1997000785 申请日期 1997.10.22
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