发明名称 Flight guidance and navigation display for a helicopter
摘要 <p>The invention relates to a flight guidance and navigation display (10) for a helicopter, comprising a three-dimensional, semicircular flight guidance and navigation tunnel (12) to display a planned flight path of the helicopter; a circular surface (14), which is integrated in the flight guidance and navigation tunnel (12), which circular surface (14) comprises a diameter that corresponds to that of the flight guidance and navigation tunnel (12), for displaying a longitudinal position within the flight guidance and navigation tunnel (12); a flight path prediction icon (16) for displaying a position of the helicopter relative to the flight guidance and navigation tunnel (12); and a command signal (18) that relates to the air speed, wherein by means of the command signal (18) a deviation from a reference speed that has been predetermined by flight planning is displayed. </p>
申请公布号 EP2116811(A3) 申请公布日期 2012.08.01
申请号 EP20090006000 申请日期 2009.04.30
申请人 EUROCOPTER DEUTSCHLAND GMBH 发明人 VAN DER SPEK, JORRIT
分类号 G01C23/00 主分类号 G01C23/00
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