发明名称 HELICOPTER LANDING GUIDANCE SYSTEM
摘要 <p>Disclosed is a helicopter landing guidance system. According to an embodiment of the present invention, the helicopter landing guidance system comprises: a plurality of tie-downs distributed over a helideck; a net stored in a helicopter and dropped to the helideck when the helicopter lands, having a plurality of hooks in one end portion thereof; and a net lifting module arranged on one side of the helicopter, binding at least a portion of the hooks to at least a portion of the tie-downs by lifting the net to the side of the helicopter, and continuing to lift the net even after the hooks are bound to the tie-downs, thereby a landing position of the helicopter can be controlled by the binding of the hooks and the tie-downs and the continuous net lifting of the net lifting module.</p>
申请公布号 KR20150034031(A) 申请公布日期 2015.04.02
申请号 KR20130114088 申请日期 2013.09.25
申请人 发明人
分类号 B63B35/50;B64F1/02;E01F3/00 主分类号 B63B35/50
代理机构 代理人
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