公开(公告)号：US4757959A

公开(公告)日：1988-07-19

申请号：US15304

申请日：1987-02-17

申请人： Barbel Schroder ,  Gunter Schroder

发明人： Barbel Schroder ,  Gunter Schroder

IPC分类号： B64D3/00 ,  B64C37/02

CPC分类号： B64D3/00

摘要： The invention is directed to a method and arrangement for providing safe vertical landing of airplanes, which are not provided with VTOL equipment or which are hindered with respect to their actual flight capabilities, as well as for providing extrinsically supported zero-run takeoff of airplanes. An airplane equipped with lower takeup means is coupled in flight to upper takeup means carried by a rotary wing aircraft flying above the airplane. The rotary wing aircraft generates the propulsion necessary to transport the airplane and the lifting force and sets it down vertically. Zero-run takeoff is initiated by lifting the airplane and accelerating it into its direction of flight by the rotary wing aircraft. When sufficient height, speed against wind and self-propulsion are gained, the airplane releases the connection to the upper takeup means and flies without assistance.

摘要翻译： 本发明涉及一种用于提供飞机的安全垂直着陆的方法和装置，该飞机没有提供垂直起落度的设备，或者相对于它们的实际飞行能力而受到阻碍，并且用于提供空中支援的零飞行起飞。 装备有较低收起装置的飞机在飞行中与由飞机上方的旋翼飞机携带的上部收起装置相耦合。 旋翼飞机产生运输飞机和提升力所需的推进力并将其垂直设置。 通过提升飞机并通过旋翼飞机将其加速到其飞行方向来启动零起飞。 当足够的高度时，获得了抵抗风和自推进的速度，飞机释放与上部收起装置的连接并且没有帮助而飞行。