公开(公告)号：US4659041A

公开(公告)日：1987-04-21

申请号：US784485

申请日：1985-10-04

申请人： Juergen Dellinger ,  Ulrich Kraemer ,  Rainer Schlieske ,  Heinz Wohlers

发明人： Juergen Dellinger ,  Ulrich Kraemer ,  Rainer Schlieske ,  Heinz Wohlers

IPC分类号： B64D17/80

CPC分类号： B64D17/80 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/165 ,  B64C2201/185

摘要： In an unmanned craft with a tail end propeller the improvement of a parachute landing system for causing the craft to land while being suspended by a parachute of the system; the fuselage for the craft has a rearwardly, laterally and, thus, asymmetrically arranged opening leading into a storage compartment for a pilot and a principal parachute system; a flap normally closes the opening but being openable and pivotable in outward direction about an axis being at least approximately vertical to the horizontal disposition of the craft and for about 135.degree.; a cable locks and limits the outward pivoting of the flap, acting as a rudder to steer the craft for 180.degree. during parachute deployment.

摘要翻译： 在具有尾端螺旋桨的无人驾驶技术中，降落伞着陆系统的改进使得飞行器在被系统的降落伞暂停时着陆; 机身的机身具有向后，侧向和因此不对称布置的开口，通向飞行员和主降落伞系统的储藏室; 翼片通常关闭开口，但是可以在向外的方向上围绕轴线打开和枢转，该轴线至少大致垂直于工艺的水平布置并且在约135度; 电缆锁定并限制了挡板的向外枢转，作为方向舵在降落伞部署期间将工艺转向180度。