公开(公告)号：EP3353053A2

公开(公告)日：2018-08-01

申请号：EP16770340.4

申请日：2016-09-19

申请人： Elson, Andrew Charles

发明人： Elson, Andrew Charles

IPC分类号： B64C3/24

CPC分类号： B64C3/22 ,  B64C3/185 ,  B64C3/187 ,  B64C3/24 ,  B64C3/26 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/104 ,  B64C2201/165 ,  B64F5/10

摘要： An aerofoil has at least one space frame and at least one pre-stressed cover supported by the space frame. The space frame has one or more structural members, the structural members including a structural foam material; and the pre-stressed cover forms at least a part of an external aerodynamic surface of the aerofoil.

公开(公告)号：EP2874875A1

公开(公告)日：2015-05-27

申请号：EP13742690.4

申请日：2013-07-19

申请人： Elson, Andrew Charles

发明人： Elson, Andrew Charles

IPC分类号： B64D5/00 ,  B64C39/02

CPC分类号： B64D5/00 ,  B64B1/40 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/082 ,  B64C2201/104 ,  B64C2201/122 ,  B64C2201/123 ,  B64C2201/162 ,  B64C2201/187 ,  B64D2211/00

摘要： A method of launching a powered unmanned aerial vehicle, the method comprising lifting the vehicle by attachment to a lighter-than-air carrier from a substantially ground-level location to an elevated altitude, wherein the vehicle is prevented from entering its flight mode during ascent, causing the vehicle to detach from the carrier while the velocity of the vehicle relative to the carrier is substantially zero, the vehicle thereafter decreasing in altitude as it accelerates to a velocity where it is capable of preventing any further descent and can begin independent sustained flight.

摘要翻译： 一种在至少13000米的高度上发射供电的无人驾驶飞行器的方法，所述方法包括通过将空载承载器从基本上地平面的位置附近提升到升高的高度，使得车辆 当车辆相对于承运人的速度基本上为零时，车辆离开载体，然后车辆随着其高度减小到能够防止任何进一步下降并且可以开始独立的持续飞行的速度。

公开(公告)号：EP3353052A2

公开(公告)日：2018-08-01

申请号：EP16770339.6

申请日：2016-09-19

申请人： Elson, Andrew Charles

发明人： Elson, Andrew Charles

IPC分类号： B64C3/24 ,  B64C1/00

CPC分类号： B64C3/22 ,  B64C3/185 ,  B64C3/187 ,  B64C3/24 ,  B64C3/26 ,  B64C37/02 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/082 ,  B64C2201/104 ,  B64C2201/165

摘要： An aircraft has a wing providing the main lifting surface for the aircraft. The wing has a structure supporting an aero-dynamic surface, and the wing has a weight, the wing structure being unable to support its own weight when the aircraft is stationary and under a load of 1 g so as to cause structural failure of the wing.