公开(公告)号：WO2011129696A3

公开(公告)日：2011-10-20

申请号：PCT/NL2011/050253

申请日：2011-04-14

Applicant: B.V. GREEN X ,  MUSTERS, Robert Jan

Inventor： MUSTERS, Robert Jan

IPC: B64C3/10 ,  B64C23/00

Abstract: The invention relates to a wing (1) for generating lift and comprises a trailing edge (5), a leading edge (3), an inner end (7), an outer end (9), a top surface (10) and a bottom surface (12). The wing comprises an aerofoil with a chord line and a span direction. The leading edge comprises a kink (21) between the inner (7) end and the outer end (9). The leading edge comprises a forward sweep part between the inner end and the kink extending towards the kink presenting an angle (a) relative to the span direction. The leading edge comprises a backward sweep part (35) between the kink and the outer end extending from the kink presenting an angle (β) relative to the span direction. The top surface comprises a flow control means (30) for controlling the lift at least partly located between a leading edge part between the kink and the outer end and located between the leading edge and the trailing edge.

公开(公告)号：WO2011129696A2

公开(公告)日：2011-10-20

申请号：PCT/NL2011050253

申请日：2011-04-14

Applicant: GREEN X B V ,  MUSTERS ROBERT JAN

Inventor： MUSTERS ROBERT JAN

IPC: B64C3/10

CPC classification number: B64C3/38 ,  A63H27/008 ,  B64C3/10 ,  B64C23/00 ,  B64C33/02 ,  B64C2201/025 ,  F01D5/12

Abstract: The invention relates to a wing for generating lift and comprises a trailing edge, a leading edge, an inner end, an outer end, a top surface and a bottom surface. The wing comprises an aerofoil with a chord line and a span direction. The leading edge comprises a kink between the inner end and the outer end. The leading edge comprises a forward sweep part between the inner end and the kink extending towards the kink presenting an angle relative to the span direction. The leading edge comprises a backward sweep part between the kink and the outer end extending from the kink presenting an angle relative to the span direction. The top surface comprises a flow control means for controlling the lift at least partly located between a leading edge part between the kink and the outer end and located between the leading edge and the trailing edge.

Abstract translation: 本发明涉及一种用于产生升降机的机翼，包括后缘，前缘，内端，外端，顶表面和底面。 机翼包括具有弦线和跨度方向的机翼。 前缘包括在内端和外端之间的扭结。 前缘包括在内端和扭结之间的向前扫掠部分，朝向扭结延伸，呈现出相对于跨度方向的角度。 前缘包括在扭结之间的反向扫掠部分和从扭结延伸的外端部，其相对于跨度方向呈现一个角度。 顶表面包括用于控制至少部分地位于扭结和外端之间的前缘部分之间且位于前缘和后缘之间的升力的流量控制装置。