首页> 外国专利> WING-TIP ARRANGEMENT HAVING VORTILONS ATTACHED TO A LOWER SURFACE, AN AIRCRAFT HAVING SUCH A WING-TIP ARRANGEMENT AND THE USE OF VORTILONS ON A WING-TIP ARRANGEMENT

WING-TIP ARRANGEMENT HAVING VORTILONS ATTACHED TO A LOWER SURFACE, AN AIRCRAFT HAVING SUCH A WING-TIP ARRANGEMENT AND THE USE OF VORTILONS ON A WING-TIP ARRANGEMENT

机译:机翼尖端布置在下部表面附有VORTILON,飞机在机翼尖端布置有此类翼梢,并且在机翼尖端布置中使用了VORTILON

摘要

A wing-tip arrangement (2) couplable with a wing (38) of an aircraft comprisesa connectionregion (4) for coupling or integration with the wing end region (10), at leastone tip, at leastone upper surface (14) and at least one lower surface (16), which extendbetween a leadingedge (6) and a trailing edge (8) of the wing-tip arrangement (2) from theconnection region (4)to the at least one tip, and at least one vortilon (18). The local dihedral ofthe wing-tiparrangement (2) changes between the at least one tip and the connection region(4), such thatat least a part of the wing-tip arrangement projects at an angle relative tothe wing, whencoupled with the wing end region (10). The at least one vortilon (18)comprises a vortilonbase (22) and a vortilon tip (24), wherein the vortilon base (22) is attachedto at least one ofthe at least one lower surface (16) of the wing-tip arrangement (2) andwherein the vortilon tip(24) faces in an upstream direction.
机译:可与飞机的机翼(38)连接的翼尖装置(2)包括连接区域(4)至少与机翼末端区域(10)耦合或集成至少一个提示延伸的一个上表面(14)和至少一个下表面(16)在领先之间翼尖装置(2)的边缘(6)和后缘(8)连接区域(4)至少一个尖端,和至少一个vortilon(18)。的本地二面体翼尖布置(2)在至少一个尖端和连接区域之间变化(4),这样至少一部分机翼尖端装置相对于一定角度突出机翼,何时与机翼端部区域(10)相连。至少一个vortilon(18)包括一个vortilon基座(22)和vortilon尖端(24),其中vortilon基座(22)已连接至少翼尖装置(2)的至少一个下表面(16)和伏地龙尖端(24)面向上游方向。

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