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    • 9. 发明申请
    • MORPHING WING FOR AN AIRCRAFT
    • 飞机的飞行员
    • US20150151830A1
    • 2015-06-04
    • US14408722
    • 2013-06-21
    • BOMBARDIER INC.
    • Fengfeng XiAllan Daniel FinistauriAmin Moosavian
    • B64C3/38B64C3/54B64C3/40
    • B64C3/38B64C3/385B64C3/40B64C3/44B64C3/52B64C3/54B64C2003/445B64C2003/543Y02T50/14
    • A morphing wing for an aircraft includes a top surface, a bottom surface, a leading edge, a trailing edge, a tip, and a root. A plurality of structural ribs is disposed between the root and tip so that they extend between the top surface and the bottom surface and intersect with a lateral axis thereof. At least one active member connects between two adjacent structural ribs along or at a first angle to the lateral axis. The active member is actively adjustable. At least one passive member connects between the two adjacent structural ribs along or at a second angle to the lateral axis. The passive member is passively adjustable. Adjustment of at least one active member moves the adjacent structural ribs with respect to one another, thereby morphing the wing from a first configuration to a second configuration.
    • 用于飞机的变形翼包括顶表面,底表面,前缘,后缘,尖端和根部。 多个结构肋设置在根部和尖端之间,使得它们在顶表面和底表面之间延伸并与其横向轴线相交。 至少一个有源构件沿着或相对于横向轴线以第一角度连接在两个相邻结构肋之间。 活动构件可以主动调节。 至少一个无源构件沿着或相对于横向轴线的第二角度在两个相邻的结构肋之间连接。 被动元件被动调节。 至少一个活动构件的调节使相邻的结构肋相对于彼此移动,从而使机翼从第一构型变形到第二构型。