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    • 1. 发明授权
    • Control surface continuous seal
    • 控制面连续密封
    • US5839698A
    • 1998-11-24
    • US958717
    • 1997-10-23
    • Joseph C. Moppert
    • Joseph C. Moppert
    • B64C3/50B64C9/06
    • B64C3/50
    • A continuous skin and seal airfoil comprises a rigid structural wing box located centrally chordwise and extending spanwise and including a spanwise extending spar, an upper skin surface and a lower skin surface. Upper and lower control surfaces are pivotally mounted on the spar for movement about a spanwise extending axis between an elevated position and a lowered position and includes an upper skin surface. In similar fashion, a lower control surface is pivotally mounted on the wing box for movement about a spanwise extending axis between an elevated position and a lowered position and includes a lower skin surface. An upper seal member extends spanwise and is fixed to both the wing box and to the upper control surface. Similarly, a lower seal member extends spanwise and is fixed to both the wing box and to the lower control surface. Actuators move the control surfaces between an elevated position and a lowered position. Positioners maintain the upper and lower seals in a substantially zero tension state as the upper and lower control surfaces are moved between the elevated and the lowered positions. The positioners include an extensible upper positioner extending between and pivotally mounted to the spar and to the upper control surface, respectively, and an extensible lower positioner extending between and pivotally mounted to the spar and to the lower control surface, respectively.
    • 连续的皮肤和密封翼型件包括刚性结构翼盒,其中心地纵向延伸并且沿翼展方向延伸,并且包括翼展方向延伸的翼梁,上皮肤表面和下皮肤表面。 上部和下部控制表面可枢转地安装在翼梁上,用于围绕升高位置和降低位置之间的翼展方向延伸轴线运动并且包括上部皮肤表面。 以类似的方式,下控制表面可枢转地安装在翼盒上,用于围绕翼展方向延伸的轴线在提升位置和降低位置之间运动,并且包括下皮肤表面。 上密封构件向翼展方向延伸并且固定到翼盒和上控制表面。 类似地,下密封构件向翼展方向延伸并且固定到翼盒和下控制表面。 执行器将控制表面移动到升高位置和降低位置之间。 当上升和下降控制表面在升高位置和下降位置之间移动时,定位器将上部和下部密封件保持在基本为零张力状态。 定位器包括分别在翼梁和上部控制表面之间分别延伸并可枢转地安装到翼梁和上部控制表面的可伸展的上部定位器,以及分别在翼梁之间延伸并可枢转地安装到翼梁和下部控制表面的可伸缩下部定位器。