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1. 发明授权

US07731123B2 Contra-bevel driven control surface 有权
标题翻译：反斜面驱动控制面
公开(公告)号：US07731123B2
公开(公告)日：2010-06-08
申请号：US11534657
申请日：2006-09-24
申请人： Kendall G. Young , Joseph A. Simon , Robert S. Cascella , Kevin D. Edge
发明人： Kendall G. Young , Joseph A. Simon , Robert S. Cascella , Kevin D. Edge
IPC分类号： B64C9/04
CPC分类号： B64C9/02 , B64C9/16 , B64C9/22 , Y02T50/32
摘要： A contra-bevel driven control mechanism repositions a control surface in a fluid environment such as an aerodynamic or hydrodynamic environment. This involves mechanically coupling an airfoil and a control surface. The control surface may pivot about a spanwise axis between upwardly deflected and downwardly deflected positions. A forward beveled rotor mounted to the airfoil and an aft beveled rotor mounted to the control surface counter rotate. The forward beveled rotor rotates about a forward chordwise axis within the airfoil while the aft beveled rotor rotates about an aft chordwise axis within the control surface. The angular rotation between the forward beveled rotor and the aft beveled rotor deflects the aft beveled rotor and the aft chordwise axis within the control surface. Additionally, this method allows the control surface to be deflected with maximum mechanical advantage when the control surface is fully deflected.
摘要翻译：反斜面驱动控制机构在诸如空气动力学或流体动力学环境的流体环境中重新定位控制表面。这涉及机翼连接翼型件和控制面。控制表面可以围绕向上偏转和向下偏转的位置之间的翼展方向轴线枢转。安装到翼型件的前斜面转子和安装到控制表面反转器的后倾斜转子。前斜面转子围绕机翼中的向前弦线轴线旋转，而后倾斜转子围绕控制表面内的向后轴线旋转。前斜面转子和后倾斜转子之间的角度旋转使后倾斜转子和后弦轴线在控制表面内偏转。此外，当控制表面完全偏转时，该方法允许控制表面以最大的机械优点被偏转。

2. 发明申请

US20090020644A1 CONTRA-BEVEL DRIVEN CONTROL SURFACE 有权
标题翻译：对比度控制表面
公开(公告)号：US20090020644A1
公开(公告)日：2009-01-22
申请号：US11534657
申请日：2006-09-24
申请人： Kendall G. Young , Joseph A. Simon , Robert S. Cascella , Kevin D. Edge
发明人： Kendall G. Young , Joseph A. Simon , Robert S. Cascella , Kevin D. Edge
IPC分类号： B64C9/02
CPC分类号： B64C9/02 , B64C9/16 , B64C9/22 , Y02T50/32
摘要： A contra-bevel driven control mechanism repositions a control surface in a fluid environment such as an aerodynamic or hydrodynamic environment. This involves mechanically coupling an airfoil and a control surface. The control surface may pivot about a spanwise axis between upwardly deflected and downwardly deflected positions. A forward beveled rotor mounted to the airfoil and an aft beveled rotor mounted to the control surface counter rotate. The forward beveled rotor rotates about a forward chordwise axis within the airfoil while the aft beveled rotor rotates about an aft chordwise axis within the control surface. The angular rotation between the forward beveled rotor and the aft beveled rotor deflects the aft beveled rotor and the aft chordwise axis within the control surface. Additionally, this method allows the control surface to be deflected with maximum mechanical advantage when the control surface is fully deflected
摘要翻译：反斜面驱动控制机构在诸如空气动力学或流体动力学环境的流体环境中重新定位控制表面。这涉及机翼连接翼型件和控制面。控制表面可以围绕向上偏转和向下偏转的位置之间的翼展方向轴线枢转。安装到翼型件的前斜面转子和安装到控制表面反转器的后倾斜转子。前斜面转子围绕机翼中的向前弦线轴线旋转，而后倾斜转子围绕控制表面内的向后轴线旋转。前斜面转子和后倾斜转子之间的角度旋转使后倾斜转子和后弦轴线在控制表面内偏转。此外，当控制表面完全偏转时，该方法允许控制表面以最大的机械优点被偏转

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