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edge morphological alteration arrangement for an airfoil having lower upper control surfaces and arrangement for converting linear motion to rotational motion

机译:具有下部上控制面的机翼的边缘形态改变装置以及用于将线性运动转换为旋转运动的装置

摘要

MORPHOLOGICAL EDGE ARRANGEMENT ARRANGEMENT THAT HAS UPPER AND LOWER CONTROL SURFACES AND ARRANGEMENT TO CONVERT LINEAR MOVEMENT IN ROTATORY MOVEMENT This is an edge control arrangement that has a lower airfoil and upper control surfaces. provided with a rib element arranged to overlap the edge of the airfoil. The rib element has first and second rib portions arranged to communicate with respectively associated upper and lower airfoil control surfaces. A first compatible connecting member has first and second ends and is disposed between the first and second rib portions of the rib member, and each of the first and second ends is coupled within a respectively associated portion of the first and second ribs. the second rib parts. Additionally, a propulsion bond having first and second propulsion bonding ends is shown, wherein the first propulsion bonding end is coupled within a selectable part between the first and second rib parts in the vicinity of the coupling of the propulsion. respectively associated end of the first compatible connecting element. The second end is arranged to receive a morphological alteration force, and the rib element is deformed in response to the morphological alteration force. Multiple rib elements may be arranged substantially parallel to each other and configured to alter morphology for their respective operational ratios. Additionally, an overlying cover has a thickness that varies in wingspan.
机译:具有上,下控制面的形态学边缘布置,以及将旋转运动转换成线性运动的布置这是一种具有较低机翼和较高控制面的边缘控制装置。设有设置成与翼型件的边缘重叠的肋元件。肋元件具有第一肋部分和第二肋部分,该第一肋部分和第二肋部分布置成分别与相关联的上部和下部翼型件控制表面连通。第一兼容连接构件具有第一端和第二端,并且布置在肋构件的第一肋部分和第二肋部分之间,并且第一端和第二端中的每一个联接在第一肋和第二肋的分别相关联的部分内。第二肋部分。另外,示出了具有第一和第二推进结合端的推进结合,其中在推进的结合附近,第一推进结合端在第一和第二肋部之间的可选部分内结合。第一兼容连接元件的相应相关端。第二端布置成接收形态学改变力,并且肋元件响应于形态学改变力而变形。多个肋元件可以基本上彼此平行地布置并且被配置成改变它们各自的工作比的形态。另外,上面的覆盖物的厚度在翼展上变化。

著录项

  • 公开/公告号BRPI0710353A2

    专利类型

  • 公开/公告日2011-08-09

    原文格式PDF

  • 申请/专利权人 FLEXSYS INC.;

    申请/专利号BR2007PI10353

  • 申请日2007-04-27

  • 分类号B64C27/54;

  • 国家 BR

  • 入库时间 2022-08-21 18:07:06

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