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