发明名称 Two-dimensional morphing structure for wing
摘要 An apparatus and methods for changing the shape of a wing using a plurality of morphing structures. One example method includes coupling a plurality of morphing structures to each other. Each morphing structure includes an anchor, a plurality of hinges, a plurality of shape-memory alloy members wherein each shape-memory alloy member extends from the anchor to a different hinge, a plurality of springs wherein each spring extends from the anchor to a different hinge, and a plurality of rigid members wherein each rigid member extends between two hinges. The method further includes actuating the plurality of shape-memory alloy members in at least some of the morphing structures wherein the shape-memory alloy members contract when actuated to pull against the hinges and anchors within the actuated morphing structures to rotate the rigid members and change the shape of the actuated morphing structure.
申请公布号 US8991769(B2) 申请公布日期 2015.03.31
申请号 US201313751247 申请日期 2013.01.28
申请人 Toyota Motor Engineering & Manufacturing North America, Inc. 发明人 Gandhi Umesh N.
分类号 B64C3/44;B64C3/52;B64C3/36;B64C3/54 主分类号 B64C3/44
代理机构 Young Basile Hanlon & MacFarlane P.C. 代理人 Darrow Christopher G.;Young Basile Hanlon & MacFarlane P.C.
主权项 1. An internal frame of an aircraft wing, comprising: a morphing structure, the morphing structure, including: an anchor;a plurality of hinges surrounding the anchor;a plurality of shape-memory alloy members wherein each shape-memory alloy member extends from the anchor to one of the plurality of hinges;a plurality of springs wherein each spring extends from the anchor to one of the plurality of hinges; anda plurality of rigid members wherein each rigid member extends between two hinges.
地址 Erlanger KY US