发明名称 Multi-Box Wing Spar and Skin
摘要 Apparatus and systems provide for the construction of wing sections having multi-box wing spars. According to one aspect of the disclosure provided herein, an aircraft wing includes multi-box wing spars attached to an aircraft fuselage, an upper wing surface, a lower wing surface, and a number of wing segments. The multi-box wing spars, upper wing surface, and lower wing surface are composite layers having continuous fibers.
申请公布号 US2017106968(A1) 申请公布日期 2017.04.20
申请号 US201615390657 申请日期 2016.12.26
申请人 The Boeing Company 发明人 Moselage, III John H.
分类号 B64C3/18;B64C3/20;B29C70/34;B64C1/26 主分类号 B64C3/18
代理机构 代理人
主权项 1. A wing, comprising: a plurality of multi-box wing spars attached to at least one beam of an aircraft fuselage; an upper wing surface; a lower wing surface; and a plurality of wing segments, wherein the plurality of multi-box wing spars, upper wing surface, and lower wing surface are composite layers comprising substantially continuous fibers.
地址 Chicago IL US