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 |