发明名称 |
Joining composite fuselage sections along window belts |
摘要 |
<p>A fuselage having a longitudinal window belt (58) has a composite outer skin including upper and lower composite skin sections (52, 54). The skin includes at least one window opening (70) located at the window belt (58). The upper and lower skin sections are joined together by a longitudinal splice joint (56) located at the window belt (58).</p> |
申请公布号 |
EP2682340(A2) |
申请公布日期 |
2014.01.08 |
申请号 |
EP20130173489 |
申请日期 |
2013.06.25 |
申请人 |
THE BOEING COMPANY |
发明人 |
DOPKER, BERNHARD;CHAN, WALLACE CHI-HUA;OSTROFF, HENRI MICHAEL |
分类号 |
B64C1/06;B64F5/00 |
主分类号 |
B64C1/06 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|