发明名称 |
JOINT FOR COMPOSITE WINGS |
摘要 |
<p>A wing joint including a T-chord and a splice plate for connecting an inboard wing panel assembly and an outboard wing panel assembly. The wing panel assemblies include a stringer co-bonded or co-cured with a wing skin. The webbing and cap of the stringer may be trimmed to expose a noodle and base flange. The noodle and base flange interface with the bottom of the T-chord and the wing skin interfaces with the splice plate. The exposed noodle may be non-flush with the base flange of the trimmed stringer. The bottom of the T-chord may include a groove to accommodate a non-flush noodle so that a gap does not exist between the T-chord and the base flange. Alternatively, shims may be used to compensate for a non-flush noodle or the base flange and web may include sacrificial plies permitting the base flange and web to be trimmed flush with the noodle.</p> |
申请公布号 |
CA2829899(A1) |
申请公布日期 |
2015.04.10 |
申请号 |
CA20132829899 |
申请日期 |
2013.10.10 |
申请人 |
THE BOEING COMPANY |
发明人 |
LIN, CHUN-LIANG;MAHN, RYAN M.;LEE, KARL B. |
分类号 |
B64C1/26;B64C3/20 |
主分类号 |
B64C1/26 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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