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
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