发明名称 RIB SUPPORT FOR WING PANELS
摘要 An innovative wing structure provides ribs to support skin panels without an attachment between the rib and the stringer free flange or the web. The support is provided by rib shear ties installed directly to the stringer skin flange. The rib incorporates a cut away to allow the stringer to pass through the rib. The composite stringer is an 'I' section and is stable under compression, not requiring mechanical methods to prevent rolling over.
申请公布号 US2008210821(A1) 申请公布日期 2008.09.04
申请号 US20060610444 申请日期 2006.12.13
申请人 THE BOEING COMPANY 发明人 TANNER RICHARD B.;BURFORD IAN C.;GENDZWILL THOMAS V.;DOTY GREGORY B.;HUCK JAMES R.;WILSON DEAN E.;KORENAGA BRIAN H.
分类号 B64C3/18;B64C3/26 主分类号 B64C3/18
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