CO-CURED STRINGERS AND ASSOCIATED MANDREL AND FABRICATION METHOD
摘要
A co-cured composite stringer and associated apparatus and method are provided. The co-cured composite stringer includes a stringer and a mandrel positioned within a channel defined in the stringer. A plurality of strips are positioned within an opening of the mandrel, and a substrate layer, such as aircraft skin, is positioned adjacent to the stringer. During application of the substrate layer to the stringer, the mandrel and plurality of strips support the stringer.
申请公布号
WO2005105402(A1)
申请公布日期
2005.11.10
申请号
WO2005US06572
申请日期
2005.03.01
申请人
THE BOEING COMPANY;ENGWALL, DWIGHT, L.;MORROW, CHRISTOPHER, J.