发明名称 Wrinkle Control for Composite Tubes
摘要 In one step of a method of fabricating a composite tube, layers of uncured composite material may be laid over a surface. In another step, spaced-apart strips of at least one of uncured, partially cured, and completely cured composite material may be laid lengthwise over the laid layers of composite material. In still another step, the spaced-apart strips may be compacted against the layers of uncured composite material. In an additional step, the compacted spaced-apart strips and the layers of uncured composite material may be further consolidated and/or cured to form a composite tube.
申请公布号 US2012141705(A1) 申请公布日期 2012.06.07
申请号 US201213350600 申请日期 2012.01.13
申请人 THE BOEING COMPANY 发明人 BOOKER GARRY A.;HOLMAN WESLEY L.
分类号 B32B1/08;B32B17/04;B32B18/00;B32B27/00 主分类号 B32B1/08
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