发明名称 Braided reinforcement for aircraft fuselage frames and method of producing the same
摘要 A machine and method for applying braid by means of a braiding machine to a mandrel, where the mandrel has a shape that approximates a wheel but has an irregularly varying radius of curvature. The machine includes drive/positioning wheel assemblies that are used to continuously reposition a cross-section of the mandrel relative to the braiding machine such that a center point of cross-section of the mandrel is maintained to be coaxial with a braiding point of the braiding machine as the mandrel 18 is rotationally advanced by the drive/positioning wheel assemblies. Repositioning of the drive/positioning wheel assemblies is controlled by a computer numerical control (CNC) controller, based on information describing one or more radiuses of curvature for sections of the mandrel and a current position of the mandrel relative to the drive/positioning wheel assemblies.
申请公布号 US7793576(B2) 申请公布日期 2010.09.14
申请号 US20080017964 申请日期 2008.01.22
申请人 A&P TECHNOLOGY, INC. 发明人 HEAD ANDREW ATKINS;GOETZ BRAD;PETER JOHN;STENARD STEVEN CHARLES;STORY THOMAS C.
分类号 D04C3/40 主分类号 D04C3/40
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