发明名称 Trimming composite skin stiffener ends
摘要 A tool for trimming the ends of stiffeners on aircraft composite skin panels accurately, rapidly and without damaging the underlying skins includes an expandable guide frame adapted to straddle and clamp to the stiffener at a selected longitudinal position thereon. The frame includes a pair of planar guide faces disposed on opposite sides of the stiffener and lying in a common plane transverse thereto. The rotatably supported opposite ends of a rotating abrasive drum are slid along respective ones of the guide faces such that the drum grinds away the stiffener in a plane parallel to the plane of the guide faces and thereby forms a trimmed end on the stiffener. The frame includes mechanisms for adjusting the angular inclination of the plane of the guide faces relative to the plane of the composite skin, and for preventing the grinding mechanism from cutting into the composite skin.
申请公布号 US7628679(B2) 申请公布日期 2009.12.08
申请号 US20060549807 申请日期 2006.10.16
申请人 THE BOEING COMPANY 发明人 FROESCHNER NEAL A.;PISZAR JIM S.
分类号 B24B9/00 主分类号 B24B9/00
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