发明名称 METHOD OF REINFORCING A STRATIFIED COMPOSITE MATERIAL PART COMPRISING AT LEAST ONE THROUGH-HOLE, REINFORCED STRATIFIED COMPOSITE MATERIAL PART
摘要 A method of reinforcing a composite material part comprising a stack of fiber layers and at least one hole with an axis. The hole crosses the layers and opens out at the level of a first face and a second face of the part. The method comprises at least one stage in the making of at least one notch in at least one layer of the part proximate to the hole or which opens out in the hole.
申请公布号 US2016023425(A1) 申请公布日期 2016.01.28
申请号 US201514805168 申请日期 2015.07.21
申请人 Airbus Operations (SAS) 发明人 Chirol Clement;Achard Victor
分类号 B32B3/26;B32B5/26 主分类号 B32B3/26
代理机构 代理人
主权项 1. A method of reinforcing a composite material part comprising a stack of fiber layers and at least one hole with an axis, said hole crossing said layers and opening out at the level of a first face and a second face of said part, said part having a thickness at the level of the axis of the hole, wherein the method comprises at least one stage comprising the making of at least one notch in at least one layer of the part proximate to the hole or which opens out in the hole.
地址 Toulouse FR