发明名称 Rework system for composite structures
摘要 A method and apparatus for reworking a composite structure. A fastener is cooled from a first temperature to a second temperature at which a diameter of a post of the fastener is reduced by a desired amount. The post of the fastener is placed into a channel in a bushing such that a desired interference fit occurs when the fastener is at the first temperature. The bushing with the fastener is positioned in a hole in the composite structure. A gap is present between an outer surface of the bushing and an inner surface of the hole. A gap is also present between an end of the bushing and a second structure.
申请公布号 US9498855(B2) 申请公布日期 2016.11.22
申请号 US201414243468 申请日期 2014.04.02
申请人 THE BOEING COMPANY 发明人 Gordon David Jonathan;Vrinceanu Catalin T.
分类号 B23P6/00;B23P11/02;F16B33/00;F16B4/00;F16B5/02;F16B19/02 主分类号 B23P6/00
代理机构 Yee & Associates, P.C. 代理人 Yee & Associates, P.C.
主权项 1. A method for reworking a composite structure, the method comprising: cooling a fastener from a first temperature to a second temperature at which a diameter of a post of the fastener is reduced by a desired amount; placing the post of the fastener into a channel in a bushing such that a desired interference fit occurs when the fastener is at the first temperature; positioning the bushing with the fastener in a hole in the composite structure, wherein a gap is present between an outer surface of the bushing and an inner surface of the hole; positioning a nut on an end of the post of the fastener; and tightening the nut to reduce a gap present between the end of the bushing and a second structure such that a desired amount of space remains between an end of the bushing and the second structure.
地址 Chicago IL US