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 US2017074302(A1) 申请公布日期 2017.03.16
申请号 US201615358026 申请日期 2016.11.21
申请人 The Boeing Company 发明人 Gordon David Jonathan;Vrinceanu Catalin T.
分类号 F16B5/02;F16B19/02;F16B33/00;F16B4/00 主分类号 F16B5/02
代理机构 代理人
主权项 1. A system for reworking a composite structure comprising: a fastener having a post with a first diameter at a first temperature that is greater than a second diameter at a second temperature; a bushing having a channel configured to receive the post, wherein the fastener and the bushing have a desired interference fit when the fastener is at the first temperature; and a cooling system configured to cool the fastener from the first temperature to the second temperature, wherein the bushing with the fastener is positioned in a hole of the composite structure with a gap between the bushing and the composite structure to rework the composite structure.
地址 Chicago IL US