发明名称 Structure repair with polymer matrix composites
摘要 An assembly is provided including a structural component having a flange-like member. A partially cured polymer matrix composite patch is wrapped around a perimeter of the flange-like member. The patch includes a plurality of layers, each layer having a plurality of fibers arranged therein. The layers of the polymer matrix composite patch are cured after being wrapped around the flange-like member of the structural component.
申请公布号 US9243407(B2) 申请公布日期 2016.01.26
申请号 US201313870182 申请日期 2013.04.25
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 Zhao Wenping;Chaudhry Zaffir A.
分类号 B29C73/10;E04C5/07;B64F5/00;B32B5/02;B32B5/26;B32B7/12 主分类号 B29C73/10
代理机构 Cantor Colburn LLP 代理人 Cantor Colburn LLP
主权项 1. A method of forming a polymer matrix patch about a load-bearing, metallic structural component, comprising: wrapping a plurality of layers around the surface of a flange-like member of the load-bearing, metallic structural component in-situ, such that the patch extends parallel to an axis of the flange-like member and wraps equidistantly, over two opposing sides of the load-bearing metallic structural component such that a first end and a second, opposite end of each the plurality of layers is arranged within a same plane on opposing sides of the structural component, each layer having a plurality of fibers arranged therein; and curing the plurality of layers.
地址 Stratford CT US