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 |