发明名称 Smooth surface forming tool and manufacture thereof
摘要 An aircraft article composite forming tool and a method for producing the tool. The aircraft article to be formed includes a composite material including an outer surface. The aircraft article composite forming tool includes a matrix laminate made of at least an upper ply including a forming surface for forming the aircraft article and outer surface. The upper ply includes a nano filament structure embedded therein.
申请公布号 US9180979(B2) 申请公布日期 2015.11.10
申请号 US201013642898 申请日期 2010.02.04
申请人 SAAB AB 发明人 Hallander Per;Petersson Mikael;Weidmann Björn;Grankäll Tommy;Strindberg Göte;Nordin Pontus
分类号 B29C33/02;B64F5/00;B29C45/73;B29C33/40;B29C70/44;B29C70/88;B82Y30/00;B29K105/16 主分类号 B29C33/02
代理机构 Venable LLP 代理人 Venable LLP ;Franklin Eric J.
主权项 1. An aircraft article composite forming and curing tool, wherein an aircraft article to be formed comprises a composite material including an outer surface, the aircraft article composite forming tool comprising: a cured matrix laminate, being a polymeric composite face sheet, comprising an upper ply including a forming surface for forming said aircraft article outer surface, wherein the upper ply comprises a nano filament structure embedded therein, wherein the matrix laminate comprises a plurality of laid-up plies, a portion of the laid-up plies comprising a nano filament structure and controllable heating elements comprising nano filament structure in suitable positions of the matrix laminate, such that a portion of the nano filament structure is exposed on the forming surface, and wherein at least a portion of the nano filament structure is coupled to an energy supply to heat the forming surface.
地址 Linköping SE