发明名称 Unitized assembly including substructure element integral with fiber metal laminate
摘要 A unitized assembly may comprise a fiber metal laminate and at least one additive layer. The fiber metal laminate may have non-metallic plies bonded to metallic plies and may include an innermost metallic ply. The at least one additive layer may be deposited onto the innermost metallic ply by friction stir welding.
申请公布号 US9027820(B2) 申请公布日期 2015.05.12
申请号 US201414172721 申请日期 2014.02.04
申请人 The Boeing Company 发明人 Heck David P.;Strahm Loren J.
分类号 B23K20/12;B64C1/12;B32B15/14;B29C65/06;B64C1/00 主分类号 B23K20/12
代理机构 代理人
主权项 1. A unitized assembly, comprising: a fiber metal laminate having non-metallic plies bonded to metallic plies including an innermost metallic ply; a first additive layer; and successively-applied additive layers; the first additive layer friction stir welded onto the innermost metallic ply, the first additive layer having a thickness less than each successively-applied additive layer, the innermost metallic ply having a thickness greater than a thickness of the other metallic plies; a boundary of a weld nugget joining the first additive layer and the innermost metallic ply is located above a first non-metallic ply and the weld nugget is smaller than a second friction stir weld nugget joining a successively applied additive layer to the first additive layer.
地址 Chicago IL US