发明名称 Method of manufacturing a structure
摘要 A method of manufacturing a structure, the method comprising: forming a panel assembly by bonding a stack of thickness control plies of composite material to a laminar composite panel, the stack of thickness control plies having a first edge proximate an edge of the laminar composite panel, a second edge opposite the first edge, and a ramp where the thickness of the stack of thickness control plies decreases towards the first or second edge; measuring the thickness of the laminate composite panel or the panel assembly; controlling the number of thickness control plies in accordance with the measured thickness; attaching a first component to the panel assembly, the first component having a surface which engages the laminar composite panel and a ramp which engages the ramp in the stack of thickness control plies; and attaching the laminar composite panel at or near its edge to a further component.
申请公布号 US9162417(B2) 申请公布日期 2015.10.20
申请号 US201313944489 申请日期 2013.07.17
申请人 AIRBUS OPERATIONS LIMITED 发明人 Iliopoulos Alex;Flood John
分类号 B32B41/00;B32B3/26;B64C3/18;B64C3/26;B29C70/34;B29K707/04;B29K709/08;B29L31/30;B64C1/12;B64C1/26 主分类号 B32B41/00
代理机构 Hauptman Ham, LLP 代理人 Hauptman Ham, LLP
主权项 1. A structure comprising: a panel assembly comprising a stack of thickness control plies of composite material bonded to a laminar composite panel, the stack of thickness control plies having a first edge proximate an edge of the laminar composite panel, a second edge opposite the first edge, a ramp where the thickness of the stack of thickness control plies decreases towards the first or second edge, and an unramped section where the thickness of the stack of thickness control plies is substantially constant; a first component attached to the panel assembly, the first component having a surface which engages the laminar composite panel, a ramp which engages the ramp in the stack of thickness control plies, and an unramped surface which engages the unramped section in the stack of thickness control plies; and a further component attached to the laminar composite panel at or near its edge.
地址 Bristol GB