发明名称 In-Situ, Multi-Stage Debulk, Compaction, and Single Stage Curing of Thick Composite Repair Laminates
摘要 A method for fabricating a repair laminate for a composite part having an exposed surface includes applying a bonding material to the exposed surface and forming an uncured ply stack assembly on the bonding material. The uncured ply stack assembly is formed by forming and compacting a series of uncured ply stacks. The ply stack assembly and bonding material are then cured.
申请公布号 US2015251363(A1) 申请公布日期 2015.09.10
申请号 US201514716520 申请日期 2015.05.19
申请人 BELL HELICOPTER TEXTRON INC. 发明人 Whitworth Denver Ray;Cribb, III Vance Newton;Jitariu Dumitru Radu
分类号 B29C73/10 主分类号 B29C73/10
代理机构 代理人
主权项 1. A method for fabricating a repair laminate for a composite part having an exposed surface, comprising: applying bonding material to the exposed surface; applying a first ply stack to the bonding material, the first ply stack having a first plurality of uncured plies; compacting the first plurality of uncured plies; applying a second ply stack to the first cured ply stack, the second ply stack having a second plurality of uncured plies; compacting the second plurality of uncured plies; and curing the ply stack assembly and bonding material.
地址 Fort Worth TX US