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 |
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代理人 |
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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 |