| 发明名称 |
CO-CURING PROCESS FOR THE JOINING OF COMPOSITE STRUCTURES |
| 摘要 |
A method of fabricating a composite assembly may include providing a first laminate and a second laminate respectively formed of first and second composite plies, and having a respective first and second cured section and a respective first and second uncured section. The method may further include interleaving the first composite plies in the first uncured section with the second composite plies in the second uncured section to form an interfacial region. The method may additionally include curing the interfacial region to join the first laminate to the second laminate and form a unitized composite assembly. |
| 申请公布号 |
US2016257427(A1) |
申请公布日期 |
2016.09.08 |
| 申请号 |
US201514639112 |
申请日期 |
2015.03.04 |
| 申请人 |
The Boeing Company |
发明人 |
Humfeld Keith D.;Nelson Karl M. |
| 分类号 |
B64F5/00;B29C70/30;B29C65/02 |
主分类号 |
B64F5/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of fabricating a composite assembly, including:
providing a first laminate and a second laminate respectively formed of first and second composite plies and having a respective first and second cured section and a respective first and second uncured section; interleaving at least one of the first composite plies in the first uncured section with the second composite plies in the second uncured section to form an interfacial region; and curing the interfacial region to join the first laminate to the second laminate and form a unitized composite assembly. |
| 地址 |
Chicago IL US |
