| 发明名称 |
COMPOSITE STRUCTURE AND METHODS OF FORMING THEREOF |
| 摘要 |
A composite structure is provided. The composite structure includes a first stiffener, a second stiffener, and an intermediate structure positioned between the first and second stiffeners such that the first stiffener is coupled to a first side of the intermediate structure, and such that the second stiffener is coupled to a second opposing side of the intermediate structure. A first radius gap is defined at least partially between the first stiffener and the intermediate structure, and a second radius gap is defined at least partially between the second stiffener and the intermediate structure. |
| 申请公布号 |
US2016144943(A1) |
申请公布日期 |
2016.05.26 |
| 申请号 |
US201414281456 |
申请日期 |
2014.05.19 |
| 申请人 |
The Boeing Company |
发明人 |
Cheng Jiangtian;Vetter Derek Paul;Woodard Patrick Alan;Behzadpour Forouzan |
| 分类号 |
B64C1/06 |
主分类号 |
B64C1/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A composite structure comprising:
a first stiffener; a second stiffener; and an intermediate structure positioned between said first and second stiffeners such that said first stiffener is coupled to a first side of said intermediate structure, and such that said second stiffener is coupled to a second opposing side of said intermediate structure; a first radius gap defined at least partially between said first stiffener and said intermediate structure; and a second radius gap defined at least partially between said second stiffener and said intermediate structure. |
| 地址 |
Seal Beach CA US |
