| 发明名称 |
COMPOSITE JOINT OPTIMIZATION |
| 摘要 |
A method including receiving a joint parameter for a joint between at least two composite structural components, a ply stackup for each of the at least two composite structural components and an electromagnetic effect parameter in a controller, iteratively processing with the controller, the joint parameter and the ply stackup and outputting an optimized joint parameter based on at least a convergence of an electromagnetic effect resistance of the joint and the at least two composite structural components, and changing, with the controller, a value of one or more of the joint parameters and the ply stackup during the iterative processing to reach the convergence of the electromagnetic effect resistance. |
| 申请公布号 |
US2017032077(A1) |
申请公布日期 |
2017.02.02 |
| 申请号 |
US201514809336 |
申请日期 |
2015.07.27 |
| 申请人 |
The Boeing Company |
发明人 |
KHOSRAVANI Shahriar;NAKHJAVANI Omid B.;BELL Vincent;TENNYSON Laine;DABIRI Farhad |
| 分类号 |
G06F17/50;G06F17/11 |
主分类号 |
G06F17/50 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method comprising:
receiving a joint parameter for a joint between at least two composite structural components, a ply stackup for each of the at least two composite structural components and an electromagnetic effect parameter in a controller; iteratively processing with the controller, the joint parameter and the ply stackup and outputting an optimized joint parameter based on at least a convergence of an electromagnetic effect resistance of the joint and the at least two composite structural components; and changing, with the controller, a value of one or more of the joint parameters and the ply stackup during the iterative processing to reach the convergence of the electromagnetic effect resistance. |
| 地址 |
Chicago IL US |
