| 发明名称 |
Method, System and Apparatus for Assembling a Composite Wing Skin with Stiffeners |
| 摘要 |
A jig apparatus and associated systems and methods for forming a composite wing skin is presented, including providing a frame with a working surface. A plurality of indexing blocks are coupled to the working surface of the frame. Each of the plurality of indexing blocks has a first indexing surface oriented perpendicular to the working surface of the frame and a second indexing surface oriented approximately parallel to the working surface of the frame. A plurality of clamping blocks are also each moveably coupled to one of the plurality of indexing blocks. Each of the plurality of clamping blocks has a clamping surface oriented perpendicular to the working surface of the frame and in facing relation to the first indexing surface of an adjacent indexing block thereby defining a plurality of channels. |
| 申请公布号 |
US2016244185(A1) |
申请公布日期 |
2016.08.25 |
| 申请号 |
US201514629131 |
申请日期 |
2015.02.23 |
| 申请人 |
The Boeing Company |
发明人 |
Pham Doan Dinh;Iden Mark Charles |
| 分类号 |
B64F5/00 |
主分类号 |
B64F5/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A jig apparatus for forming a composite wing skin, the jig apparatus comprising:
a frame with a working surface; a plurality of indexing blocks coupled to the working surface of the frame, wherein each of the plurality of indexing blocks has a first indexing surface oriented perpendicular to the working surface of the frame and a second indexing surface oriented parallel to the working surface of the frame; and a plurality of clamping blocks each moveably coupled to one of the plurality of indexing blocks, wherein each of the plurality of clamping blocks has a clamping surface oriented perpendicular to the working surface of the frame and in facing relation to the first indexing surface of an adjacent indexing block thereby defining a plurality of channels. |
| 地址 |
Chicago IL US |
