| 发明名称 | Bond assembly jig and method | ||
| 摘要 | A method for forming a composite structure on an assembly jig includes assembling an anchor member and block member on a support plate, arranging composite materials on the support plate adjacent to the anchor member, placing a shroud over the anchor member and block member, and applying heat and pressure to the bond assembly jig to cure the composite materials. | ||
| 申请公布号 | US9358732(B2) | 申请公布日期 | 2016.06.07 |
| 申请号 | US201514842381 | 申请日期 | 2015.09.01 |
| 申请人 | THE BOEING COMPANY | 发明人 | Lockleer John C.;Pham Doan D. |
| 分类号 | B29C70/54;B29C70/44;B25B11/02;B29D99/00;B29C33/30 | 主分类号 | B29C70/54 |
| 代理机构 | Parsons Behle & Latimer | 代理人 | Parsons Behle & Latimer |
| 主权项 | 1. A method of manufacturing a composite part on an assembly jig, comprising: attaching an anchor member on a support plate of an assembly jig; connecting a block member to the anchor member; arranging a first skin section on the support plate adjacent to the anchor member; arranging a spar on the block member and on the first skin section; arranging a core section on the first skin section; arranging a second skin section on the core section; removably attaching a shroud on the support plate, covering at least a portion of the anchor member without covering the first skin section and core section; enclosing the assembly jig in a chamber; and subjecting the assembly jig to heat and pressure to bond at least the first skin section to the core section. | ||
| 地址 | Chicago IL US | ||