| 发明名称 |
APPARATUS AND METHODS FOR JOINING COMPOSITE STRUCTURES OF AIRCRAFTS |
| 摘要 |
Apparatus and method for joining composite structures of aircrafts are disclosed. An example apparatus disclosed herein includes an inboard composite wing panel having a first end portion configured to be coupled to upper and lower inboard fittings composed of a metallic material and an outboard composite wing panel having a first end portion configured to be coupled to upper and lower outboard fittings composed of a metallic material. A side of body rib has a plate shaped first end portion composed of a metallic material. A fuselage frame is configured to be joined at one end of the upper inboard fitting, and the upper and lower inboard fittings and the upper and lower outboard fittings are coupled to the side of body rib at the plate shaped first end portion. |
| 申请公布号 |
US2015014484(A1) |
申请公布日期 |
2015.01.15 |
| 申请号 |
US201313938731 |
申请日期 |
2013.07.10 |
| 申请人 |
The Boeing Company |
发明人 |
Zeon Young;Achtner Gerfried Rudolf;Strachila Joseph |
| 分类号 |
B64C1/26;B64C3/18;B64C3/26 |
主分类号 |
B64C1/26 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An apparatus comprising:
an inboard composite wing panel having a first end portion configured to be coupled to upper and lower inboard fittings, the fittings composed of a metallic material; an outboard composite wing panel having a first end portion configured to be coupled to upper and lower outboard fittings, the fittings composed of a metallic material; a side of body rib having a plate shaped first end portion composed of a metallic material; and a fuselage frame configured to be joined at one end of the upper inboard fitting, the upper and lower inboard fittings and the upper and lower outboard fittings are coupled to the side of body rib at the plate shaped first end portion. |
| 地址 |
Chicago IL US |
