| 发明名称 |
Adjustable splice fitting for shimless connection of structual members |
| 摘要 |
A fuselage section may include a structural member and a frame member having a stub frame extending over the structural member. The stub frame may have a web. The fuselage section may include an intercostal extending from a terminal end of the stub frame and having an end flange. The fuselage section may additionally include an adjustable splice fitting having a web, a lower flange, and an end flange being mountable in faying contact with respective ones of the stub frame web, the structural member, and the intercostal end flange. |
| 申请公布号 |
US8740151(B1) |
申请公布日期 |
2014.06.03 |
| 申请号 |
US201213342418 |
申请日期 |
2012.01.03 |
| 申请人 |
The Boeing Company |
发明人 |
Rosman Richard R.;Lakic Branko;Cominsky Kenneth;Marciniak Douglas;Pearson Steven Edward |
| 分类号 |
B64C1/00 |
主分类号 |
B64C1/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fuselage, comprising:
a fuselage section including a structural member; a frame member including a stub frame extending over the structural member and having a web; an intercostal extending from a terminal end of the stub frame and having an end flange; and an adjustable splice fitting having a web, a lower flange, and an end flange being mountable in faying contact with respective ones of the stub frame web, the structural member, and the intercostal end flange.
|
| 地址 |
Chicago IL US |
