| 发明名称 |
COMPOSITE FAILSAFE TORQUE TUBE |
| 摘要 |
An air vehicle control surface includes an upper skin, a lower skin, a plurality of composite spars extending between the upper skin and the lower skin, and a failsafe torque tube. The failsafe torque tube includes an outer composite tube and an inner tube disposed within the outer composite tube and extending coaxially with the outer composite tube. |
| 申请公布号 |
US2017106970(A1) |
申请公布日期 |
2017.04.20 |
| 申请号 |
US201514883672 |
申请日期 |
2015.10.15 |
| 申请人 |
The Boeing Company |
发明人 |
Stawski Stanley W. |
| 分类号 |
B64C9/02;B29D23/00;B29C53/56;B32B1/08;B32B15/092 |
主分类号 |
B64C9/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An air vehicle control surface, comprising:
an upper skin, a lower skin, a plurality of composite spars extending between the upper skin and the lower skin; and a failsafe torque tube comprising:
an outer composite tube; andan inner tube disposed within the outer composite tube and extending coaxially with the outer composite tube. |
| 地址 |
Chicago IL US |
