| 发明名称 |
ROTORCRAFT ROTOR BLADE ASSEMBLY |
| 摘要 |
A rotorcraft rotor blade assembly includes an upper skin portion extending substantially a full span of the rotor blade assembly and a lower skin portion extending substantially the full span of the rotor blade assembly. Each of the upper skin portion and the lower skin portion is configured to carry at least substantially 30% of rotor blade assembly loads. |
| 申请公布号 |
US2017036759(A1) |
申请公布日期 |
2017.02.09 |
| 申请号 |
US201514817442 |
申请日期 |
2015.08.04 |
| 申请人 |
Bell Helicopter Textron Inc. |
发明人 |
Sutton Drew;Oldroyd Paul K.;Braswell, JR. James;Wolthuis Scott;Sherrill Paul |
| 分类号 |
B64C27/473 |
主分类号 |
B64C27/473 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A rotorcraft rotor blade assembly comprising:
an upper skin portion extending substantially a full span of the rotor blade assembly; and a lower skin portion extending substantially the full span of the rotor blade assembly, wherein each of the upper skin portion and the lower skin portion is configured to carry at least substantially 30% of rotor blade assembly loads. |
| 地址 |
Fort Worth TX US |
