| 发明名称 |
Skin Impact Snubber |
| 摘要 |
In some embodiments, an aircraft includes a structural assembly, a skin, and a snubber. The structural assembly comprises a first rigid element and a second rigid element. The first and second rigid elements are separated from each over by a void. The skin is disposed proximate to the structural assembly and adjacent to the void such that the skin would deflect into the void in response to an impact force received by the skin. The snubber is disposed in the void between the first and second rigid elements and positioned such that, when the skin deflects in response to the impact force, the skin contacts the snubber and the snubber reduces further deflection of the skin into the void. |
| 申请公布号 |
US2016185436(A1) |
申请公布日期 |
2016.06.30 |
| 申请号 |
US201414293250 |
申请日期 |
2014.06.02 |
| 申请人 |
Bell Helicopter Textron Inc. |
发明人 |
Wittmaak, JR. John R.;Hannan Philip J.;Lucas Maxx S.;Tiwari Chandrashekhar |
| 分类号 |
B64C1/06;B64C27/04 |
主分类号 |
B64C1/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft comprising:
a structural assembly comprising a first rigid element and a second rigid element, the first and second rigid elements separated from each over by a void; a skin disposed proximate to the structural assembly and adjacent to the void such that the skin would deflect into the void in response to an impact force received by the skin; and a snubber disposed in the void between the first and second rigid elements and positioned such that, when the skin deflects in response to the impact force, the skin contacts the snubber and the snubber reduces further deflection of the skin into the void. |
| 地址 |
Fort Worth TX US |
