| 发明名称 |
COMPOSITE OVER WRAP |
| 摘要 |
A composite wrap is provided for damping vibration in an elongated quill shaft having a cylindrical body. The composite wrap includes interior layering for disposition about a cylindrical body, exterior layering configured to define an exterior composite wrap shape and sequential cured-in-place, vibration damping, fibrous epoxy layers. The sequential cured-in-place, vibration damping, fibrous epoxy layers are radially interposed between the interior and exterior layering to dampen vibrations of and/or to adjust a resonance frequency of the cylindrical body. |
| 申请公布号 |
US2017058990(A1) |
申请公布日期 |
2017.03.02 |
| 申请号 |
US201615180334 |
申请日期 |
2016.06.13 |
| 申请人 |
Sikorsky Aircraft Corporation |
发明人 |
Bremmer Jonathan;Sauer Jeffrey G.;Lacko Robert A.;Song Shihong G.;Meeson John H. |
| 分类号 |
F16F15/12;B32B27/38;B64C27/14;B32B25/08;F16C3/02;B64C27/00;B32B5/12;B32B27/34 |
主分类号 |
F16F15/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A composite wrap for damping vibration in an elongated quill shaft having a cylindrical body, the composite wrap comprising:
interior layering for disposition about the cylindrical body; exterior layering configured to define an exterior composite wrap shape; and sequential cured-in-place, vibration damping, fibrous epoxy layers radially interposed between the interior and exterior layering to dampen vibrations of and/or to adjust a resonance frequency of the cylindrical body. |
| 地址 |
Stratford CT US |
