| 发明名称 |
ENHANCED THERMALLY CONDUCTIVE PIVOT BUSHING |
| 摘要 |
An aircraft pivot joint bushing has enhanced thermal conductivity due to the bushing having an inner cylindrical portion which has a first thermal dissipating capacity, and an outer cylindrical portion on the inner cylindrical portion which has a second thermal dissipating capacity, where the second thermal dissipating capacity is less than the first thermal dissipating capacity. |
| 申请公布号 |
US2016047412(A1) |
申请公布日期 |
2016.02.18 |
| 申请号 |
US201414457729 |
申请日期 |
2014.08.12 |
| 申请人 |
The Boeing Company |
发明人 |
Stuk Christopher J.;Koch William J. |
| 分类号 |
F16C17/12;F16C43/02;F16C33/04;F16C17/02 |
主分类号 |
F16C17/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft pivot joint bushing comprising:
an inner cylindrical portion having a first thermal dissipating capacity; an outer cylindrical portion on the inner cylindrical portion, the outer cylindrical portion having a second thermal dissipating capacity, the second thermal dissipating capacity being less than the first thermal dissipating capacity. |
| 地址 |
Chicago IL US |
