| 发明名称 |
WING MOUNT ADJUSTMENT |
| 摘要 |
A mounting apparatus includes a fixed mounting structure that is fixed relative to a vehicle wing, the fixed mounting structure including a first fixed fitting and a second fixed fitting. The mounting apparatus further includes a rotatable mounting structure having a swivel fitting configured to engage the first fixed fitting and to swivel with respect to the first fixed fitting, the rotatable mounting structure also having a slide fitting configured to slide with respect to the second fixed fitting based on the swivel fitting being engaged with the first fixed fitting. |
| 申请公布号 |
US2015021436(A1) |
申请公布日期 |
2015.01.22 |
| 申请号 |
US201313947869 |
申请日期 |
2013.07.22 |
| 申请人 |
Sikorsky Aircraft Corporation |
发明人 |
Hainsworth Barton J.;Bossardet Donald M. |
| 分类号 |
B64C7/00 |
主分类号 |
B64C7/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A mounting apparatus, comprising:
a fixed mounting structure that is fixed relative to a vehicle wing, the fixed mounting structure including a first fixed fitting and a second fixed fitting; and a rotatable mounting structure having a swivel fitting configured to engage the first fixed fitting and to swivel with respect to the first fixed fitting, the rotatable mounting structure also having a slide fitting configured to slide with respect to the second fixed fitting based on the swivel fitting being engaged with the first fixed fitting. |
| 地址 |
Stratford CT US |
