| 发明名称 |
DEPLOYMENT MECHANISM |
| 摘要 |
A deployment or hinge mechanism and, more particularly, a compact unmanned aerial vehicle (UAV) wing deployment mechanism is provided. The deployment mechanism includes a hinged mechanism that stows in a stacked configuration and deploys in a level configuration. |
| 申请公布号 |
US2016355250(A1) |
申请公布日期 |
2016.12.08 |
| 申请号 |
US201615172710 |
申请日期 |
2016.06.03 |
| 申请人 |
LOCKHEED MARTIN CORPORATION |
发明人 |
Barnes Nicholas L.;Alderfer Ryan M.;Marley Timothy J.;Schober Stephen J. |
| 分类号 |
B64C3/56;B64C39/02 |
主分类号 |
B64C3/56 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A deployment mechanism, comprising a hinged mechanism that stows in a stacked configuration and deploys in a level configuration. |
| 地址 |
Bethesda MD US |
