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
WO2016196277(A1)
申请公布日期
2016.12.08
申请号
WO2016US34613
申请日期
2016.05.27
申请人
LOCKHEED MARTIN CORPORATION
发明人
BARNES, Nicholas, L.;ALDERFER, Ryan, M.;MARLEY, Timothy, J.;SCHOBER, Stephen, J.
