发明名称 |
Mechanisms for deploying and actuating airfoil-shaped bodies on unmanned aerial vehicles |
摘要 |
Deployment and control actuation mechanisms are incorporated in unmanned aerial vehicles having folding wings and/or folding canards and/or a folding vertical stabilizer. The folding canards and folding vertical stabilizer can be deployed using respective four-bar over-center mechanisms. Elevators pivotably mounted to the folding canards and a rudder pivotably mounted to the folding vertical stabilizer can be controlled by means of respective twist link mechanisms. The folding wings have respective wing roots that are driven by respective gas springs to pivot on bearings about a wing root hub having control servo wire paths. |
申请公布号 |
EP2604510(A2) |
申请公布日期 |
2013.06.19 |
申请号 |
EP20120196943 |
申请日期 |
2012.12.13 |
申请人 |
THE BOEING COMPANY |
发明人 |
GETTINGER, JONATHAN DAVID |
分类号 |
B64C3/56;B64C5/12;B64C39/02 |
主分类号 |
B64C3/56 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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