| 发明名称 |
Solar-Powered Aircraft |
| 摘要 |
The present invention is directed to a solar-powered aircraft comprising a fixed wing panel, a motor driven propeller, a plurality of secondary wing panels, and a tail assembly having a first tail panel and a second tail panel. Each secondary wing panel being configured to rotate about a first longitudinal pivot axis extending from a distal end of the fixed wing panel through a central transverse portion of the secondary wing panel. The secondary wing panels may comprise an array of solar panels on its surface. The first tail panel comprises a second array of solar panels located on a surface of the first tail panel, the first tail panel being configured to rotate about a second longitudinal pivot axis through a central transverse portion of the first tail panel. |
| 申请公布号 |
US2016311545(A1) |
申请公布日期 |
2016.10.27 |
| 申请号 |
US201615134938 |
申请日期 |
2016.04.21 |
| 申请人 |
Aurora Flight Sciences |
发明人 |
Parks Robert W.;Giannini Francesco |
| 分类号 |
B64D31/00;B64C5/02;B64C3/42;B64C3/00 |
主分类号 |
B64D31/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A solar-powered aircraft comprising:
a fixed wing panel; a motor driven propeller; a plurality of secondary wing panels, each of said plurality of secondary wing panels configured to rotate about a first longitudinal pivot axis extending from a distal end of the fixed wing panel through a central transverse portion of the secondary wing panel,
wherein each of said plurality of secondary wing panels comprises a first array of solar panels on its surface; and a tail assembly having a first tail panel and a second tail panel,
wherein the first tail panel comprises a second array of solar panels located on a surface of the first tail panel, the first tail panel being configured to rotate about a second longitudinal pivot axis through a central transverse portion of the first tail panel. |
| 地址 |
Manassas VA US |
