发明名称 SOLAR PROPELLED AIRCRAFT STRUCTURE AND SOLAR PANELS CONTROL METHOD
摘要 A solar propelled aircraft which has a wing having solar cell modules mounted therein includes: first solar cell modules which are positioned in a wing or a tail wing of the aircraft and receive solar energy directly from the sun; second solar cell modules which are positioned in a main wing or a tail wing of the aircraft and supplied with directed energy from the earth; and rotating shafts which rotate the first solar cell modules and the second solar cell modules so that the first solar cell modules and the second solar cell modules correspond to each other in both directions. The first solar cell module at the upper surface obtains solar energy from the sun, and the second solar cell module at the lower surface obtains directed energy transferred from the earth.
申请公布号 US2017029129(A1) 申请公布日期 2017.02.02
申请号 US201615292563 申请日期 2016.10.13
申请人 KOREA AEROSPACE RESEARCH INSTITUTE 发明人 AHN Hyo Jung
分类号 B64D27/24;H02S10/40;B64C3/32;H02S20/32 主分类号 B64D27/24
代理机构 代理人
主权项 1. A solar propelled aircraft structure which has solar cell modules mounted therein, the solar propelled aircraft structure comprising: first solar cell modules which are positioned in a wing or a tail wing of the aircraft and receive solar energy directly from the sun; and rotating shafts which rotate the first solar cell modules by a controller.
地址 Daejeon KR