The solar aerostat system comprises a suspension ball unit, a hot-air balloon unit and a pod, the suspension ball unit is connected with the upper portion of the hot-air balloon unit, and the pod is connected with the lower portion of the hot-air balloon unit; the suspension ball unit is filled with suspension gas; variable hot air is filled into the hot air balloon unit; the surface of the suspension ball unit and/or the surface of the hot-air balloon unit are/is a solar cell film, and the solar cell film supplies power to the hot-air balloon unit and the pod. The invention further discloses a lift-off method of the solar aerostat system for planet exploration. The solar aerostat system has the advantages that the height of the solar aerostat system for planet exploration can be controlled and adjusted, and the solar aerostat system can reside for a long time.
本发明公开行星探测用太阳能浮空器系统,包括悬浮球单元、热气球单元、吊舱,所述悬浮球单元连接所述热气球单元的上部,所述吊舱连接所述热气球单元的下部;所述悬浮球单元内充入悬浮气体;所述热气球单元内充入可变量的热气;且所述悬浮球单元表面和/或热气球单元表面为太阳能电池薄膜,太阳能电池薄膜为所述热气球单元和吊舱供电。本发明还公开行星探测用太阳能浮空器系统的升空方法。本发明的有益效果:实现行星探测用太阳能浮空器系统的高度可控制调节以及能够长期驻留。
Solar aerostat system for planet exploration and lift-off method
行星探测用太阳能浮空器系统及升空方法
2024-01-05
Patent
Electronic Resource
Chinese
IPC: | B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / B64G Raumfahrt , COSMONAUTICS / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / H02S GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRA-RED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, E.G. USING PHOTOVOLTAIC [PV] MODULES , Erzeugung elektrischer Energie durch Umwandlung von Infrarot-Strahlung, sichtbarem Licht oder ultraviolettem Licht, z.B. unter Verwendung von Photovoltaik [PV]-Modulen |
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