The invention relates to the field of electric manned aircrafts, in particular to a light electric manned aircraft. The light electric manned aircraft comprises a flight main body, a heat dissipation mechanism, a battery mechanism and a lift mechanism, a cabin and a battery cabin are formed on the flight main body, and the battery cabin is located above the cabin in the vertical direction; the heat dissipation mechanism is installed in the battery cabin, the battery mechanism is contained in the battery cabin and installed on the heat dissipation mechanism, and the lift mechanism is installed on the flying main body, located at the battery cabin and connected with the battery mechanism. In this way, the battery compartment plays a role of a structural shell for the battery mechanism, and therefore the fusion design of the battery mechanism and the flight main body is achieved; and meanwhile, the heat dissipation mechanism not only dissipates heat of the battery mechanism, but also plays a role in supporting the battery mechanism, so that a supporting piece does not need to be arranged at the bottom of the battery mechanism, and the weight of the electric manned aircraft is further reduced under the condition of ensuring heat dissipation.
本申请涉及电动载人飞行器领域,特别是涉及一种轻型电动载人飞行器。轻型电动载人飞行器包括飞行主体、散热机构、电池机构以及升力机构,飞行主体上形成有座舱和电池舱,且沿竖直方向,电池舱位于座舱的上方;散热机构安装于电池舱内,电池机构收容于电池舱内,且安装于散热机构上,升力机构安装于飞行主体上并位于电池舱处,且升力机构与电池机构连接。如此,电池舱对电池机构起到结构外壳的作用,从而实现电池机构和飞行主体的融合设计;同时,散热机构既对电池机构进行散热,又对电池机构起到支撑的作用,因此无需在电池机构的底部设置支撑件,在保证散热的情况下进一步减轻了电动载人飞行器的重量。
Light electric manned aircraft
轻型电动载人飞行器
2023-06-30
Patent
Electronic Resource
Chinese
Power device of electric manned aircraft and electric manned aircraft
European Patent Office | 2021
|European Patent Office | 2021
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