The invention relates to a hydrogen-electricity hybrid power device for a hovercar. The hydrogen-electricity hybrid power device comprises a first-stage duct, a transition duct and a second-stage duct, the air outlet end of the first-stage duct is connected to the second-stage duct through the transition duct; a hydrogen reactor is arranged in the first-stage duct, and the hydrogen reactor is fixed with the first-stage duct through a plurality of supporting pieces A; a primary filter screen is arranged at the front end of the first-stage duct and is fixed on the first-stage duct through a hoop, so that low-altitude sundries and dust are prevented from entering the reactor. The backflow pipe is arranged, and the problems of oxygen supply, heat dissipation and cooling and the like of the hydrogen reactor are solved through duct airflow; the motor power supply requirement of the ducted fan is met; the defects that an airborne battery and a power device of an aerocar are large in mass, short in flight time and small in thrust are overcome. The weight of the aerocar can be reduced, the effective load of the aerocar is improved, and the flight distance of the aerocar is increased.
本发明涉及一种飞行汽车用氢电复合动力装置,包括第一级涵道、过渡涵道和第二级涵道;第一级涵道的出气端经过过渡涵道连接到第二级涵道;第一级涵道内设有氢反应堆,氢反应堆通过若干个支撑件A与第一级涵道进行固定;第一级涵道的前端设有初级滤网,初级滤网通过卡箍固定在第一级涵道上,防止低空杂物及灰尘进入反应堆。本发明设有回流管,利用涵道气流来解决氢反应堆的氧气供给、散热冷却等问题;解决了函道风扇的电机供电需求;本发明克服了飞行汽车机载电池及动力装置质量大、飞行时间短、推力小的缺点。能够减轻飞机重量,提升飞行汽车的有效载重、增加飞行汽车的飞行距离。
Hydrogen-electricity hybrid power device for hovercar and control method
一种飞行汽车用氢电复合动力装置及控制方法
18.10.2022
Patent
Elektronische Ressource
Chinesisch
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