The utility model provides a fuel
cell structure for an aerocar, which relates to the technical field of aerocar
fuel cells and comprises a U-shaped conductive plate, the outer wall of the U-shaped conductive plate is subjected to conductive anti-
corrosion treatment and is in contact with a membrane
electrode, a radiating fin and a sealing
gasket are integrated on the inner wall of the U-shaped conductive plate, and the U-shaped conductive plate is packaged to form a bipolar plate
assembly; a plurality of bipolar plate assemblies and a membrane
electrode are overlapped to form an electric
pile, the electric
pile is covered with a wind scooper and is in sealed connection with a cooling fan to form a
forced convection heat dissipation channel, and cooling air is filtered by filter cotton at a negative pressure opening of the electric
pile and then is subjected to closed-loop circulation heat dissipation. A shock pad is arranged at the bottom of the galvanic pile and connected with a hovercar body through a
system shock absorption support, a
hydrogen supply
system is separated from an electric appliance chamber through a separation plate, and a main gas
storage tank circulates to an
anode flow field after the flow is adjusted through a
proportional valve; the air supply
system supplies air to the
cathode flow field through an
air compressor and a humidifier. The utility model has the advantages of compact structure,
high heat dissipation efficiency, strong
shock resistance, low maintenance cost and the like, and is suitable for the field of eVTOL hovercars.