The application discloses a
hydrogen fuel
control system for unmanned aerial vehicles, which comprises a
hydrogen bottle, a pressure reducing valve, a
hydrogen inlet valve, a first
pressure sensor, a fuel
cell stack, a steam-water separator, a double-variable
peristaltic pump, a second
pressure sensor, a controller, a drain valve, a temperature sensor and a
current sensor. The
system constitutes a closed hydrogen circulation loop to recover unreacted hydrogen. The controller monitors the hydrogen circulation pressure, the stack temperature and the load current in real time through a sensing network composed of double pressure sensors, a temperature sensor and a
current sensor, analyzes the load change and the water-heat state based on the built-in program, and cooperatively regulates the rotating speed and the
extrusion degree of the double-variable
peristaltic pump, dynamically optimizes the flow and the flushing intensity of the hydrogen circulation. The
system solves the water-
heat management problem of the fuel
cell of the unmanned aerial vehicle under dynamic working conditions, improves the hydrogen
utilization rate, effectively prevents
water flooding and membrane
dryness, and guarantees the efficient, stable and long-life operation of the
system.