Integrated electric propulsion unmanned aerial vehicle based on micro gas turbine

The invention belongs to the technical field of aircrafts and provides an integrated electric propulsion unmanned aerial vehicle based on a micro gas turbine. The integrated electric propulsion unmanned aerial vehicle based on a micro gas turbine comprises the micro gas turbine, a starting integrated machine, a storage battery, an air dynamic foil bearing, a motor, a propeller and electronic equipment, wherein the micro gas turbine comprises an air compressor, a turbine and a combustion chamber; the air compressor is connected to the turbine through the combustion chamber; air is sucked into the combustion chamber through the air compressor to be mixed and combusted with a fuel so as to generate fuel gas to propel the turbine to rotate; the starting integrated machine, the air compressor and the turbine are fixed to a supporting shaft through the air foil bearing; and the storage battery is connected to the motor, the propeller and the electronic equipment through cables. The integrated electric propulsion un