Anti-icing system of unmanned aerial vehicles

摘要

The invention relates to the field of aviation engineering, namely to the deicing system UAV and may be used to prevent icing of the wing leading edge and air pressure of the receiver tube. Deicing system of unmanned aircraft includes a heated tube, the ejection tube mixed hot air and an ejector disposed between the silencer of the internal combustion engine and the heating tubes. Using the proposed utility model prevents icing of the leading edge and air pressure of the receiver tube of the drone and creates the optimum temperature for his equipment, machinery and payload. 2 FIG.