The invention discloses a large-load fixed-wing bomb dropping unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The large-load fixed-wing bomb-dropping unmanned aerial vehicle is composed of a vehicle body, main wings, ailerons, a horizontal
tail wing, a vertical
tail wing and a
rudder. A main beam of the main wing is formed by CNC (computer
numerical control)
processing of a PMI (polymethacrylimide) material, and thin-layer carbon sheets are adhered to the upper and lower parts of the main beam and are The
aileron PMI foam is made of a material; the horizontal empennage, the vertical empennage and the
rudder are of
cork wood frame
skin structures; the
fuselage adopts four square carbon tubes as a longitudinal main force transmission structure to bear main loads in the flying process; the power
system mainly adopts a two-
stroke 3.5 cc
methanol engine as a power source, and is provided with a set of
speed reduction group gears, so that the rotating speed is reduced, and the output is increased. Compared with an existing design, the loading capacity of the unmanned aerial vehicle
system is improved, meanwhile, light weight, low cost,
high loading capacity and high maneuverability are taken into consideration, and after the
missile cabin is transformed, specific tasks in other fields can be executed by additionally installing instruments and equipment in other fields.