The invention discloses a rear ventilation cooling device of a
piston engine, and relates to the technical field of unmanned aerial vehicle
piston engines, an engine fairing and a
fuselage are coordinated in appearance for aerodynamic design, an
air channel door is completely attached to the fairing after being closed, the opening degree is controllable after the
air channel door is opened, cooling
airflow is introduced into an
air channel from an external flow field, and closed-
loop control over an engine cylinder body is achieved through adjustment of the air inflow. According to the flightspeed of the unmanned aerial vehicle, the environment temperature and the engine cylinder temperature, the air passage door is controlled to be opened at different opening degrees, the engine cylindertemperature is controlled within the optimal temperature range, the engine cooling air entraining requirement is met, and the flight resistance can be reduced.
Forced convection heat dissipation is conducted on the engine cylinder body in the flow guide cover, cooling
airflow flows out of a rear opening of the flow guide cover, the section of the rear opening of the flow guide cover is close to the rotating plane of the
propeller, auxiliary heat dissipation can be conducted through the suction effect of the
propeller during work, the cylinder
body cooling response speed is high, the structureis simple, and the
cooling efficiency is high.