The invention discloses an aero-engine cooling device. The aero-engine cooling device structurally comprises a device body, a water inlet valve, ventilation ports and water flow channels, wherein theinner part of the device body is hollow, the shape of the device body is cylindrical, the water inlet valve communicates with an outer shell, moreover, the connecting mode of the water inlet valve andthe outer shell is a fixed connection mode, the outer shell is connected with an inner shell through the ventilation ports, the ventilation ports are uniformly distributed on the device body, the water flow channels are distributed around the ventilation ports, the water flow channels communicate with one another, moreover, the water flow channels are closed in the device body, the connecting mode of the inner shell and fixing screw holes is a fixed connection mode, the fixing screw holes are uniformly distributed inside the device body. According to the aero-engine cooling device, the waterinlet valve, the ventilation ports and the water flow channels are arranged on the aero-engine cooling device so that water cooling, air cooling and air flow cooling can be performed when an aero-engine is used, so that the cooling modes of the aero-engine are greatly increased, and the functionality is complete.