A
turbine moving blade with an internal
cooling channel with a dustproof structure comprises a
rotational flow cavity arranged between ribbed U-shaped cooling channels in the moving blade, the
rotational flow cavity is connected with the cooling channels with inclined ribs through square nozzles, and the top of the
rotational flow cavity shrinks and is connected with a blade top dust removal hole through a hollow turbulent flow column of a channel
elbow. Under the rotating condition, particulate pollutants in the channel are gathered on the pressure face side of the channel and then enter the rotational flow cavity from the square
nozzle under induction of the inclined ribs. Tangently-incident
cold air forms rotational flow in the rotational flow cavity, particles are difficult to deposit in the rotational flow cavity due to the high tangential speed, and the particles can only enter the hollow channels of the turbulent flow columns along with the
cold air and finally flow out of the blades through the blade top dust removal holes. Under limited
cold air consumption, particles are separated from cold air and discharged out of the blades through rotation, the guiding effect of the turbulent flow ribs and
inertia of the particles, and the
heat transfer uniformity of the blades is optimized through rotational flow cooling.