The invention belongs to the technical field of vortex eliminating structures, and particularly relates to a T-shaped groove tip vortex structure, a pump-jet
propeller comprising the T-shaped groove tip vortex structure and a design method of the T-shaped groove tip vortex structure. The T-shaped groove tip vortex structure is composed of an annular groove 1b and rectangular grooves 1a which are evenly formed in the front side of the annular groove 1b in an
annular array mode. The bottoms of the rectangular groove 1a and the annular groove 1b are flush, the front and rear side wall surfaces are perpendicular to the rotor shaft, and the left and right side wall surfaces are perpendicular to the bottom surface. The grooves are formed in the inner wall of the guide
pipe, so that the
tip clearance of the rotor is increased, the
radial gradient of the speed is reduced, the radial free vortex becomes dispersed, the speed of
discharge flow and the
pressure difference between the tip pressure surface and the
suction surface are reduced, the strength of
tip clearance separation vortex and
discharge flow are weakened, fusion of the separation vortex and the
discharge flow is weakened, and the strength of the tip vortex is reduced; damage and dissipation effects of the inner wall of the groove on vortexes and discharge flow are achieved; the annular structure at the
tail end of the groove prolongs the action interval of the groove on the tip discharge vortex, and finally a good
cavitation inhibition effect is achieved.