The invention discloses a tie piece structure for reducing turbulent flow losses. A wedge-shaped groove channel or a rectangular groove channel is formed in the position of an
airflow front
stagnation point of the tie piece structure in the radial direction of the tie piece structure, wherein the tie piece structure is an annular structure with the cross section being cylindrical or elliptical; the grooving length L of the tie piece structure is equal to 0.05R to 0.15 R, and R is the
radius of a tie piece or half of a
short axis of an
ellipse; the wedge-shaped inclination
angle alpha is equal to 0.3 degree, and when alpha is equal to 0 degree, the rectangular groove channel is formed. According to the tie piece structure, by means of grooving of the tie piece, high-energy fluid is injected into a low-energy fluid region at the
tail of the tie piece in a synthetic
jet flow manner, and therefore the capacity of the tie piece for resisting the adverse pressure gradient is improved, and the
tail vortex-shedding inhibition degree is improved; meanwhile, because the groove is formed in the position of the
airflow front
stagnation point of the tie piece, the tie piece flowing resistance is reduced to a great extent, and the efficiency of
turbine blades is effectively improved; and the tie piece structure reduces the additional
mass of the blades at the same time so that additional
centrifugal force loads can be reduced, and the safe running margin is effectively improved.