The high-temperature gas leakage flow generated by the turbine tip clearance not only reduces the turbine efficiency

but also exacerbates the thermal load on the tip. Based on experimental model and numerical calculation method of fluid-solid coupling

the flow mechanism of the interaction between gap flow and cooling jet at the tip of turbine groove and the effect of top jet cooling on the heat transfer effect of the groove wall are studied. The effects of the ratio of cooling hole inclination angle

the cooling hole inlet angle

and the thermal conductivity of the solid material on the Nu number of the wall surface are analyzed. The results show that the large blow ratio (M=1.5) can effectively improve the heat transfer between the rib and the bottom of groove near the pressure side

and the Nu number distribution is more uniform. The "jet effect" generated by the intake angle changes the high-speed zone of the cooling airflow. Relative position of the outlet

when the intake angle β>0°

the cooling gas can effectively block the high temperature fluid to reduce the Nu number of the wall surface. The low thermal conductivity material reduces the convective heat transfer of the airflow to the solid wall

so that the convective heat transfer of the wall surface is more uniform.