The invention provides a gas turbine blade comprising V rib-pit composite cooling structures. The gas turbine blade comprises an upper wall and a lower wall, wherein the upper wall is a suction surface, the lower wall is a pressure surface, the V rib-pit composite cooling structures are arranged on the inner walls of the upper wall and the lower wall, each V rib-pit composite cooling structure comprises a composite cooling unit, wherein the composite cooling unit comprises a right-angle V-rib and a circular pit behind the right-angle V-rib. The gas turbine blade has the advantages that the heat exchange area of the whole structure is increased, the heat exchange effect is improved, a fracture between the adjacent V-shaped ribs enhances the turbulent flow generated by the gas flow, so thatthe gas flow is separated to a large extent, and then is attached to the wall surface, so that the boundary layer is damaged in a large extent, the turbulence degree of the fluid is greatly enhanced,the heat exchange is greatly enhanced, the rib are interrupted, so that the blockage ratio is reduced, the pressure loss is reduced, the disturbance is enhanced while the front and rear air pressure of the rib is balanced, and the heat exchange is greatly enhanced.