The invention discloses a
turbine moving blade internal composite cooling structure. The
turbine moving blade internal composite cooling structure comprises a
leading edge rotational flow cooling passage, a middle chord U-shaped cooling passage and a
tail edge trapezoidal cooling passage, wherein the U-shaped cooling passage comprises a U-shaped cooling passage inlet section, a U-shaped cooling passage outlet section and a U-shaped cooling passage top turning area which are integrally formed, wherein the U-shaped cooling passage inlet section and the U-shaped cooling passage outlet section communicate through the U-shaped cooling passage top turning area, and the U-shaped cooling passage inlet section, the U-shaped cooling passage outlet section and the
rotational flow cooling passage communicate through a plurality of
jet flow holes which are formed in a staggered mode; a plurality of ball sockets / ball protrusions and air film hole structures are arranged on the surface of the whole cooling passage; and a plurality of fin structures are arranged in the U-shaped cooling passage and the
tail edge trapezoidal cooling passage. According to the
turbine moving blade internal composite cooling structure, through
coupling of multiple structures, the structural strength of the blade is guaranteed, and the advantages of
high heat transfer,
low resistance, high adaptability and the like are achieved.