The invention provides a
turbine guide vane structure with a rib upper through seam on a
trailing edge. The through seam is formed in a separation rib; after cooling
airflow passes through an outflow seam, part of cooling air can cool the interiors of the separation rib through the through seam in the separation rib, so that under the condition that the
cold air flow is not increased, the
convection heat exchange intensity of the inner wall surface and the side wall surface of the separation rib is enhanced, and the comprehensive
cooling effect of the
trailing edge is improved; preferably, the through seam is an inclined seam, when cooling
airflow passes through the separation rib, the strength of
cold air vortexes generated under the influence of the separation rib can be weakened, so that the interaction between lip plate falling vortexes and the
cold air vortexes can be weakened, and the air film
cooling efficiency of the surface of the separation rib is improved. The structure is reasonable in design and simple in structure, and the inclined seam is formed in the side wall surface of the separation rib, so that the
heat exchanger has good
heat transfer and cooling characteristics, has good
machining integrity and is more practicable.