The present invention relates to the technical field of gas
turbine hot end cooling, and discloses a flat cat-ear air film hole cooling structure and a construction method for
gas turbines, comprising a
solid wall with an outer wall surface and an inner wall surface, the outer wall surface being used to contact a high-temperature mainstream; the air film hole comprising an elliptical column section opened on the
solid wall and an expansion section connected to and coaxial with the elliptical column section, the connection between the elliptical column section and the expansion section being an inlet profile line, a
cold air inlet being formed on the inner wall surface at one end of the elliptical column section away from the expansion section, a
cold air outlet being formed on the outer wall surface at one end of the expansion section away from the elliptical column section, and the profile line of the
cold air outlet being an outlet profile line. The present invention can form an ideal anti-
kidney vortex structure, promote the
lateral expansion of cold air, increase the air film coverage area in the direction of the air film, enhance the air film wall attachment effect, thereby improving the air film
cooling efficiency, and at the same time can form a relatively uniform slit-shaped outflow, reducing the aerodynamic loss of the mixing of cold air and the mainstream.