Turbine blade with dual serpentine cooling

摘要

A turbine blade with a dual serpentine flow cooling circuit to provide cooling to the airfoil section and to the blade tip section. An aft flowing multiple pass serpentine circuit includes a first leg located adjacent to the leading edge region of the blade and is connected to a leading edge impingement cavity through a row of impingement holes. A showerhead arrangement is connected to the impingement cavity to provide film cooling to the leading edge of the blade. A second aft flowing serpentine circuit is located in the tip region and is connected to the impingement cavity to supply the cooling air to the second serpentine. A row of impingement holes and exit cooling slots is arranged along the trailing edge region and connected to the first serpentine. A trailing edge discharge hole is located in the tip region to discharge cooling air from the second serpentine. The second serpentine includes film cooling holes on the pressure side to discharge film cooling air. The first serpentine includes film cooling holes on the pressure side and the suction side to provide film cooling to selected areas of the pressure and the suction side walls.