Inventors:
Gene C. F. Tsai - Lexington MA
Sung Tung - Lexington MA
Terence C. Flaherty - Marblehead MA
Robert F. Manning - Newburyport MA
Assignee:
General Electric Company - Cincinnati OH
International Classification:
F01D 508
Abstract:
An airfoil for use in a gas turbine engine includes a pressure side and a suction side joined at a trailing edge wall that defines a trailing edge. The airfoil includes at least one cooling hole extending through the trailing edge wall so as to pass cooling fluid from the pressure side of the airfoil to the suction side.