Dority & Manning, P.A.
Airfoil trailing edge segment
Turbine nozzle sections and airfoils having trailing edge segments are provided. In one embodiment, a turbine nozzle section comprises an inner band defining a pocket; an outer band defining an opening therethrough; and an airfoil radially extending from the inner band to the outer band and including pressure and suction sides. The airfoil has a body segment including a cavity and a plurality of ejector apertures defining a passageway from the cavity to an outer surface of the airfoil, and a trailing edge segment including an inner end and an outer end. The body segment defines a projection projecting inwardly from the suction side, and the trailing edge segment defines a notch opening toward the suction side. The projection is received within the notch. The inner end of the trailing edge segment is received within the inner band pocket, and the outer end is positioned within the outer band opening.
General Electric Company
F F F F F F F Y F F F F F
F05D F01D F01D F05D F01D F01D F05D Y02T F01D F01D F05D F05D F02K
additional inventional inventional additional inventional inventional additional additional inventional inventional additional additional additional
Matthew Mark Brandon ALIanson
Weaver Reynolds