Notched turbine vane baffle
AssigneeRtx Corporation
InventorsJaime G. Ghigliotty Rosado, Russell J. Bergman
Life of this patent
Estimating the term…
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AssigneeRtx Corporation
InventorsJaime G. Ghigliotty Rosado, Russell J. Bergman
Estimating the term…
An assembly for a turbine engine includes an airfoil and a baffle. A cavity projects spanwise into the airfoil from an airfoil tip end towards an airfoil base end. The baffle is disposed in the cavity with an outer passage formed between the baffle and a wall of the airfoil. The baffle extends spanwise from a baffle base end disposed at the airfoil base end to a baffle tip end disposed at the airfoil tip end. The baffle extends longitudinally from a baffle end to a baffle trailing edge. The baffle extends laterally between a baffle first side and a baffle second side. An inner passage projects spanwise into the baffle from the baffle tip end towards the baffle base end. A notch is disposed in the baffle trailing edge at the baffle base end. The notch fluidly couples the inner passage to the outer passage.
An assembly for a turbine engine, comprising:
An assembly for a turbine engine, comprising:
An apparatus for a turbine vane in a turbine engine, comprising:
Dependencies are inferred from the claim text.