Turbine component with a thin interior partition
AssigneeUnited Technologies Corporation
InventorsDilip M. Shah, Alan D. Cetel, Venkatarama K. Seetharaman, Raymond Surace
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Abstract
A hollow turbine airfoil or a hollow turbine casting including a cooling passage partition. The cooling passage partition is formed from a single crystal grain structure nickel based super alloy, a cobalt based super alloy, a nickel-aluminum based alloy, or a coated refractory metal.
Claims18
A hollow turbine airfoil comprising a cooling passage partition comprising a single crystal grain structure nickel based super alloy, a cobalt based super alloy, a nickel-aluminum based alloy, or a coated refractory metal.
A hollow turbine casting comprising a cooling passage partition comprising a single crystal grain structure nickel based super alloy, a cobalt based super alloy, a nickel-aluminum based alloy, or a coated refractory metal.
Dependencies are inferred from the claim text.