Skin passageway trip strips
AssigneeRtx Corporation
InventorsJaime G. Ghigliotty Rosado, Brandon W. Spangler, David E. Gambardella, Benjamin B. Simpson
Life of this patent
Estimating the term…
Loading patent…
AssigneeRtx Corporation
InventorsJaime G. Ghigliotty Rosado, Brandon W. Spangler, David E. Gambardella, Benjamin B. Simpson
Estimating the term…
A turbine engine airfoil element has: an airfoil having: an exterior surface including a pressure side and a suction side; and a plurality of spanwise passageways including: a plurality of main body passageways along a camber line; and a plurality of skin passageways between the main body passageways and the exterior surface, wherein; the skin passageways have: a downstream direction from one or more inlets; a skin side; first and second lateral rounded transitions from the skin side; a parting line; and a longitudinally spaced plurality of protrusions from the skin side; and the protrusions have a height profile having: first and second tapering portions tapering from a maximum height, the first and second portions extending downstream; and first and second inwardly concave transitions to the skin passageway lateral rounded transitions.
A method for manufacturing a casting core, the casting core having:
A die for molding a casting core, the die having a closed condition and an open condition and comprising:
A die for molding a casting core, the die having a closed condition and an open condition and comprising:
Dependencies are inferred from the claim text.