Radial turbine nozzle vane

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/00 (2006.01) B21D 53/78 (2006.01) B21H 7/16 (2006.01) F01D 9/04 (2006.01)

Patent

CA 2112597

A radial inflow turbine having a radial nozzle assembly comprising a plurality of vanes, wherein downstream of the throat, the vane suction surfaces, relative to a radius of the circle on which the vane trailing edges lie, have a specified range of angles, or decreasing radii of curvature.

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