Controlled reaction l-2r steam turbine blade

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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F01D 5/00 (2006.01) F01D 5/14 (2006.01)

Patent

CA 2091698

57,269 ABSTRACT OF THE DISCLOSURE A high performance steam turbine blade is provided in which the geometry of the blade airfoil is configured to minimize energy loss through the row of blades and control the radial distribution of the degree of reaction. The velocity of the steam over the blade surface is minimized to reduce friction losses, rapid deceleration of the steam velocity as it expands toward the trailing edge is avoided to prevent boundary layer separation and the reaction distribution is adjusted so that a relatively high reaction occurs at the base of the airfoil, thereby reducing secondary flow, and a relatively low reaction occurs at tip of the airfoil, thereby minimizing tip leakage.

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