Stationary blade design for l-oc row

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

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F01D 5/14 (2006.01)

Patent

CA 2054077

55,461 ABSTRACT OF THE DISCLOSURE A stationary blade of a steam turbine having a rotor and an inner cylinder for mounting the stationary blade in a row with plural identical stationary blades, comprising an airfoil having a leading edge, a trailing edge, a pressure-side concave surface and suction-side convex surface extending between the leading and trailing edges, A stagger angle being defined by as an angle of a chord between the leading and trailing edges to a longitudinal axis of the rotor; an outer ring for connecting a proximal end of the airfoil to the inner cylinder; an inner ring connected to a distal end of the airfoil; and a seal assembly carried by the inner ring and sealingly engaging the rotor; wherein the stagger angle ranges from about 42° at the distal end of the airfoil to about 52° at the proximal end.

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