Improved performance low pressure end blading

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

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170/65

F01D 17/00 (2006.01) F01D 5/14 (2006.01)

Patent

CA 2011127

A method for optimizing thermodynamic performance of a steam turbine by matching a last stage blade flow area to condenser pressure by adjusting blade angular orientation to set gaging to an optimum value. The method is also used to correct incidence by setting blade angular orientation upstream of tho last blade row.

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