Performance deterioration of the governing stage nozzle caused by solid particle erosion in the steam turbine

Abstract In the steam turbine, solid particle erosion on a nozzle cascade is known to damage the profile and surface smoothness of the cascade, which increases the flow loss of steam. The present study aims to make clear the relations between nozzle loss and surface degradation, aerodynamic parameters, as well as the shape, location, and size of the erosion notch. A series of numerical simulations were conducted to model the aerodynamic performance of various existing eroded nozzles. The results indicate that the nozzle loss caused by the surface degradation shows an approximate linear decrease with an increase in notch depth. The nozzle loss caused by the erosion notch increases with either a decrease in the exit Mach number or an increase of the notch area. For the same erosion-induced weight loss of the nozzle, the asymmetric notch and local notch cause more nozzle loss than the symmetric notch and quasi-global notch. This means that the performance deterioration can be reduced to a minimum value if the erosion is uniform along the span-wise of the nozzle. In addition, a combined experimental and numerical investigation is conducted to explore the erosion damage process of the nozzle. The result suggests that the eroded nozzle should be replaced by a new nozzle before the notch begins to propagate.

[1]  Paul W. Giel,et al.  Transonic turbine blade loading calculations using different turbulence models : effects of reflecting and non-reflecting boundary conditions , 2007 .

[2]  S. Thangam,et al.  Analysis of an RNG based turbulence model for separated flows , 1992 .

[3]  T. Coakley,et al.  Skin Friction and Velocity Profile Family for Compressible Turbulent Boundary Layers , 1993 .

[4]  Jr-Ming Miao,et al.  Numerical study of spacing effect on unsteady blade aerodynamics in a transonic turbine stage with different turbulence models , 2004 .

[5]  J. Moore,et al.  Secondary Flows and Losses Downstream of a Turbine Cascade , 1985 .

[6]  D. G. Gregory-Smith,et al.  Growth of Secondary Losses and Vorticity in an Axial Turbine Cascade , 1988 .

[7]  W. Tabakoff,et al.  The influence of coating processes and process parameters on surface erosion resistance and substrate fatigue strength , 1988 .

[8]  S. Orszag,et al.  Renormalization group analysis of turbulence. I. Basic theory , 1986, Physical review letters.

[9]  Zhenping Feng,et al.  Effects of Coating Thickness, Test Temperature, and Coating Hardness on the Erosion Resistance of Steam Turbine Blades , 2010 .

[10]  Yiping Dai,et al.  Nozzle passage aerodynamic design to reduce solid particle erosion of a supercritical steam turbine control stage , 2007 .

[11]  Asher Sigal,et al.  New correlation of roughness density effect on the turbulent boundary layer , 1990 .

[12]  John D. Denton,et al.  The 1993 IGTI Scholar Lecture: Loss Mechanisms in Turbomachines , 1993 .

[13]  Richard B. Rivir,et al.  Turbine Blade Surface Deterioration by Erosion , 2004 .

[14]  Siamack A. Shirazi,et al.  Numerical and experimental investigation of the relative erosion severity between plugged tees and elbows in dilute gas/solid two-phase flow , 2006 .

[15]  Widen Tabakoff,et al.  Erosion and Deposition in Turbomachinery , 2006 .

[16]  Richard B. Rivir,et al.  The Many Faces of Turbine Surface Roughness , 2001 .

[17]  S. Hata,et al.  Evaluation of erosion and fatigue resistance of ion plated chromium nitride applied to turbine blades , 2007 .

[18]  B. S. Mann Solid-particle erosion and protective layers for steam turbine blading , 1999 .