Simulations of Multi-Phase Particle Deposition on Endwall Film-Cooling

Demand for clean energy has increased motivation to d esign gas turbines capable of burning alternative fuels such as coal derived synthesis gas (syngas). One challenge associated with burning coal derived syngas is that trace amounts of particulate matter in the fuel and air can deposit on turbine hardware reducing the effectiveness of film cooling. For the current study, a method was developed to dynamically simulate multi-phase particle deposition through injection of a low melting temperature wax. The method was developed so the effects of deposition on endwall film cooling could be quantified using a large scale vane cascade in a low speed wind tunnel. A microcrystalline wax was injected into the mainstream flow using atomizing spray nozzles to simulate both solid and molten particulate matter in a turbine gas path. Infrared thermography was used to quantify cooling effectiveness with and without deposition at various locations on a film cooled endwall. Measured results indicated reductions in adiabatic effectiveness by as much as 30% whereby the reduction was highly dependent upon the location of the film-cooling holes relative to the vane. NOMENCLATURE a speed of sound A surface area C chord length Cp particle specific heat �hfus specific latent heat of fusion D film cooling hole diameter, D=0.46cm dp particle diameter h heat transfer coefficient

[1]  Jared Crosby Particle Size, Gas Temperature, and Impingement Cooling Effects on High Pressure Turbine Deposition in Land Based Gas Turbines from Various Synfuels , 2005 .

[2]  Scott Lewis,et al.  Film Cooling Effectiveness and Heat Transfer Near Deposit-Laden Film Holes , 2011 .

[3]  S. Krishnaiah,et al.  Determination of thermal properties of some supplementary cementing materials used in cement and concrete , 2006 .

[4]  T. Fletcher,et al.  Deposition Near Film Cooling Holes on a High Pressure Turbine Vane , 2012 .

[5]  K. Thole,et al.  Heat Transfer for a Turbine Blade With Nonaxisymmetric Endwall Contouring vortical secondary flows that are present near the endwall of an axial gas , 2011 .

[6]  Karen A. Thole,et al.  Film-Cooling Flowfields With Trenched Holes on an Endwall , 2009 .

[7]  Jie Yang,et al.  Melting characteristics during the vitrification of MSWI fly ash with a pilot-scale diesel oil furnace. , 2008, Journal of hazardous materials.

[8]  David G. Bogard,et al.  Scaling of Performance for Varying Density Ratio Coolants on an Airfoil With Strong Curvature and Pressure Gradient Effects , 2001 .

[9]  Jeffrey P. Bons,et al.  Effects of Particle Size, Gas Temperature and Metal Temperature on High Pressure Turbine Deposition in Land Based Gas Turbines From Various Synfuels , 2007 .

[10]  D. Bogard,et al.  Experimental Simulation of Contaminant Deposition on a Film Cooled Turbine Airfoil Leading Edge , 2012 .

[11]  Lei Wang,et al.  Investigation of MSWI fly ash melting characteristic by DSC-DTA. , 2007, Waste management.

[12]  Robert J. Moffat,et al.  Describing the Uncertainties in Experimental Results , 1988 .

[13]  Karen A. Thole,et al.  Flowfield Measurements for a Highly Turbulent Flow in a Stator Vane Passage , 2000 .

[14]  Karen A. Thole,et al.  The Effects of Simulated Particle Deposition on Film Cooling , 2009 .

[15]  Karen A. Thole,et al.  Effect of Midpassage Gap, Endwall Misalignment, and Roughness on Endwall Film-Cooling , 2006 .

[16]  T. Fletcher,et al.  Evolution of Surface Deposits on a High-Pressure Turbine Blade-Part II. Convective Heat Transfer , 2006 .

[17]  SIMULATED LAND-BASED TURBINE DEPOSITS GENERATED IN AN ACCELERATED DEPOSITION FACILITY , 2005 .

[18]  K. Thole,et al.  Effects of Surface Deposition, Hole Blockage, and TBC Spallation on Vane Endwall Film-Cooling , 2006 .

[19]  Daniel G. Knost,et al.  Heat transfer and film-cooling for the endwall of a first stage turbine vane , 2005 .

[20]  Karen A. Thole,et al.  Bump and trench modifications to film-cooling holes at the vane-endwall junction , 2008 .

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

[22]  Karen A. Thole,et al.  Heat Transfer for a Turbine Blade With Non-Axisymmetric Endwall Contouring , 2009 .

[23]  Richard A. Dennis,et al.  Development of Baseline Performance Values for Turbines in Existing IGCC Applications , 2007 .