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Modelling the convective zone of a utility boiler Norberto Fueyo Antonio Gómez Fluid Mechanics Group University of Zaragoza. Contents. Motivation 2D example Geometrical modelling Mathematical modelling 2D validation Application to a 350 MW(e) boiler Conclusions Further work. Motivation.
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Modelling the convective zone of a utility boilerNorberto Fueyo Antonio GómezFluid Mechanics GroupUniversity of Zaragoza
Contents • Motivation • 2D example • Geometrical modelling • Mathematical modelling • 2D validation • Application to a 350 MW(e) boiler • Conclusions • Further work
Furnace modelling • Aim: • Modelling • Simulation • Validation • of • Multiphase flow (including turbulence), • Heat transfer (including radiation) • Pollutant (NOx) formation • in • Furnace of power-production utilities
Strategy (‘divide and conquer’) + = (Model coupling through boundary conditions) Convective zone Furnace
Convective-zone modelling • Aim: • Modelling • Simulation • Validation • of • Fluid flow (including turbulence) and • Thermal fields (gas and tube sides) • Heat transfer • in • Convective zone of boiler Out In
Model input • Geometrical data (tubes, banks, etc) • Fluid (shell-side and tube-side) and solid (tube) properties • Operating conditions (inlet mass-flow rates, inlet temperatures, etc)
Model output • Detailed fields of:- • Velocity • Pressure • Turbulence • Shell fluid, tube fluid and wall temperature • Shell-to-wall and tube-to-wall heat-transfer coefficients • Heat-transfer rate (W/m3) • Overall heat-transfer rate, per tube-bank (W)
Complex 2D case Hotter gas in Colder gas out Manifold Vapour in/out
The problem • Geometrically complex problem • Tubes • Tube-banks • Interconnections • Tubes representented as distributed, sub-grid features • Specify geometry in ASCII file • Subordinate mesh to geometry
Strategy (schematic) Convective-zone database (ASCII) Parserprogram (in-house made) Geometrical data, mesh, etc Simulation parameters (Q1) Simulation (Earth) Graphical results: (PHOTON, TECPLOT) Numerical results
Element types • General data • 2D tubebanks (tube wall) • 3D tube banks • Bank arrays (2D, usually) • Manifolds (virtual) • Internal • Inlets • Outlets
Data required for each element • Feature name • Position and dimensions • Tube orientation • Internal and external tube diameter • Tube pitch • Tube material • Fluid velocity • Fluid Cp, Prandtl number, density, viscosity • Tube-bank conectivity • Some others ...
Typical database entry [tubebank] type = 3D long_name = Lower_Economizer_1 short_name = Ecoinf1 [[descrip]] posi = (14.323,1,22.61) dime = (6.34,8.24,2.3) alig = +2 diam = 50.8 pich = (146.26,0,83.3) poro dint = 46 velo dens enul pran mate = SA.210.A1 [[connect]] From_bank = ent1 In_face = South Out_face Link
Main physical models - shell side • Full Navier-Stokes equations, plus enthalpy equation, plus turbulence statistics (typically, k-epsilon model) • Full account of volume porosity due to tube-bank presence • Shell-side pressure-loss via friction factors in momentum equations • Shell-side modification of turbulent flowfield due to presence of tubes • Empirical heat-transfer correlations, based on tube-bank geometry (diameters, pitch, etc) • Simple (but flexible) account of shell-side fouling
Main physical models - tube side • One-directional enthalpy equation (along the tube direction) • Mass-flow rates in the tubes obtained from mass balance • Empirical heat-transfer correlations, based on tube geometry (diameter)
Applications • 2-D, multiple tube-bank configuration(functional validation) • 2-D, single tube-bank configuration(numerical validation) • 3-D convective zone(validation in real-case application)
2D validation • Validation with single-bank configuration: Air V T1 ST SL D NL Tw NT T2
Single-bank: thermal results • Theory: Log Mean Temp Difference method (1-4) and Number of Transfer Units method (5)
Single-bank: pressure loss • Theor 1: Grimison correlation • Theor 2: Gunter and Shaw correlation
350 Mw boiler • NB: still not fully converged, but nevertheless ... • Physically plausible • Results follow
Boiler layout Turbine V L Turbine Final reheater Dividing walls 2SH Reheater 1SH Vapour UE Gases 1SH Primary Superheater 2SH Secondary superheater UE Upper economizer LE Lower economizer LE Flue gas Vapour Gases
Typical geometry • As interpreted by the graphics program from database • Some bounding walls not plotted for the sake of clarity
Computational mesh • 75x64x142 • Approx 680,000 cells
Heat-transfer rate • NB per cell
Comparison with measurements • Results not fully converged • Effect of fouling to be studied • Geometry not 100% accurate
Computational details • Finite-volume formulation of equations • Number of cells: approx 670,000 (75x64x142) • Number of dependent variables: 8 (pressure correction, 3 shell-side velocity components, k, epsilon, tube-side and shell-side enthalpy) • Running time: • Around 12 minutes CPU time per sweep (PENTIUM 300) • Around 1500 iterations to convergence