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
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 In Out
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)
A 2D example
Complex 2D case Hotter gas in Colder gas out Manifold Vapour in/out
2D: pressure contours
2D: shell-side temperature
2D: Tube-side temperature
2D: Wall (tube) temperature
2D: Shell-side heat-transf coef
2D: Tube-side heat-transf coef
Geometrical modelling
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 Parser program (ASCII) (in-house made) Geometrical data, mesh, etc Simulation parameters (Q1) Simulation (Earth) Numerical results Graphical results: (PHOTON, TECPLOT)
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
Mathematical modelling
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)
Results
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: Test cases
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 1SH Primary Superheater 2SH Secondary superheater Turbine V L Turbine Final reheater Dividing walls 2SH Reheater 1SH Vapour UE 1SH Primary Superheater 2SH Secondary superheater UE Upper economizer LE Lower economizer Gases 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
Shell-side temperature
Flow field (velocity vectors)
Pressure field
Shell temperature
Tube-side temperature
Tube-wall temperature
Heat-transfer rate NB per cell
Tube-side heat-transfer coeff
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