CFD analysis of the flow in the reheater shroud of the boiler spine - PowerPoint PPT Presentation

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CFD analysis of the flow in the reheater shroud of the boiler spine

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There are a number of critical welds vulnerable to reheat cracking, see 12.3, 12.8 and12.4 ... Showed the small variation in temperature around the weld. Conclusions ... – PowerPoint PPT presentation

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Title: CFD analysis of the flow in the reheater shroud of the boiler spine


1
CFD analysis of the flow in the reheater shroud
of the boiler spine
  • E Romero
  • British Energy

2
Introduction
  • A description of the problem
  • A discussion of the functionality of FEAT used in
    the analysis of the problem

3
Boiler support spine at HRA/HYA
  • There are a number of critical welds vulnerable
    to reheat cracking, see 12.3, 12.8 and12.4

4
Flow in the reheater shroud
  • The gas flow in the reheater shroud is critical
    in maintaining the temperature of weld 12.3 at
    reasonable levels.
  • 6kg/s of pressurised CO2 flowing through a 18mm
    annular gap
  • Outer walls heated by the main boiler gas flow
  • Inner wall cooled by the feed pipes in the centre
    of the spine.

5
CFD Models
  • A 2D axisymmetric model of the passage including
    the spine body and the shroud
  • A 3D model of one azimuthal segment containing a
    bleed hole also comprising the walls.

6
2D Model - Reheater shroud
  • Axisymmetric representation of the reheater
    shroud passage and solid walls
  • Bleed holes represented by smaller convergent
    passages with the same area.

7
3D Model - Bleed Holes
  • One octant of the reheater shroud passage
  • PATRAN generated mesh

8
Boundary conditions (2D Model)
  • Internal wall exposed to a natural convection
    flow. Modelled through a temperature dependent
    Nusselt number calculated with the help of CO2
    material database.
  • External wall exposed to a gas flow with an axial
    thermal gradient and radiation to reheater tubes.

9
Results (2D Model)
  • After judicious use of upwinding in the dead
    space and length scale limiting (LSCUTFAC)
    reasonable results obtained with ?-?.
  • Bleed holes modelled as convergent passages

10
Results (2D Model) 2
  • The key result was to justify a small gas
    temperature rise
  • In addition it supported reasonable heat transfer
    in the dead space

11
Results (3D Model)
  • Not an ideal solution in CFD terms
  • However it showed significant stirring of gas in
    the dead space
  • Showed the small variation in temperature around
    the weld

12
Conclusions
  • CFD analysis of the flow in the reheater shroud
    has shown that rise in gas temperature is small
    and has helped to support weld temperature
    predictions.
  • Much of FEATs functionality has been brought to
    bear Turbulence modelling, axi-symmetric ray
    tracing, variable properties, multifrontal
    solution, FE mesh handling, TURCYC.
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