Metal Temperature Prediction of a Dry Low NOx Class Flame Tube by Computational Fluid Dynamics Conjugate Heat Transfer Approach

Author:

Da Soghe Riccardo1,Bianchini Cosimo1,Andreini Antonio2,Mazzei Lorenzo2,Riccio Giovanni3,Marini Alessandro3

Affiliation:

1. Ergon Research srl, via Panciatichi 92, Florence 50127, Italy e-mail:

2. Department of Industrial Engineering Florence (DIEF), University of Florence, via di Santa Marta 3, Firenze (FI) 50139, Italy e-mail:

3. GE Oil and Gas, via Matteucci 2, Florence 50100, Italy e-mail:

Abstract

Combustor liner of present gas turbine engines is subjected to high thermal loads as it surrounds high temperature combustion reactants and is hence facing the related radiative load. This generally produces high thermal stress levels on the liner, strongly limiting its life expectations and making it one of the most critical components of the entire engine. The reliable prediction of such thermal loads is hence a crucial aspect to increase the flame tube life span and to ensure safe operations. The present study aims at investigating the aerothermal behavior of a GE Dry Low NOx (DLN1) class flame tube and in particular at evaluating working metal temperatures of the liner in relation to the flow and heat transfer state inside and outside the combustion chamber. Three different operating conditions have been accounted for (i.e., lean–lean partial load, premixed full load, and primary load) to determine the amount of heat transfer from the gas to the liner by means of computational fluid dynamics (CFD). The numerical predictions have been compared to experimental measurements of metal temperature showing a good agreement between CFD and experiments.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

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