A statistical model to predict ignition probability

被引:31
作者
Esclapez, Lucas [1 ,2 ,3 ]
Collin-Bastiani, Felix [1 ,2 ]
Riber, Eleonore [1 ]
Cuenot, Benedicte [1 ]
机构
[1] CERFACS, 42 Ave G Coriolis, F-31057 Toulouse 01, France
[2] Safran Aircraft Engines, F-77550 Moissy Cramayel, France
[3] LBNL, Ctr Computat Sci & Engn CCSE, 1 Cyclotron Rd, Berkeley, CA 94720 USA
关键词
Ignition probability; Gas turbine; Turbulent combustion;
D O I
10.1016/j.combustflame.2020.10.051
中图分类号
O414.1 [热力学];
学科分类号
摘要
Ignition capability is a critical design constraint for aeronautical gas turbines. However the current trend toward overall lean burn is detrimental to the engine ignition and relight and the ignition system must be adapted to ensure a fast and reliable light-round in all circumstances. As ignition is a stochastic phenomenon, the optimization of an ignition system requires to build ignition probability maps, which is difficult and costly with either experiment or numerical simulation as both require many tests. This work proposes a model to predict the ignition probability map, knowing only flow statistics in non-reacting conditions, i.e., with only one test. The originality of the model is to construct statistics of the flame kernel trajectory, which are then combined with local flow indicators to evaluate the ignition probability at the considered sparking location. Application to a swirled burner operated in premixed, non-premixed and spray combustion modes illustrates the model concepts and demonstrates its ability to recover the experimental ignition map with good accuracy. (C) 2020 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:180 / 195
页数:16
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