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Low emissions trapped vortex combustor

Yangbo Deng (Marine Engineering College, Dalian Maritime University, Dalian, China.)
Fengmin Su (Marine Engineering College, Dalian Maritime University, Dalian, China.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 4 January 2016

311

Abstract

Purpose

The purpose of this paper is to study the combustion and emission characteristics of an improved trapped vortex combustor (TVC).

Design/methodology/approach

An experiment is carried out to study the effect of the bluff bodies’ layout on the flow of the improved TVC. Results confirm that an equation achieving the proper cavity size of a TVC can be used to design the reasonable configuration of the improved TVC. A numerical simulation is used to study the flow, combustion and emission characteristics of the improved TVC.

Findings

The flow resistance, the vortex configuration, the combustion efficiency and the emissions of the improved TVC are influenced by the equivalence ratio of the main flow, the position and the flow injection angle in the cavity.

Research limitations/implications

The investigation on the lean-premixed combustion of the improved TVC will provide a theory basis for the design of the improved TVC.

Practical implications

The improved TVC will be used in the gas turbines burning synfuels. There are the implications which offer an opportunity to avoid use of diluent gas to reduce the flame temperatures of the combustion in the gas turbines burning synfuels.

Originality/value

The improved TVC with the reasonable layout of the bluff bodies provides a method implementing lean-premixed combustion in the gas turbines burning synfuels.

Keywords

Acknowledgements

The authors wish to acknowledge that this work was supported by the National Science Funds Commission – Shenhua Group “Coal Joint Fund” (Grant No. U1361111) and the National Natural Science Foundation of China (Grant No. 51076020).

Citation

Deng, Y. and Su, F. (2016), "Low emissions trapped vortex combustor", Aircraft Engineering and Aerospace Technology, Vol. 88 No. 1, pp. 33-41. https://doi.org/10.1108/AEAT-09-2013-0172

Publisher

:

Emerald Group Publishing Limited

Copyright © 2016, Emerald Group Publishing Limited

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