Development of a gas turbine fuel nozzle for DME and a design method thereof

Lee, M; Yoon, Y

HERO ID

1553577

Reference Type

Journal Article

Year

2012

HERO ID 1553577
In Press No
Year 2012
Title Development of a gas turbine fuel nozzle for DME and a design method thereof
Authors Lee, M; Yoon, Y
Journal Fuel
Volume 102
Page Numbers 823-830
Abstract DME (dimethyl ether, CH3OCH3) is a potentially attractive fuel for gas turbines because of low pollutant emission and easy transportation and storage. However, the high flame speed and a low ignition temperature of DME present a high risk of flash-back, which can be a potentially serious problem. To solve this problem and achieve better combustion performance, the present study contrived a new fuel nozzle for DME that can obtain optimal combustion of DME in the gas turbine combustor, thereby achieving cost reduction of power generation, enhancement in reliability of power plants and diversification of usable fuel. The configuration of a fuel nozzle for DME and a design method using Wobbe Index are both described in detail. The combustion performance of the newly developed DME fuel nozzle was verified through a gas turbine combustion test and the results showed considerable improvement in the performance of NOx and CO emissions and the prevention of flash-back. (C) 2012 Elsevier Ltd. All rights reserved.
Doi 10.1016/j.fuel.2012.05.017
Wosid WOS:000308804500096
Url http://www.sciencedirect.com/science/article/pii/S0016236112003602
Is Certified Translation No
Dupe Override No
Comments Source: Web of Science WOS:000308804500096
Is Public Yes
Keyword Dimethyl ether (DME); Gas turbine combustion; Combustor design; Wobbe Index