COMBINED HEAT AND POWER SUPPLY DEMONSTRATION OF MICRO-MIX HYDROGEN COMBUSTION APPLIED TO M1A-17 GAS TURBINE

被引:0
|
作者
Horikawa, Atsushi [1 ]
Ashikaga, Mitsugu [1 ]
Yamaguchi, Masato [1 ]
Ogino, Tomoyuki [1 ]
Aoki, Shigeki [1 ]
Wirsum, Manfred [2 ]
Funke, Harald H. -W. [3 ]
Kusterer, Karsten [4 ]
机构
[1] Kawasaki Heavy Ind Co Ltd, Kobe, Hyogo, Japan
[2] Rhein Westfal TH Aachen, Aachen, Germany
[3] Aachen Univ Appl Sci, Aachen, Germany
[4] B&B AGEMA GmbH, Aachen, Germany
关键词
Industrial Gas Turbine; Combustor development; Fuels; Hydrogen; Emission;
D O I
暂无
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
Kawasaki Heavy Industries, Ltd. (KHI), Aachen University of Applied Sciences, and B&B-AGEMA GmbH have investigated the potential of low NOx micro-mix (MMX) hydrogen combustion and its application to an industrial gas turbine combustor. Engine demonstration tests of a MMX combustor for the M1A-17 gas turbine with a co-generation system were conducted in the hydrogen-fueled power generation plant in Kobe City, Japan. This paper presents the results of the commissioning test and the combined heat and power (CHP) supply demonstration. In the commissioning test, grid interconnection, loading tests and load cut-off tests were successfully conducted. All measurement results satisfied the Japanese environmental regulation values. Dust and soot as well as SOx were not detected. The NOx emissions were below 84 ppmv at 15 % O-2. The noise level at the site boundary was below 60 dB. The vibration at the site boundary was below 45 dB. During the combined heat and power supply demonstration, heat and power were supplied to neighboring public facilities with the MMX combustion technology and 100 % hydrogen fuel. The electric power output reached 1800 kW at which the NOx emissions were 72 ppmv at 15 % O-2, and 60 %RH. Combustion instabilities were not observed. The gas turbine efficiency was improved by about 1 % compared to a non-premixed type combustor with water injection as NOx reduction method. During a total equivalent operation time of 1040 hours, all combustor parts, the M1A-17 gas turbine as such, and the co-generation system were without any issues.
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页数:7
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