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contributor authorY. Ozawa
contributor authorM. Saiga
contributor authorS. Watanabe
contributor authorJ. Hirano
contributor authorM. Sato
date accessioned2017-05-08T23:44:06Z
date available2017-05-08T23:44:06Z
date copyrightJuly, 1994
date issued1994
identifier issn1528-8919
identifier otherJETPEZ-26729#511_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113536
description abstractCatalytic combustion is an ultralow NOx combustion method, so it is expected that this method will be applied to a gas turbine combustor. However, it is difficult to develop a catalytic combustor because catalytic reliability at high temperature is still insufficient. To overcome this difficulty, we designed a catalytic combustor in which premixed combustion was combined. By this device, it is possible to obtain combustion gas at a combustion temperature of 1300°C while keeping the catalytic temperature below 1000°C. After performing preliminary tests using LPG, we designed two types of combustor for natural gas with a capacity equivalent to one combustor used in a 20 MW class multican-type gas turbine. Combustion tests were conducted at atmospheric pressure using natural gas. As a result, it was confirmed that a combustor in which catalytic combustor segments were arranged alternately with premixing nozzles could achieve low NOx and high combustion efficiency in the range from 1000°C to 1300°C of the combustor exit gas temperature.
publisherThe American Society of Mechanical Engineers (ASME)
titleTest Results of Low NOx Catalytic Combustors for Gas Turbines
typeJournal Paper
journal volume116
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2906849
journal fristpage511
journal lastpage516
identifier eissn0742-4795
keywordsCombustion chambers
keywordsGas turbines
keywordsNitrogen oxides
keywordsCombustion
keywordsTemperature
keywordsNatural gas
keywordsNozzles
keywordsAtmospheric pressure
keywordsReliability
keywordsCombustion gases AND High temperature
treeJournal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 003
contenttypeFulltext


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