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contributor authorK. K. Srinivasan
contributor authorS. R. Bell
contributor authorW. Gong
contributor authorS. B. Fiveland
contributor authorS. R. Krishnan
contributor authorS. Singh
contributor authorM. Willi
contributor authorK. C. Midkiff
date accessioned2017-05-09T00:19:58Z
date available2017-05-09T00:19:58Z
date copyrightJanuary, 2006
date issued2006
identifier issn1528-8919
identifier otherJETPEZ-26894#213_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133738
description abstractThe Advanced (injection) Low Pilot Ignited Natural Gas (ALPING) engine is proposed as an alternative to diesel and conventional dual fuel engines. Experimental results from full load operation at a constant speed of 1700rev∕min are presented in this paper. The potential of the ALPING engine is realized in reduced NOx emissions (to less than 0.2g∕kWh) accompanied by fuel conversion efficiencies comparable to straight diesel operation. Some problems at advanced injection timings are recognized in high unburned hydrocarbon (HC) emissions (25g∕kWh) and poor engine stability reflected by high COVIMEP (about 6%). This paper focuses on the combustion aspects of low pilot ignited natural gas engines with particular emphasis on advanced injection timings (45°–60° BTDC). Ignition phasing at advanced injection timings (∼60° BTDC), and combustion phasing at retarded injection timings (∼15° BTDC) are recognized as important combustion parameters that profoundly impact the combustion process, HC emissions, and the stability of engine operation.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Advanced Injection Low Pilot Ignited Natural Gas Engine: A Combustion Analysis
typeJournal Paper
journal volume128
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1915428
journal fristpage213
journal lastpage218
identifier eissn0742-4795
keywordsCombustion
keywordsEngines
keywordsIgnition
keywordsGas engines
keywordsFuels
keywordsDiesel
keywordsNatural gas
keywordsEmissions AND Pressure
treeJournal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 001
contenttypeFulltext


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