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contributor authorF. S. Schaub
contributor authorR. L. Hubbard
date accessioned2017-05-08T23:20:04Z
date available2017-05-08T23:20:04Z
date copyrightOctober, 1985
date issued1985
identifier issn1528-8919
identifier otherJETPEZ-26626#922_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/99748
description abstractThis paper describes the procedure developed by Cooper-Bessemer for large-bore gas engines to calculate the knock rating of gas fuel blends and to predict with accuracy the required engine build to use that fuel with optimum detonation margin. Engine prototype test work has included fuel sensitivity tests mapped as a function of compression ratio, fuel air ratio, ignition advance, combustion air temperature, and engine rating. Success in predicting production engine operation for a given application involving a particular fuel blend has been gratifying. The basic reference method blend selected was normal butane in methane. Details are included in the paper to illustrate the problems in making sensitivity correlations between small-bore fuel research engines and large-bore production engines.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Procedure for Calculating Fuel Gas Blend Knock Rating for Large-Bore Gas Engines and Predicting Engine Operation
typeJournal Paper
journal volume107
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3239837
journal fristpage922
journal lastpage930
identifier eissn0742-4795
keywordsGaseous fuels
keywordsEngines
keywordsGas engines
keywordsFuels
keywordsTemperature
keywordsCombustion
keywordsExplosions
keywordsEngineering prototypes
keywordsCompression
keywordsIgnition AND Methane
treeJournal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 004
contenttypeFulltext


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