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contributor authorD. Taraza
date accessioned2017-05-09T00:10:09Z
date available2017-05-09T00:10:09Z
date copyrightJuly, 2003
date issued2003
identifier issn1528-8919
identifier otherJETPEZ-26823#791_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/128362
description abstractThe goal of this two-part paper is to develop a methodology using the variation of the measured crankshaft speed to calculate the mean indicated pressure (MIP) of a multicylinder engine and to detect cylinders that are lower contributors to the total engine output. Both the gas pressure torque and the crankshaft’s speed are, under steady-state operating conditions, periodic functions of the crank angle and may be expressed by Fourier series. For the lower harmonic orders, the dynamic response of the crankshaft approaches the response of a rigid body and that makes it is possible to establish correlations between the amplitudes and phases of the corresponding harmonic orders of the crankshaft’s speed and of the gas pressure torque. The inherent cycle-to-cycle variation in the operation of the cylinders requires a statistical approach to the problem. The first part of the paper introduces the statistical model for a harmonic component of the gas pressure torque and determines the correlation between the amplitudes and phases of the harmonic components of the gas pressure torque and the MIP of the engine. In the second part of the paper the statistical model is used to calculate the MIP and to detect deficient cylinders in the operation of a six-cylinder four-stroke diesel engine.
publisherThe American Society of Mechanical Engineers (ASME)
titleStatistical Correlation Between the Crankshaft’s Speed Variation and Engine Performance—Part I: Theoretical Model
typeJournal Paper
journal volume125
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1563244
journal fristpage791
journal lastpage796
identifier eissn0742-4795
keywordsTorque
keywordsPressure
keywordsEngines AND Cylinders
treeJournal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 003
contenttypeFulltext


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