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contributor authorGong Chen
date accessioned2017-05-09T00:23:46Z
date available2017-05-09T00:23:46Z
date copyrightApril, 2007
date issued2007
identifier issn1528-8919
identifier otherJETPEZ-26949#589_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135761
description abstractPeak cylinder pressure (pmax) of a compression-ignition engine can be affected by the engine inlet air condition, such as its inlet air temperature (Ti) and pressure (pi). The variation of peak cylinder pressure due to varying inlet air temperature or pressure is analytically studied. A model is developed and simplified, and thus the variations of pmax can be predicted along with varying inlet air temperature or pressure. The analysis and prediction indicate that cylinder active compression ratio (CR) and intake air boost ratio (pm0∕pi0) play relatively significant roles in affecting the variation of pmax over inlet air temperature and pressure, and the pressure variation is proportional to CRk and ratio pm0∕pi0. Comparison between the predicted results using the simplified model and those from engine experiments shows a close agreement in both the trend and magnitude. The investigation and prediction also include modeling the variation in pmax due to varying the cylinder TDC clearance volume (Vc). The simplified model is presented and shows that the change in pmax versus varying Vc also depends on the cylinder compression ratio. It is indicated that for a certain change in the clearance volume, a higher compression-ratio configuration would produce a greater change in pmax than a lower one does, especially as the rest of the engine design and operating parameters remain unchanged.
publisherThe American Society of Mechanical Engineers (ASME)
titlePrediction of Peak Cylinder Pressure Variations Over Varying Inlet Air Condition of Compression-Ignition Engine
typeJournal Paper
journal volume129
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2431389
journal fristpage589
journal lastpage595
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002
contenttypeFulltext


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