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contributor authorK. Dasgupta
contributor authorA. Mukherjee
contributor authorR. Maiti
date accessioned2017-05-09T00:00:19Z
date available2017-05-09T00:00:19Z
date copyrightMay, 1999
date issued1999
identifier issn1087-1357
identifier otherJMSEFK-27342#300_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122517
description abstractIn this paper the authors have presented an integrated study of an orbital rotor Low Speed High Torque (LSHT) hydrostatic unit in a Hydrostatic Transmission (HST) System and an attempt has been made to estimate some critical parameters of such class of geometrically complex machine. Owing to the close tolerance in between the rotor-stator interface of the motor leakage takes place from the high pressure to the low pressure chamber and is difficult to estimate during operation. Based on the simulation and experimental investigations, a semi-empirical approach is proposed here to estimate its interchamber leakage resistance and for that the machine need not be disassembled. Using the actual parametric values, the overall dynamic model of the plant has been validated experimentally.
publisherThe American Society of Mechanical Engineers (ASME)
titleEstimation of Critical System Parameters That Affect Orbit Motor Performance—Combining Simulation and Experiments
typeJournal Paper
journal volume121
journal issue2
journal titleJournal of Manufacturing Science and Engineering
identifier doi10.1115/1.2831220
journal fristpage300
journal lastpage306
identifier eissn1528-8935
keywordsEngines
keywordsSimulation
keywordsHydrostatics
keywordsMachinery
keywordsRotors
keywordsLeakage
keywordsIndustrial plants
keywordsStators
keywordsDynamic models
keywordsTorque
keywordsPressure
keywordsHigh pressure (Physics) AND Electrical resistance
treeJournal of Manufacturing Science and Engineering:;1999:;volume( 121 ):;issue: 002
contenttypeFulltext


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