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contributor authorYuan Mao Huang
contributor authorYung-Shane Liaw
contributor authorResearch Assistant
date accessioned2017-05-09T00:05:29Z
date available2017-05-09T00:05:29Z
date copyrightDecember, 2001
date issued2001
identifier issn1050-0472
identifier otherJMDEDB-27707#583_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/125592
description abstractThe purpose of this study was to analyze the impact of blades with slots in a rotary compressor. The equations for contact forces were derived from Newton’s law. Updated moving Lagrangian descriptions with the hybrid technique and the Newark time integration method were used to determine the nodal displacement vectors. The finite element method was used to analyze the contact forces and the stresses of blades. The maximum blade contact force of 2.3 KN was larger than the maximum static force of 1 KN. The maximum blade impact Von Mises stress of 12.3 Mpa that occurred at the contact point was greater than the previous calculated static stress of 5.15 Mpa. Hence, the impact effect was significant. Experimental modal analysis was also used to determine the first and second natural frequencies of blades.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Impact of Sliding Blades in a Rotary Compressor
typeJournal Paper
journal volume123
journal issue4
journal titleJournal of Mechanical Design
identifier doi10.1115/1.1416150
journal fristpage583
journal lastpage589
identifier eissn1528-9001
treeJournal of Mechanical Design:;2001:;volume( 123 ):;issue: 004
contenttypeFulltext


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