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contributor authorD. M. Tsay
contributor authorH. C. Chen
contributor authorM. J. Her
contributor authorResearch Engineer
date accessioned2017-05-09T00:07:32Z
date available2017-05-09T00:07:32Z
date copyrightJanuary, 2002
date issued2002
identifier issn1528-8919
identifier otherJETPEZ-26810#177_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126820
description abstractReferring to machining technologies used for turbomachinery components, generally there are two cutting strategies: point cutting and flank cutting. Based on considerations of the cost, efficiency, and surface roughness, flank cutting by using a five-axis machining tool is a promising way to machine blade surfaces of turbomachinery components constructed by ruled surfaces. In this article, a flank cutting technology for centrifugal compressor impellers is developed by using the B-spline curve interpolation, ruled surface construction, and coordinate transformations. Also, an impeller with 12 blades is actually machined to verify the proposed approach by using a five-axis machining center.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Study on Five Flank Machining of Centrifugal Compressor Impellers
typeJournal Paper
journal volume124
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1413768
journal fristpage177
journal lastpage181
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 001
contenttypeFulltext


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