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contributor authorH. Sixsmith
contributor authorH. Altmann
date accessioned2017-05-08T23:03:21Z
date available2017-05-08T23:03:21Z
date copyrightAugust, 1977
date issued1977
identifier issn1087-1357
identifier otherJMSEFK-27662#637_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/90180
description abstractA regenerative or peripheral compressor has been developed with aerodynamic blading in place of the usual straight radial vanes on the rotor. The blades are shrouded by a core, around which a helical toroidal flow path is established. Two compressors have been constructed, the first with a single row of blades and the second with two rows side by side to provide parallel counterrotating flow paths. The diameter of the impellers is 0.30 m. The characteristics of the compressor resemble those of a Rootes blower, with a steep variation of pressure with respect to flow rate. At a speed of 4000 rpm the isothermal efficiency reaches a maximum of 57 percent when the pressure ratio is 1.17 and the flow rate is 0.2 m3 /s. When the flow rate is reduced by throttling to 0.165 m3 /s the pressure ratio is raised to 1.50, but the isothermal efficiency is reduced to 44 percent. The theory, design, and development of the compressor are discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Regenerative Compressor
typeJournal Paper
journal volume99
journal issue3
journal titleJournal of Manufacturing Science and Engineering
identifier doi10.1115/1.3439291
journal fristpage637
journal lastpage647
identifier eissn1528-8935
keywordsCompressors
keywordsFlow (Dynamics)
keywordsPressure
keywordsBlades
keywordsImpellers
keywordsDesign AND Rotors
treeJournal of Manufacturing Science and Engineering:;1977:;volume( 099 ):;issue: 003
contenttypeFulltext


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