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contributor authorD. P. Kenny
date accessioned2017-05-09T00:19:39Z
date available2017-05-09T00:19:39Z
date copyrightJanuary, 1969
date issued1969
identifier issn1528-8919
identifier otherJETPEZ-26673#37_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133578
description abstractA novel, low-cost diffuser based upon discrete pipe drillings has been developed for high-performance centrifugal compressors. These discrete drillings are arranged in symmetrical array to mutually intersect in a radial plane so that a gradual transition from the open vaneless space at rotor tip to the individual throats of each pipe is implicitly defined. To draw a comparison, alternate cambered-vane and flat-plate diffusers were defined using the best available yet practical thinking. With a nominal 5:1 stage pressure ratio, rotor, 81.8 percent efficiency was obtained with the “pipe” diffuser at 5.42 pressure ratio. This efficiency level exceeded the best cambered-vane and flat-plate performance by 6.8 and 8.8 percent, respectively. Further testing with a second rotor yielded 81.3 percent efficiency at 6:1 pressure ratio for the pipe diffuser and 73 percent efficiency at 6:1 for the cambered-vane diffuser.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Novel Low-Cost Diffuser for High-Performance Centrifugal Compressors
typeJournal Paper
journal volume91
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3574671
journal fristpage37
journal lastpage46
identifier eissn0742-4795
keywordsDiffusers
keywordsCompressors
keywordsPipes
keywordsRotors
keywordsPressure
keywordsFlat plates
keywordsSymmetry (Physics) AND Testing
treeJournal of Engineering for Gas Turbines and Power:;1969:;volume( 091 ):;issue: 001
contenttypeFulltext


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