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contributor authorE. O. Bransford
contributor authorR. A. Stein
date accessioned2017-05-08T23:21:22Z
date available2017-05-08T23:21:22Z
date copyrightJuly, 1960
date issued1960
identifier issn1528-8919
identifier otherJETPEZ-26609#221_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/100501
description abstractIn its simplest terms, the design of a rotary-vane compressor of a given displacement consists of selecting a particular combination of rotor and cylinder radius, cylinder length, and number of vanes. A study of the rotary-vane compressor has shown that the choice is not entirely arbitrary since thermodynamic and mechanical losses occurring in the compressor are intimately associated with these basic dimensions. One of the more important of these geometrically dependent losses was found to be potentially severe overcompression during the discharge process. In this paper, an equation is developed that describes in generalized form the relation of overcompression to the dimensions of the compressor. This equation is used to evolve an energy-loss criterion for design control of this loss. An example of the application of the criterion to a refrigeration compressor is included.
publisherThe American Society of Mechanical Engineers (ASME)
titleDesign Control of Overcompression in Rotary-Vane Compressors
typeJournal Paper
journal volume82
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3672771
journal fristpage221
journal lastpage226
identifier eissn0742-4795
keywordsCompressors
keywordsDesign
keywordsCylinders
keywordsDimensions
keywordsEquations
keywordsDisplacement
keywordsRefrigeration
keywordsRotors AND Energy dissipation
treeJournal of Engineering for Gas Turbines and Power:;1960:;volume( 082 ):;issue: 003
contenttypeFulltext


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