CENTRIFUGAL COMPRESSOR DESIGN AND PERFORMANCE

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Compressor Performance

Author : Theodore Gresh
ISBN : 9780128142202
Genre : Technology & Engineering
File Size : 43.29 MB
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Compressor Performance: Aerodynamics for the User, Third Edition continues the book's 25 year history as a trusted reference on compressor design and maintenance. This new edition is updated throughout to cover new regulations and technology relevant to compressors, with new content adding coverage of strings of equipment, including gas turbines. Users will find sections that run the full spectrum of information needed for an individual to select, operate, test and maintain axial or centrifugal compressors. In addition, basic aerodynamic theory provides users with the how's and why's of compressor design, and troubleshooting guidelines help maintenance engineers save time in the field. Provides detailed instructions for best practice field performance tests to ASME standards Includes illustrations with detailed diagrams of compressor equipment Presents new case studies of equipment string analysis Includes extensive reference material in an appendix, including Mollier diagrams, permissible deviations and fluctuations, and surge identification procedures
Category: Technology & Engineering

Centrifugal Compressors

Author : Meherwan P. Boyce
ISBN : 9780878148011
Genre : Technology & Engineering
File Size : 23.3 MB
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Annotation The proper selection of a compressor is a complex and important decision. The successful operation of many plants depends on smooth and efficient compressor operations. To ensure the best selection and proper maintenance of a centrifugal compressor, the engineer must have a knowledge of many engineering disciplines. Boyce provides an up-to-date reference in the field of centrifugal compressors covering all major aspects of design, operation, and maintenance. As well, he includes technical details on sizing, plant layout, fuel selection, types of drives, and performance characteristics of all major components in a co-generation or combined-cycle power plant.
Category: Technology & Engineering

Centrifugal Compressors

Author : Ronald H. Aungier
ISBN : 0791800938
Genre : Technology & Engineering
File Size : 66.18 MB
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A mechanical engineer with a Pennsylvania turbomachinery company, A ungier describes his own system and strategy for designing and analyzing centrifugal compressor aerodynamics. To address the novice as well as the experienced in the field, he presents the basic thermodynamic and fluid dynamic principles, empirical models, and key numerical methods that form the basis of his methods. His strategy, or design practice, he found harder to describe because it involves a process of reasoning rather than following an established set of principles. He recognizes that his is only one of many possible methods, but makes no effort to compare or contrast his with any other.
Category: Technology & Engineering

Process Centrifugal Compressors

Author : Klaus H. Lüdtke
ISBN : 9783662094495
Genre : Science
File Size : 22.25 MB
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Originating in the process compressor industry, this text primarily addresses: rotating equipment engineers, project engineers, engineering contractors, and compressor user companies in oil and gas field operations, natural gas processing, petroleum refining, petrochemical processing, industrial refrigeration, and chemical industries. It enables the reader to assess compressors and defines the constraints influencing the compressor design.
Category: Science

Analytical Correlation Of Centrifugal Compressor Design Geometry For Maximum Efficiency With Specific Speed

Author : Michael R. Galvas
ISBN : UIUC:30112106884189
Genre : Mathematics
File Size : 41.95 MB
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Centrifugal compressor performance was examined analytically to determine optimum geometry for various applications as characterized by specific speed. Seven specific losses were calculated for various combinations of inlet tip-exit diameter ratio, inlet hub-tip diameter ratio, blade exit backsweep, and inlet-tip absolute tangential velocity for solid body prewhirl. The losses considered were inlet guide vane loss, blade loading loss, skin friction loss, recirculation loss, disk friction loss, vaneless diffuser loss, and vaned diffuser loss. Maximum total efficiencies ranged from 0.497 to 0.868 for a specific speed range of 0.257 to 1.346. Curves of rotor exit absolute flow angle, inlet tip-exit diameter ratio, inlet hub-tip diameter ratio, head coefficient and blade exit backsweep are presented over a range of specific speeds for various inducer tip speeds to permit rapid selection of optimum compressor size and shape for a variety of applications.
Category: Mathematics