Selection of System Characteristic of Turbo-Compressor Package Based on Efficiency Analysis according to Full-Scale Test Results. Part ІV. Analysis of System Characteristics of Turbo-Compressor Package GPA-C-6,3А /56-1,45 and Possibility of Optimization
Keywords:
package, compressor, exergy analysis, system characteristics, package exergy efficiencyAbstract
This paper presents the obtained system characteristics of the package GPA-C-6,3А /56-1,45 using functional and functional-exergy approaches as well as design and experimental data on efficiency of centrifugal compressor (CC) and gas turbine (GT). When functional approach served the package efficiency was 25,8%, and when functional-exergy approach served it was 26,5%. At this in both cases there is a difference between the optimum condition of the package operation at which the max efficiency of the package is reached, and design condition of centrifugal compressor operation. The specified differences are determined by using impellers with blades exit angle 320 and vaned diffusers in centrifugal compressor stages. The analytical dependence to determine TCA fuel efficiency factor is presented. Coincidence of optimum of characteristics of the package exergy efficiency and fuel consumption factor of centrifugal compressor weight output is determined. In this case the package max exergy efficiency meets min value of the fuel consumption value. Using experimental data the design model verification for thermodynamic analysis of the operating process of the skid turbo-compressor package of linear compressor stations having single casing centrifugal compressor is performed. It is shown that mismatching of max values of the package efficiency by weight output for TCA system characteristics is 2,0% (relative one), that provides the required accuracy of the parameters when TCA designing.References
Parafeynik V.P., Shcherbakov N.S., Ryabov A.A., Shevchuk V.V., Raznoshynskyy V.N., Tertyshnyiy I.N., Prilipko S.A. “Selection system characteristics of turbo-compressor package based on efficiency on full-scale test results. Part I. State of the art and subject of research” Engineering Industry Problems. 2016 (V.19, 4):12-18.
Parafeynik V.P., Shcherbakov N.S., Ryabov A.A., Shevchuk V.V., Raznoshynskyy V.N., Tertyshnyiy I.N., Prilipko S.A. “Selection system characteristics of turbo-compressor package based on efficiency on full-scale test results. Part II. Methodological Approach to Design Modular Turbo-Compressor Packages for CS of Gas Industry” Engineering Industry Problems. 2017 (V.20,1): 3–11.
Shcherbakov N.S., Parafeynik V.P., Ryabov A.A., Shevchuk V.V., Raznoshynskyy V.N., Tertyshnyiy I.N., Prilipko S.A. “Selection of System Characteristic of Turbo-Compressor Package Based on Efficiency Analysis according to Full-Scale Test Results. Part ІІІ. Efficiency Research of Basic Systems of Turbo-Compressor Package GPA-C-6,3A/56-1,45 on Full-Scale Test Results” Engineering Industry Problems. 2017 (V.20,2): 11–18.
Tertyshnyiy I.N., Prilipko S.A., Miroshnichenko E.A., Parafeynik V.P. “Thermodynamic Analysis of Operating Process Efficiency of Booster Turbo-Compressor Packages with Gas Turbine Drive. Part I.” Engineering Industry Problems. 2015 (V.18, 4/1): 9-17.
Tertyshnyiy I.N., Prilipko S.A., Parafeynik V.P. “Thermodynamic Analysis of Operating Process Efficiency of Booster Turbo-Compressor Packages with Gas Turbine Drive. Part I.” Engineering Industry Problems. 2016 (V.19, 2): 10–18.
S.G. Sokolov “Air craft turbo-compressor packages and methods of efficiency increasing” Abstract of Ph.D Thesis in Engineering Science: 05.04.06.– М., 1984. 18 p.
Parafeynik V.P. “Scientific Basis of Development of Turbo-Compressor Units with Gas Turbine” Abstract of Doctor Thesis in Engineering Science Spec. 05.05.16 . – Kharkov, 2009. 41 p.
Parafeynik V.P., Nefyedov A.N., Yevdokimov V.E., Tertyshnyiy I.N. “Regards geometry optimization of natural gas centrifugal compressors rotor bundle” Compressor equipment and pneumatic. 2012 (No.2): 10–17.
Bondarenko G.A., Yurko I.V. “Optimization method of gas dynamic characteristics of axial-radial compressor stage with inlet guide channel” Visnyk NTU «KhPI». 2013 (No.14, 988): 49–53.
Downloads
Published
Issue
Section
License
Copyright (c) 2018 В. П. Парафейник, И. Н. Тертышный, С. А. Прилипко, А. А. Рябов
This work is licensed under a Creative Commons Attribution-NoDerivatives 4.0 International License.
All authors agree with the following conditions:
- The authors reserve the right to claim authorship of their work and transfer to the journal the right of first publication of the work under the license agreement (the agreement).
- Authors have a right to conclude independently additional agreement on non-exclusive spreading the work in the form in which it was published by the jpurnal (for example, to place the work in institution repository or to publish as a part of a monograph), providing a link to the first publication of the work in this journal.
- Journal policy allows authors to place the manuscript in the Internet (for example, in the institution repository or on a personal web sites) both before its submission to the editorial board and during its editorial processing, as this ensures the productive scientific discussion and impact positively on the efficiency and dynamics of citation of published work (see The Effect of Open Access).