Selection of Systemic Characteristics for Turbo-Compressor Package Based on Efficiency Analysis According to Full Scale Tests Results. Part I

• Видавець: Інститут енергетичних машин і систем ім. А. М. Підгорного Національної академії наук України
• Дата: 2016
• Автори: Парафейник, В. П., Щербаков, Н. С., Рябов, А. А., Шевчук, В. В., Разношинский, В. Н., Тертышный, И. Н., Прилипко, С. А.
• Формат: Стаття
• Мова: Russian
• Опубліковано: Інститут енергетичних машин і систем ім. А. М. Підгорного Національної академії наук України 2016
• Теми: turbo-compressor package; centrifugal compressor; gas turbine engine; compressor polytropic efficiency; turbine effective efficiency; package integral characteristics; package systematic characteristics; exergy approach; турбокомпрессорный агрегат; центробежный компрессор; газотурбинный двигатель; политропный КПД компрессора; эффективный КПД двигателя; интегральная характеристика агрегата; системная характеристика агрегата; эксергетический подход; УДК 621.515; турбокомпресорний агрегат; відцентровий компресор; газотурбінний двигун; політропний ККД компресора; ефективний ККД двигуна
• Онлайн доступ: https://journals.uran.ua/jme/article/view/86774

The methodology of efficiency analysis of gas turbine turbo-compressor package and its systems to select the systematic characteristics and more appropriate mode of its operation at pre-design  studies stage while creating new equipment for gas pipelines compressor stations will be finalized in the present work based on the full-scale results of bench and prototype models of the series-produced turbo-compressor package GPA-C-6,3A manufactured by Sumy NPO PJSC and State Enterprise “Ivchenko Progress”. The first part of the work presents the target of research, i.e. modular package designed for line compressor stations and equipped with centrifugal compressor NC-6,3/56В-1,45 providing outlet pressure of compressed gas 5,49 MPa and gas turbine D-336.  The main design solutions and the special features of the package which predetermine the package design layout as well as general approach for method development of thermodynamic analysis of the package of container type are considered.  Also the work presents the requirements to scope of testing of separate systems including parameters data for operation of centrifugal compressor, gas turbine, auxilliary systems of the package to perform thermodynamic analysis of its operating process when the package runs under conditions of back-to-back test rig