Source: https://journal-me.com/en/archive/vol19-2016-iss4-paper2/
Timestamp: 2019-04-25 15:46:11+00:00

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This paper is devoted to the development of methods for selecting the system characteristics of turbo-compressor units on the basis of the analysis of the test results of the test and pilot models of 6.3 MW turbo-compressor units. On their basis, a new generation of the GPA-Ts-6.3A-type high-performance units was created. Part I of the work presents the state of the problem, as well as objects of research. The requirements for the testing of individual systems with the aim of a thermodynamic analysis of the characteristics of the unit during its operation under the conditions of a closed-loop stand are formulated.
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