2015
DOI: 10.1088/1757-899x/90/1/012047
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Numerical Investigation of Different Radial Inlet Forms for Centrifugal Compressor and Influence of the Deflectors Number by Means of Computational Fluid Dynamics Methods with Computational Model Validation

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Cited by 19 publications
(6 citation statements)
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“…VIGV is designed to create swirling air supplied to the rotor blades of the first stage of the compressor in order to reduce the relative velocities and obtain optimal angles of flow on the rotor blade profile. There are examples of successful application of CFD methods to the input and output devices of a centrifugal compressor [17,18].…”
Section: Resultsmentioning
confidence: 99%
“…VIGV is designed to create swirling air supplied to the rotor blades of the first stage of the compressor in order to reduce the relative velocities and obtain optimal angles of flow on the rotor blade profile. There are examples of successful application of CFD methods to the input and output devices of a centrifugal compressor [17,18].…”
Section: Resultsmentioning
confidence: 99%
“…Further development of the centrifugal compressors [1][2][3][4][5][6][7][8][9][10][11][12] design is associated with increases in rotor rotational velocities, and as a result of loads on structural elements and plant capacities, while maintaining a sufficient level of operational safety both from the strength of the nodes and the stability of the performance. One of the causes of accidents on the compressor is getting into the surge due to an inoperative surge protection system, or not being able to take into account all the factors affecting the compressor in the surge state.…”
Section: Introductionmentioning
confidence: 99%
“…When calculating the ncr rotor of a single-shaft five-stage CC that compresses hydrogencontaining gas (rotor length L = 1.605 m, mass Mr = 237.8 kg, shaft diameter in support bearings dsb = 0.07 m, maximum shaft diameter ds.max= 0.174 m, mass of the impellers Mimp = 13.3 ... 11.6 kg), with an increase in the coefficient of rigidity of the oil layer in the reference OS from 10 8 to 10 10 N / m, the speed of the first harmonic of ncr increased almost 1.3 times, the second harmonic -in approximately 1.5 times. Reduction of the stiffness coefficient of the gas layer kg in the end LS of the shaft (from 1.6*10 6 to 2*10 5 N / m) and in the LS dummis (from 4.6*10 6 to 5*10 5 N / m) with km equal 10 8 ...10 10 N / m practically does not affect the value ncr of the rotor [11][12][13][14][15][16][17][18][19][20].…”
Section: Introductionmentioning
confidence: 99%