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Discussion Group T11: Dry Gas Seals for Compressors
(Turbomachinery Laboratories, Texas A&M Engineering Experiment Station, 2015)
Operational modal analysis application for the measure of logarithm decrement in centrifugal compressor
(Turbomachinery Laboratories, Texas A&M Engineering Experiment Station, 2015)
The results of a stability test on a centrifugal compressor during the full load test of the entire compression train are presented. A Magnetic Exciter was installed at the shaft end in order to excite the first lateral ...
Numerical Prediction And Experimental Validation Of Rotor Thermal Instability
(Turbomachinery Laboratories, Texas A&M Engineering Experiment Station, 2015)
The increasing demand of higher efficiency and increased equipment compactness is pushing the modern rotordynamic design towards higher and higher bearing peripheral speeds. Due to the increased viscous dissipation, fluid ...
Axial Thrust in High Pressure Centrifugal Compressors: Description of a Calculation Model Validated by Experimental Data from Full Load Test
(Turbomachinery Laboratories, Texas A&M Engineering Experiment Station, 2015)
The residual axial thrust acting on the rotor of a centrifugal compressor is the result of the non-uniform pressure distribution on the surfaces in contact with the process gas, plus the differential pressure acting on the ...
Discussion Group T09: Advanced Topics in Centrifugal Compressor Design
(Turbomachinery Laboratories, Texas A&M Engineering Experiment Station, 2015)