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Now showing items 11-20 of 26
Honeycomb Seal Effect on Rotor Response to Unbalance
(Texas A&M University. Turbomachinery Laboratories, 2014)
High pressure centrifugal compressors are often equipped with honeycomb seal on balance drum in order to optimize rotordynamic stability. In very high pressures applications (>200 bar) the direct stiffness and damping of ...
Discussion Group T11 Dry Gas Seals for Compressors and Pumps
(Texas A&M University. Turbomachinery Laboratories, 2013)
Discussion Group T9: Advanced Topics in Centrifugal Compressor Design
(Texas A&M University. Turbomachinery Laboratories, 2014)
Discussion Group T9 Advanced Topics in Centrifugal Compressor Design
(Texas A&M University. Turbomachinery Laboratories, 2013)
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 T18 Advanced Topics in Centrifugal Compressor Design
(Texas A&M University. Turbomachinery Laboratories, 2012)
Discussion Group T3 Dry Gas Seals for Compressors and Pumps
(Texas A&M University. Turbomachinery Laboratories, 2012)
Discussion Group T11: Dry Gas Seals for Compressors
(Texas A&M University. Turbomachinery Laboratories, 2014)
Definition of a Screening Criterion for Centrifugal Compressor Vibrations Induced by Inlet Gas Flow
(Turbomachinery Laboratories, Texas A&M Engineering Experiment Station, 2016)
Lecture 4: The gas flow entering from the inlet flange of a centrifugal compressor may induce radial forces on the rotor, by directly impinging onto shaft or by generating asymmetric pressure fluctuations in the gas volume ...