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Now showing items 11-20 of 27
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 ...
Dry Gas Seals for Compressors
(Turbomachinery Laboratory, Texas A&M Engineering Experiment Station, 2018)
How to specify an integrally geared compressor
Typical process applications
Controlling an integral gear compressor - IGV, VFD
Rotordynamic considerations
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)
Optimization of Swirl Brake Design and Assessment of Its Stabilizing Effect on Compressor Rotordynamic Performance
(Texas A&M University. Turbomachinery Laboratories, 2014)
The rotordynamic stability of high pressure compressors is strongly affected by the aerodynamic effects induced by the gas flow through rotor-stator seals. In particular the tangential velocity (swirl) of the gas flowing ...