Vibration induced hot spots in radial fluid film bearings can cause spiral vibrations. The phenomenon is known as Morton effect. Various authors have described the phenomenon of spiral vibrations caused by rubbing in general [1 – 4] and specifically by the differential viscous shearing in fluid film bearings [5 – 8]. The history of the case of a turbo-expander for the cryogenic industry is described. The investigated machine has a single relatively stiff rotor with two overhung impellers. The rotor is supported on two tilting pad bearings, as they are commonly used for these applications. It was designed in line with API 617 7th edition [11]. During internal factory testing excessive vibration at high speed suddenly developed, in spite of very high damping and comfortable separation margins of the relevant rotor vibration modes. The vibrations evolution in a polar plot had the appearance of a spiral, as they are typically observed in case of vibration induced hot spots. The tilting pad bearings were suspected as the most likely cause for the hot spots. In parallel to the tests, hot spot stability analyses with a rotor dynamic model of the turbo-expander were carried out. The applied method, introduced by Schmied [5] allows the handling of general rotor systems. The hot spot model is based on the theory of Kellenberger [3] using a thermal equation between the shaft’s thermal deflection and the shaft displacement at the hot spot location. The analytical results gave evidence of the instabilities and confirmed the fluid-film bearings as the source of the hot spot. The model was used to assess changes for the solution of the problem. The following measures were studied: Reduction of the oil viscosity, stiffening of the rotor and reduction of the bearing width. The final successfully implemented solution was a combination of lower bearing width and reduced viscosity. Apart from this thoroughly studied case, an overview of further turbo-expanders regarding their hot spot behavior is given.
Skip Nav Destination
ASME Turbo Expo 2008: Power for Land, Sea, and Air
June 9–13, 2008
Berlin, Germany
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4315-4
PROCEEDINGS PAPER
Hot Spots in Turboexpander Bearings: Case History, Stability Analysis, Measurements and Operational Experience
Joachim Schmied,
Joachim Schmied
DELTA JS, Zu¨rich, Switzerland
Search for other works by this author on:
Josef Pozivil,
Josef Pozivil
Cryostar SAS, He´singue, France
Search for other works by this author on:
Joseph Walch
Joseph Walch
Cryostar SAS, He´singue, France
Search for other works by this author on:
Joachim Schmied
DELTA JS, Zu¨rich, Switzerland
Josef Pozivil
Cryostar SAS, He´singue, France
Joseph Walch
Cryostar SAS, He´singue, France
Paper No:
GT2008-51179, pp. 1267-1277; 11 pages
Published Online:
August 3, 2009
Citation
Schmied, J, Pozivil, J, & Walch, J. "Hot Spots in Turboexpander Bearings: Case History, Stability Analysis, Measurements and Operational Experience." Proceedings of the ASME Turbo Expo 2008: Power for Land, Sea, and Air. Volume 5: Structures and Dynamics, Parts A and B. Berlin, Germany. June 9–13, 2008. pp. 1267-1277. ASME. https://doi.org/10.1115/GT2008-51179
Download citation file:
35
Views
Related Proceedings Papers
Related Articles
Active Control of Rotor Vibrations by Two Feedforward Control Algorithms
J. Dyn. Sys., Meas., Control (September,2009)
Performance Analysis of Capillary Compensated Hybrid Journal Bearing by Considering Combined Influence of Thermal Effects and Micropolar Lubricant
J. Tribol (January,2017)
Transient Analysis of Gas-Expanded Lubrication and Rotordynamic Performance in a Centrifugal Compressor
J. Eng. Gas Turbines Power (April,2016)
Related Chapters
Research Tools
Bearing Dynamic Coefficients in Rotordynamics: Computation Methods and Practical Applications
Summary and Conclusions
Bearing Dynamic Coefficients in Rotordynamics: Computation Methods and Practical Applications
Unbalance
Fundamentals of Rotating Machinery Diagnostics