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      KCI등재 SCIE SCOPUS

      Identification of the dynamic performance of a gas foil journal bearing operating at high temperatures†

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      https://www.riss.kr/link?id=A103789227

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      다국어 초록 (Multilingual Abstract)

      This paper presents an experimental investigation of the dynamic force performance of gas foil bearings (GFBs) at high temperatures. A dynamic performance test rig with a GFB mounted on a rotating hollow shaft, heated by a cartridge heater inside the...

      This paper presents an experimental investigation of the dynamic force performance of gas foil bearings (GFBs) at high temperatures.

      A dynamic performance test rig with a GFB mounted on a rotating hollow shaft, heated by a cartridge heater inside the hollow shaft, andexcited by two orthogonally positioned electromagnetic shakers determines the frequency dependent stiffness and damping coefficientsof the test GFB for increasing shaft temperatures. The test heater temperatures are 21°C (room temperature without heating), 100°C,200°C, 300°C, and 400°C, and the excitation frequencies are 120 Hz, 140 Hz, 160 Hz, and 180 Hz. The test rotating speed and static loadare 12 krpm and 30 N, respectively. The vibration amplitude of the test GFB is adjusted to approximately 30 μm by controlling the poweramplifier connected to the electromagnetic shakers throughout the series of experiments. The test results show that both the direct stiffnessand damping coefficients of the test GFB increase with increasing excitation frequencies. As the shaft temperature increases, thedirect stiffness coefficients decrease by ~ 8%, and the direct damping coefficients decrease by approximately 30%. A model predictionbenchmarked against the test data reveals that the cross-coupled stiffness coefficients are smaller than the direct stiffness coefficients forthe test GFB.

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      참고문헌 (Reference)

      1 "http://www.hightempmetals.com/techdata/hitemp Inconel718data.php"

      2 "http://psec.uchicago.edu/thermal_coefficients/cte_metals_05517-90143.pdf"

      3 "Webpage:C200MicroTurbine"

      4 T. H. Kim, "Thermal performance measurement of a bump type gas foil bearing floating on a hollow shaft for increasing rotating speed and static load" 134 : 024501-, 2012

      5 S. Le Lez, "Static and dynamic characterization of a bump-type foil bearing structure" 129 : 75-83, 2007

      6 T. H. Kim, "Rotordynamic performance of an oil-free turboblower focusing on load capacity of gas foil thrust bearings" 134 (134): 022501-, 2012

      7 Y. B. Lee, "Rotordynamic performance measurement of an oil-free turbocompressor supported on gas foil bearings" P-1212-, 2010

      8 M. Salehi, "On the frictional damping characterization of compliant bump foils" 125 : 804-813, 2003

      9 Y.-B. Lee, "Numerical analysis for bump foil journal bearing considering top foil effect and experimental investigation" 2006

      10 S. Howard, "Misalignment in gas foil journal bearings: An experimental study" 131 : 022501-, 2009

      1 "http://www.hightempmetals.com/techdata/hitemp Inconel718data.php"

      2 "http://psec.uchicago.edu/thermal_coefficients/cte_metals_05517-90143.pdf"

      3 "Webpage:C200MicroTurbine"

      4 T. H. Kim, "Thermal performance measurement of a bump type gas foil bearing floating on a hollow shaft for increasing rotating speed and static load" 134 : 024501-, 2012

      5 S. Le Lez, "Static and dynamic characterization of a bump-type foil bearing structure" 129 : 75-83, 2007

      6 T. H. Kim, "Rotordynamic performance of an oil-free turboblower focusing on load capacity of gas foil thrust bearings" 134 (134): 022501-, 2012

      7 Y. B. Lee, "Rotordynamic performance measurement of an oil-free turbocompressor supported on gas foil bearings" P-1212-, 2010

      8 M. Salehi, "On the frictional damping characterization of compliant bump foils" 125 : 804-813, 2003

      9 Y.-B. Lee, "Numerical analysis for bump foil journal bearing considering top foil effect and experimental investigation" 2006

      10 S. Howard, "Misalignment in gas foil journal bearings: An experimental study" 131 : 022501-, 2009

      11 L. San Andrés, "Metal mesh foil bearing: Effect of motion amplitude, rotor speed, static load, and excitation frequency on force coefficients" 133 : 122503-, 2011

      12 N. Rayner, "Identification of dynamic coefficients of annular turbulent seals, NASA, Lewis Research Center Rotordynamic Instability Problems in High-Performance Turbomachinery" NASA 295-312, 1984

      13 T. H. Kim, "Heavily loaded gas foil bearings:A model anchored to test data" 130 : 012504-, 2008

      14 L. San Andres, "Forced nonlinear response of gas foil bearing supported rotors" 41 : 704-715, 2008

      15 H. W. Coleman, "Experimentation and Uncertainty Analysis for Engineers" Wiley 1998

      16 K. Sim, "Effect of cooling flow rate on temperature of a bump type gas foil bearing floating on a hot rotor" 2012

      17 S. Howard, "Dynamic stiffness and damping characteristics of a high-temperature air foil journal bearing" 44 : 657-663, 2001

      18 C. P. R. Ku, "Compliant foil bearing structural stiffness analysis: Part 1- Theoretical model including strip and variable bump foil geometry" 114 : 394-400, 1992

      19 C. P. R. Ku, "Compliant foil bearing structural stiffness analysis-Part2: Experimental investigation" 115 : 364-369, 1993

      20 T. H. Kim, "Characterization of a foil bearing structure at increasing temperatures:Static load and dynamic force performance" 131 : 041703-, 2009

      21 L. San Andres, "Analysis of gas foil bearings integrating FE top foil models" 42 : 111-120, 2009

      22 K. C. Radil, "An experimental investigation into the temperature profile of a compliant foil air bearing" 47 (47): 470-479, 2004

      23 M. Salehi, "Advancements in the structural stiffness and damping of a large compliant foil journal bearing: An experimental study" 129 : 154-161, 2007

      24 L. San Andrés, "A metal mesh foil bearing and a bump-type foil bearing: Comparison of performance for two similar size gas bearings" 2012

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      2016 1.04 0.51 0.84
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      0.74 0.66 0.369 0.12
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