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Original Articles

Performance of a Complaint Foil Seal in a Small Gas Turbine Engine Simulator Employing a Hybrid Foil/Ball Bearing Support System

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Pages 458-464 | Published online: 25 Mar 2008

REFERENCES

  • Heshmat , H. , “ Advancements in the Performance of Aerodynamic Foil Journal Bearings: High Speed and Load Capability ,” Trib. Trans. , 116 , 1 , pp 287 – 295 ( 1994 ).
  • Salehi , M. and Heshmat , H. , “ On the Flow and Thermal Analysis of the Compliant Gas Foil Seal and Foil Bearing ,” Trib. Trans. , 43 , 2 , pp 318 – 324 ( 2000 ).
  • DellaCorte , C. , Valco , M. J. , Radil , K. C. and Heshmat , H. , “ Performance and Durability of High Temperature Foil Bearings for Oil-Free Turbomachinery ,” NASA/TAM-1999–209187 , presented at 55th STLE Annual Meeting, May 7–11, ( 1999 ).
  • Ku , C.-P. R. and Heshmat , H. , “ Compliant Foil Bearing Structural Stiffness Analysis Part I: Theoretical Model Including Strip and Variable Bump Foil Geometry ,” Jour. of Trib., Trans ASME , 113 , 2 , pp 364 – 369 ( 1992 ).
  • Salehi , M. , Heshmat , H. , Walton , J. and Cruzen , S. , “ The Application of Foil Seals to a Gas Turbine Engine ,” MAA Paper 99–2821, 35th MAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit , June 20–24, ( 1999 ).
  • Hendricks , R. C. , Griffin , T. A. , Kline , T. R. , Csavina , K. R. , Pancholi , A. and Sood , D. , “ Relative Performance Comparison Between Baseline Labyrinth and Dual-Brush Compressor Discharge Seals in a T-700 Engine Test ,” in Proc. 39th ASME Int'l. Gas Turbine and Aero-engine Conf., The Hague, Netherlands , Paper No. 94-GT-266 , ( 1994 ).

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