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Volumn , Issue , 1999, Pages 1-10

The application of foil seals to a gas turbine engine

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PROPULSION; FOIL BEARINGS; GAS TURBINES; HIGH TEMPERATURE APPLICATIONS; ROLLER BEARINGS; SIMULATORS;

EID: 84963860072     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-2821     Document Type: Conference Paper
Times cited : (17)

References (7)
  • 1
    • 33748164866 scopus 로고    scopus 로고
    • On the performance of Hybrid Foil-Magnetic Bearings
    • ASME paper, 98-GT-378, Presented at the, Stockholm, Sweden June 2-5,1998
    • Heshmat, H., Chen, H.M., and Walton, J.F, 1998, “On the performance of Hybrid Foil-Magnetic Bearings”, ASME paper, 98-GT-378, Presented at the International Gas Turbine & Aero-engine Congress & Exhibition, Stockholm, Sweden June 2-5,1998.
    • (1998) International Gas Turbine Aero-Engine Congress & Exhibition
    • Heshmat, H.1    Chen, H.M.2    Walton, J.F.3
  • 3
    • 0020834644 scopus 로고
    • Analysis of Gas-Lubricated Compliant Thrust Bearings
    • ASME
    • Heshmat, H., Walowit, J., and Pinkus, O. “Analysis of Gas-Lubricated Compliant Thrust Bearings.” J. Lubr. Tech. Trans. ASME 105, no. 4 (1983): 638-646.
    • (1983) J. Lubr. Tech. Trans , vol.105 , Issue.4 , pp. 638-646
    • Heshmat, H.1    Walowit, J.2    Pinkus, O.3
  • 4
    • 0026843276 scopus 로고
    • Compliant Foil Bearing Structural Stiffness Analysis: Part I--Theoretical Model Including Strip and Variable Bump Foil Geometry
    • ASME
    • Ku, C.-P.R., and Heshmat, H. “Compliant Foil Bearing Structural Stiffness Analysis: Part I--Theoretical Model Including Strip and Variable Bump Foil Geometry.” Journal of Tribology, Trans. ASME Vol. 114, no. 2 (1992): 394-400.
    • (1992) Journal of Tribology, Trans , vol.114 , Issue.2 , pp. 394-400
    • Ku, C.-P.R.1    Heshmat, H.2
  • 5
    • 0343142284 scopus 로고
    • Compliant Foil Bearings For Use In Cryogenic Turbopumps
    • Held at NASA/MSFCMay 17-19, 1994, NASA CP3282, Sept. 19
    • Walton, J.F. and Heshmat, H. “Compliant Foil Bearings For Use In Cryogenic Turbopumps.” Proceedings of Advanced Earth-to-Orbit Propulsion Technology Conference Held at NASA/MSFCMay 17-19, 1994, NASA CP3282 Vol. 1, Sept. 19,1994, pp. 372-381.
    • (1994) Proceedings of Advanced Earth-To-Orbit Propulsion Technology Conference , vol.1 , pp. 372-381
    • Walton, J.F.1    Heshmat, H.2
  • 6
    • 84926380540 scopus 로고
    • Relative Performance Comparison Between Baseline Labyrinth and Dual-Brush Compressor Discharge Seals in a T-700 Engine Test
    • The Hague, Netherlands, June 13-16, Paper No. 94-GT-266
    • Hendricks, R.C., Griffin, T.A., Kline, T.R., Csavina, K.R., Pancholi, A., and Sood, D., 1994a, “Relative Performance Comparison Between Baseline Labyrinth and Dual-Brush Compressor Discharge Seals in a T-700 Engine Test,” 39th ASME International Gas Turbine and Aero-engine Conference, The Hague, Netherlands, June 13-16, 1994.Paper No. 94-GT-266
    • (1994) 39Th ASME International Gas Turbine and Aero-Engine Conference
    • Hendricks, R.C.1    Griffin, T.A.2    Kline, T.R.3    Csavina, K.R.4    Pancholi, A.5    Sood, D.6


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.