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TECHNICAL PAPERS

Stress Redistribution for Increased Creep Life in the GE MS6001 B Second-Stage Blade

[+] Author and Article Information
P. E. DiCristoforo

TurboCare, 2140 Westover Road, Chicopee, MA 01022

M. Elledge

BP Amoco Chemicals, 510 Old Bayou Drive, Dickinson, TX 77539

J. Eng. Gas Turbines Power 126(1), 127-130 (Mar 02, 2004) (4 pages) doi:10.1115/1.1498271 History: Received December 01, 2000; Revised March 01, 2001; Online March 02, 2004
Copyright © 2004 by ASME
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References

Jaqueway, J. K., and Pistor, R. J., 1997, “Redesign of the MS6001 First Stage Bucket for Improved Cooling and Extended Life,” presented at IGTI Turbo Expo in Orlando, FL, June.
White, F. M., 1984, Heat Transfer, Addison-Wesley, Reading, MA.
Webb,  R. L., Eckert,  E. R. G., and Goldstein,  R. J., 1971, “Heat Transfer and Friction in Tubes with Repeated-Rib Roughness” Int. J. Heat Mass Transf., 14, pp. 601–617.
Granacher, J., and Preussler, T., 1987, “Creep of Some Gas Turbine Materials,” Advances in Materials Technology for Fossil Powered Plants, pp. 511–518.

Figures

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Pressure side stress comparison (Mpa)
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Suction side stress comparison (MPa)
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Pitchline stress comparison (MPa)
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Pressure side temperature comparison (°C)
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Suction side temperature comparison (°C)
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Pitchline temperature comparison (°C)
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Shroud mismatch after 48,000 hours

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