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                       50 Hz frequency range and 1 % was above 51.5 Hz. Thus the resonant vibration was highly probable
                       and could lead  to high vibratory  stress. In addition  to  resonant  vibration,  the fluctuations from
                       under-frequency to over-frequency operation and frequent interruption  of the normal  operation
                       obviously would have caused excessive vibration which the defective and corroded braze joints were
                       unable to withstand leading to situations conducive to crack initiation and ultimately to failure.
                       From our simulated HCF test it was concluded that damage accumulation at a lower load can lead
                       to crack initiation rapidly even though the mean stress is increased slightly. If thc braze joint had
                       been strong enough, the short term effect  of resonance or frequency fluctuation demanded from the
                       system of power supply could have been overcome and the blades would have survived. Thus, faulty
                       brazing and improper operating conditions had a combined effect leading to the present failure. It
                       appears that the degradation of the braze joint was the primary cause and the vibrations causing
                       high cycle fatigue was the ultimate cause of failure of the turbine blades.


                                                    5. CONCLUSIONS
                         The work has shown that the LP blades of a steam turbine, whose material conditions were found
                       to be good,  failed due to high cycle fatigue. The fatigue loading conditions were brought  about
                       primarily by the failure of braze joints which had been used to join the lacing rods to the blades to
                       impart rigidity.
                         Due to failure of the brazed joints, the natural frequencies of the blades were affected. Fretting
                       between the lacing rod and blade interface was operative and led to the formation of weak points
                       favourable for fatigue crack initiation. The failure of the brazed joint was due to a poor  brazing
                       operation carried out during the earlier overhauling period, worsened by corrosion during service.
                       The crack growth was aided by excessive vibration due to frequent fluctuation from under-frequency
                       to over-frequency operation. The effect of resonant vibration, which also seemed to occur, would
                       lead to an increase in AK value and mean stress of the cyclic loading and favour the situation of
                       crack initiation and growth.

                       Acknowledgements-The  authors would like to thank  Drs  R. N. Ghosh, S. Tarafder, V.  Ranganath, N. Parida and  G.
                       Sridhar for many  stimulating discussions. The authors are grateful  to Prof. I?.  Ramachandra Rao.  Director, National
                       Metallurgical Laboratory, for encouragement and permission to publish this work.


                                                      REFERENCES
                        1.  Atrens, A., Meyer. H.,  Faber, G. and Schneider. K.. in Corrosion in Power Generatinq Equipment. ed. M. 0. Speidel and
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                        2.  Modern Power Stalion Practice, 3rd edn. British Electricity International, Pergamon Press, 1992, p. 73.
                        3.  Viswanathan, R., Damage Mechanisms and Life Assessment of  High Temperature Components. ASM International. 1989.
                         p. 313.
                        4. Failure Analysis of  Steam Turbine Blades. NML Report: NML/MTC/CIEP/I.46,  1997.
                        5.  Beeven, C. J., Cook, R. J.,  Knott, J. F. and Ritchie, R. O., Metal Science, 1975, 9, 119.
                        6.  Griffiths, J. R.. Mogford, I. L. and Richards, C. E.. MetalScience, 1971. 5, 150.
                        7.  Mcdonald, M. M., in Metals Handbook, Vol. 13,9th edn. ASM International, p. 876.
                        8.  Kawakatsu, I.,  WeldJ., 1973, 52,2335.
                        9.  Kearton, W. J., Steam  Turbine Theory and Practice. CBS Publishers, 1988.
                       10.  Dieter, G. E., MechanLul Metallurgy. McGraw-Hill Publication, 1988, p. 375.
                       I I.  Tarafder, S., in Failure Analysis, ed. S. R. Singh et al. NML, 1997, p. 147.
                       12. Thornton. D. L., Mechanics Applied to  Vibration and Balance. Chapman & Hall Ltd, 1951, p. 560.
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