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Failure Analysis Case Studies N
                   D.R.H. Jones (Editor)
                   0 2001 Elsevier Science Ltd.  All rights reserved                       21 1






                              AN  INVESTIGATION  OF  THE  FAILURE  OF  LOW
                                    PRESSURE  STEAM  TURBINE BLADES


                              N. K. MUKHOPADHYAY, S. GHOSH CHOWDHURY,* G. DAS,
                                 I. CHATTORAJ, S. K. DAS and D. K. BHATTACHARYA
                                     National Metallurgical Laboratory, Jamshedpur 831007, India
                                                 (Receiued 16 March 1998)

                       Abstract-An  analysis of the failure of LP turbine blades of a 210 MW thermal power plant has been presented
                       in this paper. The blade material is of 12% Cr steel with tempered martensitic microstructure. Microstructural
                       analysis as well as hardness and tensile tests did not indicate any degradation in terms of microstructure and
                       mechanical properties. Physical discontinuities were observed in the braze joint which might have been formed
                       due to improper brazing operation. Failure of the brazed joints between the blade and lacing rod was found
                       to be due to improper brazing operations and corrosion effects during service. Fractographic evidence showed
                       that the cracks were initiated from various points on the blade surface, which were at the interface with the
                       lacing rod.  Striations and beach marks were  also observed which  indicated the occurrence of  high  cyclic
                       loading on the blades.  Frequency data obtained from plant indicated the possibility  of excessive Vibration
                       generated due to fluctuation in grid frequency during operation. Thus, the situation was aggravated due to a
                       resonant condition of vibration, facilitating the propagation of cracks which were initiated earlier. Q 1998
                       Elsevier Science Ltd. All rights reserved.
                       Keywords: Thermal power plant, turbine blade failure, vibration. fatigue.


                                                1.  INTRODUCTION

                   Steam turbine blades are critical components in power plants which convert the linear motion of
                   high temperature and high pressure steam flowing down a pressure gradient into a rotary motion
                   of the turbine shaft. As the steam enters turbine from the boiler, it passes through different stages
                   such as high pressure (HP), intermediate pressure (IP) and low pressure (LP) zones. Statistics shows
                   that LP turbine blades are generally more susceptible to failure compared to those of the HP and
                   IP. There are various mechanisms by which LP blades fail [I-31.  Almost 50% of the failures are
                   related to fatigue, stress corrosion cracking and corrosion fatigue. The fatigue failure takes place as
                   a result of vibration  arising from the fluctuation of bending stress due to the asymmetric flow of
                   steam. Once a crack is initiated, the component is assumed to have failed since crack growth takes
                   place rapidly.  Even  this  fatigue failure  can  be  accentuated  by  corrosion.  Creep damage  is not
                   important for the LP blades. It is reported that failure initiates from various locations of the blade
                   and these are 26% from shroud, 20% from lacing hole, 40% in the aerofoil region and 14% in the
                   blade attachment [l]. Therefore, the mechanism of the failure varies along the length of the blades.
                     In general, LP blades in a steam turbine assembly are designed to run for 30 years, but many
                   cases of  premature  failure of  blades are encountered  in practice.  A recent survey indicates that
                   causes for about 40% of the failures could not be pinpointed [l]. To reduce the incidence of failure,
                   it is necessary to take into account all the aspects important for the performance of a blade. Thus,
                   it  is  necessary to  understand  the  metallurgy  of  the  blade  material,  operating  stresses and  the
                   operating environment. As the blade’s design is complex, the actual state of stress is highly compli-
                   cated. However, if the design conditions do not deviate in service, the state of the stresses in a blade
                   should not cause any concern. The stresses acting on the blades mainly originate from centrifugal
                   loading and vibratory  response of the blades. Vibratory  stresses are normally maintained  at low



                    *Author lo whom correspondence should be addressed.
                   Reprinted from Engineering Failure Analysis 5 (3), 18 1-1 93 (1 998)
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