Gas turbine hot section parts are high-value components which have finite lives. Their durability has an important role in controlling maintenance intervals and the associated costs. This paper reviews the sources of degradation in some components, the technology available to quantify the damage, and publicly available assessment procedures which can be used for component life assessment.
WoodM. I.Internal damage accumulation and imminent failure of an industrial gas turbine blade. ASME Conference preprint 96-GT-510, 1996 (American Society of Mechanical Engineers, New York).
2.
WilsonJ. D.Van ZeverenF.TouchtonG.Siemens V84.2/V94.2 combustion turbine life management system. In Proceedings of the Quadrennial Power Stations Conference, Association des Ingenieurs de Montefiore, Liege, Belgium, 1997, pp. 335–338.
3.
SwaminathanV. P.AllenJ. M.Surface degradation and cracking in combustion turbine blade cooling passages. Mater. Mfg Processes, 1995, 10, 867–886.
4.
BernsteinH. L.Life management system for the GE Frame 7E gas turbine. In Life Assessment and Repair Technology for Combustion Turbine Hot Section Components, 1990, pp. 111–118 (American Society for Metals, Metals Park, Ohio).
5.
ToupinT.GT field data management: A prerequisite for reliability centred maintenance implementation and reliability-availability-maintainability optimisation. In Proceedings of ‘PowerGen’ 95, Asia', 1995, Vol. 2, pp. 335–354 (penwell Publishing).
6.
HoffelnerW.Lifetime analysis of highly loaded hot section components in industrial turbines. In Life Assessment and Repair Technology for Combustion Turbine Hot Section Components, 1990, pp. 35–39 (American Society for Metals, Metals Park, Ohio).
7.
KarlssonS.-ÃPerssonC.PerssonP.-O.Metallo-graphic approach to turbine blade life time predictions. Mater. Mfg Processes, 1995, 10, 939–953.
8.
McClungR. C.BernsteinH. L.BuckinghamJ. P.AllenJ. M.TouchtonG. L.Probabilistic analysis of industrial gas turbine durability. ASME Conference preprint 93-GT-427, 1993 (American Society of Mechanical Engineers, New York).
9.
WoodM. I.The assessment of service induced degradation of nickel based superalloy gas turbine blading. Mater. Mfg Processes, 1995, 10, 903–924.
10.
WoodfordD. A.Test methods for accelerated development, design and life assessment of high temperature alloys. Mater. Des., 1993, 14, 231–242.
11.
RoothR.On-line blade temperature measurement. In Proceedings of the Quadrennial Power Stations Conference, Association des Ingenieurs de Montefiore, LiÃe, Belgium, 1997, pp. 345–352.