Method for estimation of the average local working temperatures and the residual resource of metal coatings of gas-turbine blades

Krukovskii, P. G.; Tadlya, K.

doi:10.1007/s10891-007-0058-0

Cited by 2 publications

(2 citation statements)

References 1 publication

Supporting

Mentioning

Contrasting

Order By: Relevance

“…In case of NiCoCrAlY coatings, applied on gas turbines blades and vanes to withstand oxidation and corrosion, the evaluation of the service temperature is generally based on the depletion of the dispersed ß phase or on the evolution of the interdiffusion layers [12,13]. New metallic coatings are characterized by the addition of small amounts of other elements like Re.…”

Section: Introductionmentioning

confidence: 99%

Development of a Tool for Temperature Estimation From Microstructural Condition of a Nicoraly+Re Coating Applied on the Surface of Gas Turbine Hot Components

Costa

Vacchieri

Barbareschi

et al. 2013

Journal of Engineering for Gas Turbines and Power

View full text Add to dashboard Cite

The hot gas path components of gas turbines have to withstand to severe conditions in terms of high temperature oxidation, hot corrosion, and creep-fatigue phenomena. The evaluation of components residual life is an important matter for gas turbines producers and the estimation of service temperatures is a key tool for this evaluation. The most diffused methods to estimate service temperatures of gas turbines blades and vanes in Ni based superalloys are related to the microstructural evolution of the dispersed intermetallic phase y, NÍ3AI. The aim of this work has been the determination of a tool to estimate service temperature on the basis of the microstructural evolutions of a NiCoCrAlY-\-Re coating. In order to obtain a deep characterization of the coating after exposure at different durations and temperatures, an extensive experimental test program has been planned. Samples of Ni based superalloys, covered by the investigated coating, have been aged in chamber furnaces in the temperature range 700 °C-1000 °C with durations up to 20,000 h. The microstructure of this coating is characterized by ß phase, NiAl, which is the Al reservoir, embedded in the matrix, that is constituted by 7' phase at low temperature and by y phase over 900°C. Moreover, electron back scattered diffraction and X-ray diffraction measurements on samples have revealed three classes of secondary phases: the first one has been identified as a-Cr2Re3, the second one as Cr carbideCr23C(j and the third one as a-Cr. a phase is very abundant at the lower temperatures while it disappears after long exposures at temperatures higher than 900 °C. The a phase composition is different at different temperatures and the Re content in particular increases with the temperature. Starting from the a phase composition determined at different temperatures, a tool has been constructed that relates the service temperature to the Re content in the same phase. The new tool has been applied to the analyses of different components. The results of the new method have been compared to those ones obtained with the method based on y' features, developed in the past through huge experimental campaigns. The agreement between the two methods is generally good, they can be used in a complementary way due to the fact that the 7' one seems to be more suitable for high temperature ranges (T > 900 °C) where it gives a reliable estimation, while the a method is more suitable in the temperature range 700 °C-900 °C.

show abstract

Section: Introductionmentioning

confidence: 99%

Development of a Tool for Temperature Estimation From Microstructural Condition of a Nicoraly+Re Coating Applied on the Surface of Gas Turbine Hot Components

Costa

Vacchieri

Barbareschi

et al. 2013

Journal of Engineering for Gas Turbines and Power

View full text Add to dashboard Cite

show abstract

“…This full characterization enables the development of an evolution library that is useful as feedback in calculation and simulation processes or as a source of empirical parameters defining a direct relationship between data and working temperature [12,13].…”

Section: Introductionmentioning

confidence: 99%

Phase evolution in an MCrAlY coating during high temperature exposure

Costa

Barbareschi

Guarnone

et al. 2012

J min metall B Metall

View full text Add to dashboard Cite

MCrAlY (M = Ni and/or Co) coating systems are often applied on gas turbine blades and vanes to withstand the challenges of severe conditions. During service MCrAlY coatings are subjected to microstructural transformations that can be an indication of components service temperatures. The development of indirect methods to measure this parameter is of great concern in the gas turbine “world” due to the impossibility of direct measurements. \ud In the present work the evolution of an MCrAlY coating applied on René80 by LPPS (Low Pressure Plasma Spray) technique has been studied in order to verify if it was possible to identify a microstructural indicator of the service temperature. The specimens were exposed for different lengths of time at test temperatures of 700 – 800 – 900 °C in order to characterize the phase evolution with time and temperature. Selective etching was employed for optical metallographic investigation. Scanning Electron Microscopy (SEM) observation combined with Electron Backscattered Diffraction (EBSD) and Energy Dispersive Spectroscopy (EDS) showed that the coating is composed of a γ- Co matrix, β-AlNi, σ-(Cr, Co), Cr carbide and Y-rich phases. Among these phases, the sigma phase resulted in a temperature – composition dependence that can be a useful tool for evaluating the local service temperature and modelling the residual lifetime

show abstract

Method for estimation of the average local working temperatures and the residual resource of metal coatings of gas-turbine blades

Cited by 2 publications

References 1 publication

Development of a Tool for Temperature Estimation From Microstructural Condition of a Nicoraly+Re Coating Applied on the Surface of Gas Turbine Hot Components

Development of a Tool for Temperature Estimation From Microstructural Condition of a Nicoraly+Re Coating Applied on the Surface of Gas Turbine Hot Components

Phase evolution in an MCrAlY coating during high temperature exposure

Contact Info

Product

Resources

About