Status of Through-Process Simulation for Coated Gas Turbine Components (TP C8)

R. Herzog; N. Warnken; I. Steinbach; B. Hallstedt; C. Walter; J. Müller; D. Hajas; E. Münstermann; J. M. Schneider; R. Nickel; D. Parkot; K. Bobzin; E. Lugscheider; P. Bednarz; O. Trunova; L. Singheiser

doi:10.1002/9783527610983.ch5

Status of Through-Process Simulation for Coated Gas Turbine Components (TP C8)

R. Herzog^*, N. Warnken, I. Steinbach, B. Hallstedt, C. Walter, J. Müller, D. Hajas, E. Münstermann, J. M. Schneider, R. Nickel, D. Parkot, K. Bobzin, E. Lugscheider, P. Bednarz, O. Trunova, L. Singheiser

^*Corresponding author for this work

Metallurgy and Materials

Research output: Chapter in Book/Report/Conference proceeding › Chapter

Abstract

This chapter gives an overview on integrative, through-process modeling and simulation approach for coated turbine blades on different scales. The approach includes the modeling of the production, materials properties, and in-service degradation processes and is accompanied by the actual production and testing of coated CMSX-4 single-crystal turbine blades and laboratory specimens. Especially, solidification of the blade alloy during casting, microstructural changes during homogenization and aging heat treatments, chemical vapor deposition of an Al₂O₃ diffusion barrier coating, physical vapor deposition (sputtering) of a (Ni,Co)CrAlY bond coat, atmospheric plasma spraying of a Y₂O₃ stabilized ZrO₂ thermal barrier coating, microstructural changes, and development of critical stresses under in-service conditions are addressed.

Original language	English
Title of host publication	Integral Materials Modeling: Towards Physics-Based Through-Process Models
Publisher	Wiley Interscience/John Wiley and Sons
Pages	49-61
Number of pages	13
ISBN (Print)	9783527317110
DOIs	https://doi.org/10.1002/9783527610983.ch5
Publication status	Published - 26 Apr 2007

Keywords

Alumina interdiffusion barrier
Atmospheric plasma spraying of ceramic TBC
Bond coat/TBC interface
Coated gas turbine components
Crack formation
CVD processing
Heat treatment
Integral materials modeling
Nickel-based superalloy
Solidification
Through-process simulation
TP C8

ASJC Scopus subject areas

Materials Science(all)

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10.1002/9783527610983.ch5

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Herzog, R., Warnken, N., Steinbach, I., Hallstedt, B., Walter, C., Müller, J., Hajas, D., Münstermann, E., Schneider, J. M., Nickel, R., Parkot, D., Bobzin, K., Lugscheider, E., Bednarz, P., Trunova, O., & Singheiser, L. (2007). Status of Through-Process Simulation for Coated Gas Turbine Components (TP C8). In Integral Materials Modeling: Towards Physics-Based Through-Process Models (pp. 49-61). Wiley Interscience/John Wiley and Sons. https://doi.org/10.1002/9783527610983.ch5

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title = "Status of Through-Process Simulation for Coated Gas Turbine Components (TP C8)",

abstract = "This chapter gives an overview on integrative, through-process modeling and simulation approach for coated turbine blades on different scales. The approach includes the modeling of the production, materials properties, and in-service degradation processes and is accompanied by the actual production and testing of coated CMSX-4 single-crystal turbine blades and laboratory specimens. Especially, solidification of the blade alloy during casting, microstructural changes during homogenization and aging heat treatments, chemical vapor deposition of an Al2O3 diffusion barrier coating, physical vapor deposition (sputtering) of a (Ni,Co)CrAlY bond coat, atmospheric plasma spraying of a Y2O3 stabilized ZrO2 thermal barrier coating, microstructural changes, and development of critical stresses under in-service conditions are addressed.",

keywords = "Alumina interdiffusion barrier, Atmospheric plasma spraying of ceramic TBC, Bond coat/TBC interface, Coated gas turbine components, Crack formation, CVD processing, Heat treatment, Integral materials modeling, Nickel-based superalloy, Solidification, Through-process simulation, TP C8",

author = "R. Herzog and N. Warnken and I. Steinbach and B. Hallstedt and C. Walter and J. M{\"u}ller and D. Hajas and E. M{\"u}nstermann and Schneider, {J. M.} and R. Nickel and D. Parkot and K. Bobzin and E. Lugscheider and P. Bednarz and O. Trunova and L. Singheiser",

year = "2007",

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doi = "10.1002/9783527610983.ch5",

language = "English",

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Herzog, R, Warnken, N, Steinbach, I, Hallstedt, B, Walter, C, Müller, J, Hajas, D, Münstermann, E, Schneider, JM, Nickel, R, Parkot, D, Bobzin, K, Lugscheider, E, Bednarz, P, Trunova, O & Singheiser, L 2007, Status of Through-Process Simulation for Coated Gas Turbine Components (TP C8). in Integral Materials Modeling: Towards Physics-Based Through-Process Models. Wiley Interscience/John Wiley and Sons, pp. 49-61. https://doi.org/10.1002/9783527610983.ch5

TY - CHAP

T1 - Status of Through-Process Simulation for Coated Gas Turbine Components (TP C8)

AU - Herzog, R.

AU - Warnken, N.

AU - Steinbach, I.

AU - Hallstedt, B.

AU - Walter, C.

AU - Müller, J.

AU - Hajas, D.

AU - Münstermann, E.

AU - Schneider, J. M.

AU - Nickel, R.

AU - Parkot, D.

AU - Bobzin, K.

AU - Lugscheider, E.

AU - Bednarz, P.

AU - Trunova, O.

AU - Singheiser, L.

PY - 2007/4/26

Y1 - 2007/4/26

N2 - This chapter gives an overview on integrative, through-process modeling and simulation approach for coated turbine blades on different scales. The approach includes the modeling of the production, materials properties, and in-service degradation processes and is accompanied by the actual production and testing of coated CMSX-4 single-crystal turbine blades and laboratory specimens. Especially, solidification of the blade alloy during casting, microstructural changes during homogenization and aging heat treatments, chemical vapor deposition of an Al2O3 diffusion barrier coating, physical vapor deposition (sputtering) of a (Ni,Co)CrAlY bond coat, atmospheric plasma spraying of a Y2O3 stabilized ZrO2 thermal barrier coating, microstructural changes, and development of critical stresses under in-service conditions are addressed.

AB - This chapter gives an overview on integrative, through-process modeling and simulation approach for coated turbine blades on different scales. The approach includes the modeling of the production, materials properties, and in-service degradation processes and is accompanied by the actual production and testing of coated CMSX-4 single-crystal turbine blades and laboratory specimens. Especially, solidification of the blade alloy during casting, microstructural changes during homogenization and aging heat treatments, chemical vapor deposition of an Al2O3 diffusion barrier coating, physical vapor deposition (sputtering) of a (Ni,Co)CrAlY bond coat, atmospheric plasma spraying of a Y2O3 stabilized ZrO2 thermal barrier coating, microstructural changes, and development of critical stresses under in-service conditions are addressed.

KW - Alumina interdiffusion barrier

KW - Atmospheric plasma spraying of ceramic TBC

KW - Bond coat/TBC interface

KW - Coated gas turbine components

KW - Crack formation

KW - CVD processing

KW - Heat treatment

KW - Integral materials modeling

KW - Nickel-based superalloy

KW - Solidification

KW - Through-process simulation

KW - TP C8

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M3 - Chapter

AN - SCOPUS:84890692764

SN - 9783527317110

SP - 49

EP - 61

BT - Integral Materials Modeling: Towards Physics-Based Through-Process Models

PB - Wiley Interscience/John Wiley and Sons

ER -

Status of Through-Process Simulation for Coated Gas Turbine Components (TP C8)

Abstract

Keywords

ASJC Scopus subject areas

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