Specific features of residual stress measurements in thermal barrier coatings


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Abstract

Techniques for measuring the residual stresses in bilayer thermal barrier coatings of a NiCrAlY alloy metal sublayer and 8-wt% stabilized ZrO2–8Y2O3 ceramic upper layer are developed with the inhomogeneous composition and stress relaxation upon removal of the top layers taken into account. The outer ceramic layer is shown to undergo quenching-induced tensile stress up to 200 MPa, whereas the metal sublayer is subjected to compressive stress of 600 MPa which is associated with an increase in the specific volume as a result of the formation of a thermally grown oxide (TGO).

About the authors

S. Y. Betsofen

Moscow Aviation Institute

Author for correspondence.
Email: s.betsofen@gmail.com
Russian Federation, Moscow, 125993

A. A. Ashmarin

Institute of Metallurgy and Material Sciences

Email: s.betsofen@gmail.com
Russian Federation, Moscow, 119991

A. A. Lozovan

Moscow Aviation Institute

Email: s.betsofen@gmail.com
Russian Federation, Moscow, 125993

B. V. Ryabenko

Scientific and Industrial Centre for Gas Turbine Technology “Saturn”

Email: s.betsofen@gmail.com
Russian Federation, Moscow, 105118

A. N. Lutsenko

All Russian Research Institute of Aviation Materials

Email: s.betsofen@gmail.com
Russian Federation, Moscow, 105118

A. M. Mamonov

Moscow Aviation Institute

Email: s.betsofen@gmail.com
Russian Federation, Moscow, 125993

D. E. Molostov

Moscow Aviation Institute

Email: s.betsofen@gmail.com
Russian Federation, Moscow, 125993

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