Specific features of residual stress measurements in thermal barrier coatings


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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).

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S. Betsofen

Moscow Aviation Institute

编辑信件的主要联系方式.
Email: s.betsofen@gmail.com
俄罗斯联邦, Moscow, 125993

A. Ashmarin

Institute of Metallurgy and Material Sciences

Email: s.betsofen@gmail.com
俄罗斯联邦, Moscow, 119991

A. Lozovan

Moscow Aviation Institute

Email: s.betsofen@gmail.com
俄罗斯联邦, Moscow, 125993

B. Ryabenko

Scientific and Industrial Centre for Gas Turbine Technology “Saturn”

Email: s.betsofen@gmail.com
俄罗斯联邦, Moscow, 105118

A. Lutsenko

All Russian Research Institute of Aviation Materials

Email: s.betsofen@gmail.com
俄罗斯联邦, Moscow, 105118

A. Mamonov

Moscow Aviation Institute

Email: s.betsofen@gmail.com
俄罗斯联邦, Moscow, 125993

D. Molostov

Moscow Aviation Institute

Email: s.betsofen@gmail.com
俄罗斯联邦, Moscow, 125993

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