Finite element analysis of thermal stress in Cu2O coating synthesized on Cu substrate

• Autorzy: Shorinov O.

Identyfikatory

DOI

10.5604/01.3001.0016.0753

• Języki publikacji: EN

Abstrakty

EN

Purpose: The paper aims to find the magnitude and nature of thermal residual stresses that occur during cooling of a copper sample with a thermally synthesized oxide layer of Cu2O. Design/methodology/approach: Thermo-mechanical analysis was performed by the finite element method using Ansys Software. The results of thermal analysis were used to study the resulting stress-strain state of the thin film/coating system after cooling. Findings: Based on the modeling results, the paper determined the most stress-strain areas of the sample with a coating, which are the free edges of the interfaces between the copper substrate and the Cu2O oxide layer. Research limitations/implications: The main limitations of the study are the use of certain simplifications in the condition setup, for instance, uniform cooling of the thin film/coating system, homogeneity and isotropy of substrate and thin film materials, invariance of their properties with temperature changes, etc. Practical implications: The results obtained can be used to control the stress-strain state of the thin film/coating system and prevent deformations and destruction of thin-film structures during their production and operation of products with them. Originality/value: The study of new promising methods for the formation of oxide nanostructures, for instance in a plasma environment, requires a sufficient theoretical basis in addressing the origin and development of stresses.

Słowa kluczowe

EN

stress-strain state; residual stress; oxide layers; thermo-mechanical modelling; coefficient of thermal expansion

PL

stan naprężenie-odkształcenie; naprężenie szczątkowe; warstwy tlenkowe; modelowanie termomechaniczne; współczynnik rozszerzalności cieplnej

• Wydawca: International OCSCO World Press
• Czasopismo: Archives of Materials Science and Engineering
• Rocznik: 2022
• Tom: Vol. 115, nr 2
• Strony: 58--65
• Opis fizyczny: Bibliogr. 27 poz.

Twórcy

autor

Shorinov O.

• Department of Aircraft Engines Manufacturing Technologies, Faculty of Aircraft Engines, National Aerospace University «Kharkiv Aviation Institute», Kharkiv, 61070, Ukraine

• https://orcid.org/0000-0002-5057-6679

Bibliografia

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Uwagi

PL

Opracowanie rekordu ze środków MEiN, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2022-2023).