journal article·2018-11

Residual thermal stresses prediction for CVD coating/substrate system based on a numerical model

Yang Wang, Zhaofeng Chen, Ning Pan, Binbin Li, Shengjie Yu, Sheng Cui

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Abstract

Abstract For a chemical vapor deposition (CVD) coating/substrate system, an improved and optimized numerical model is established to predict the residual thermal stresses. This model takes into account both the normal and bending strains and is developed based on the concept of a misfit strain between coating and substrate. Comparisons are presented between predictions from this model and from finite element analysis. The effects of coating thickness, elastic modulus, temperature difference, and multiple deposition on the residual stresses in the coating/substrate system have also been analyzed in detail. Furthermore, some confirmatory CVD SiC experiments with different layers have also been conducted according to the analysis model. The predictions that the multiple deposition system can relieve the residual thermal stresses and reduce the microcracks in the outermost coating effectively, are consistent with the numerical model.
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Research context

OpenAlex topics: Metal and Thin Film Mechanics · Silicon Carbide Semiconductor Technologies · Diamond and Carbon-based Materials Research

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Jiangsu Collaborative Innovation Center for Advanced Inorganic Function Composites Nanjing University of Aeronautics and Astronautics Nanjing People's Republic of China

Suzhou Superlong Aviation Heat Resistance Material Technology Co., Ltd Suzhou P.R. China

Fiber & Polymer Science, Biological & Agricultural Engineering University of California Davis California

Jiangsu Collaborative Innovation Center for Advanced Inorganic Function Composites College of Materials Science and Engineer Nanjing Tech University Nanjing China

Funding

Aeronautical Science Foundation of China · National Natural Science Foundation of China

References (23)

Show source-provided references
1. 10.1016/j.jeurceramsoc.2016.05.05110.1016/j.jeurceramsoc.2016.05.051 ↗
2. 10.1016/j.jeurceramsoc.2013.12.01210.1016/j.jeurceramsoc.2013.12.012 ↗
3. 10.1016/j.jeurceramsoc.2016.07.02810.1016/j.jeurceramsoc.2016.07.028 ↗
4. 10.1111/ijac.1266210.1111/ijac.12662 ↗
5. 10.1016/j.jmrt.2015.10.00410.1016/j.jmrt.2015.10.004 ↗
6. 10.1016/j.surfcoat.2017.03.01910.1016/j.surfcoat.2017.03.019 ↗
7. 10.1111/ijac.1252610.1111/ijac.12526 ↗
8. 10.1115/1.403265510.1115/1.4032655 ↗
9. 10.1177/00219983690030020610.1177/002199836900300206 ↗
10. 10.1115/1.317182710.1115/1.3171827 ↗
11. 10.1016/S0040-6090(97)00199-510.1016/S0040-6090(97)00199-5 ↗
12. 10.1016/j.tsf.2005.04.02710.1016/j.tsf.2005.04.027 ↗
13. 10.1016/j.surfcoat.2016.02.02810.1016/j.surfcoat.2016.02.028 ↗
14. 10.1016/j.jeurceramsoc.2015.12.03810.1016/j.jeurceramsoc.2015.12.038 ↗
15. 10.1016/j.tsf.2005.07.23610.1016/j.tsf.2005.07.236 ↗
16. 10.1016/j.compstruct.2012.11.01910.1016/j.compstruct.2012.11.019 ↗
17. 10.1016/j.compositesa.2008.07.00910.1016/j.compositesa.2008.07.009 ↗
18. 10.1016/j.scriptamat.2008.07.01010.1016/j.scriptamat.2008.07.010 ↗
19. 10.1063/1.131377610.1063/1.1313776 ↗
20. 10.1063/1.203927710.1063/1.2039277 ↗
21. 10.1007/BF0111570110.1007/BF01115701 ↗
22. HansonJR HauserJL KilfeatherJF HendriksHB HansonJR.Multi‐layer metal core circuit board laminate with a controlled thermal coefficient of expansion. US US 4496793 A[P].1985.
23. EndrinoJ DerflingerV GeyC.Highly oxidation resistant hard coating materials for cutting tools. EP EP1771602[P].2011.