ICCM21(6)fullpaperFormatted.pdf (298.67 kB)
Download fileThe mechanics of interface fracture in layered composite materials: (6) spallation of thermal barrier coatings of turbine blades
conference contribution
posted on 2017-06-23, 14:36 authored by Bo Yuan, Christopher HarveyChristopher Harvey, Rachel ThomsonRachel Thomson, Gary CritchlowGary Critchlow, Simon WangSimon WangIt is consensus that local spallation failures in thermal barrier coatings (TBCs) are determined synergistically by many factors. The present experimental test results confirm a completely new spallation failure mechanism for the electron beam-physical vapour deposited (EB-PVD) TBCs on
engine turbine blades, which is hypothesized in the latest work [1, 2] for the study of thin film spallation. That is, the spallation is driven by pockets of energy concentration (PEC). This paper reports the experimental study.
History
School
- Aeronautical, Automotive, Chemical and Materials Engineering
Department
- Aeronautical and Automotive Engineering
Published in
21st International Conference on Composite MaterialsCitation
YUAN, B. ... et al, 2017. The mechanics of interface fracture in layered composite materials: (6) spallation of thermal barrier coatings of turbine blades. 21st International Conference on Composite Materials (ICCM-21), Xi'an, China, 20th-25th August 2017.Publisher
Chinese Society for Composite MaterialsVersion
- AM (Accepted Manuscript)
Publisher statement
This work is made available according to the conditions of the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) licence. Full details of this licence are available at: https://creativecommons.org/licenses/by-nc-nd/4.0/Acceptance date
2017-04-20Publication date
2017Notes
This is a conference paper.Publisher version
Language
- en
