2014
DOI: 10.1007/s11666-014-0185-z
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Residual Stress Analysis of Laser-Drilled Thermal Barrier Coatings Involving Various Bond Coats

Abstract: International audienceThe gas turbine combustion chamber of aero-engines requires a thermal barrier coating (TBC) by thermal spraying. Further heat protection is achieved by laser drilling of cooling holes. The residual stresses play an important role in the mechanical behaviour of TBC. It could also affect the TBC response to delamination during laser drilling. In this work, studies of the cracking behaviour after laser drilling and residual stress distribution have been achieved for different bond coats by p… Show more

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Cited by 4 publications
(3 citation statements)
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“…Once i G reaches its critical value ( ic G ), multilayer delamination may occur in the top-coat [16]. Furthermore, in order to prevent the overheating of the component and to realize further heat protection, numerous cooling holes are drilled throughout the chamber wall [17][18][19]. These holes enable a protective air film to flow from the external side into the internal face of the TBC-coated chamber.…”
Section: Introductionmentioning
confidence: 99%
“…Once i G reaches its critical value ( ic G ), multilayer delamination may occur in the top-coat [16]. Furthermore, in order to prevent the overheating of the component and to realize further heat protection, numerous cooling holes are drilled throughout the chamber wall [17][18][19]. These holes enable a protective air film to flow from the external side into the internal face of the TBC-coated chamber.…”
Section: Introductionmentioning
confidence: 99%
“…The coated material is a thermal-refractory ceramic with a thickness around 200μm. The presence of this coated before the drilling operation induces several defaults such as a macro delamination of the coatings [12] [15]. The holes are more or less inclined (up to 20 • from surface) and are millimetric.…”
Section: Introductionmentioning
confidence: 99%
“…When the ablation area ratio is greater than the critical value, the strength of the material decreased rapidly. During laser ablation, two forms of residual stress are generated: one is that higher power causes material evaporation and the formation of plasma, which generates a stress wave that propagates into the material causing compressive residual stress [18]; and the other is that thermal residual stresses are generated in the heat affected zone due to differences in cooling rates and shrinkage rates between the surface and the inner region. For nanosecond-laser drilling, both residual stresses exist, whereas for millisecond lasers, thermal residual stress is the dominant residual stress around the hole.…”
Section: Yield Strengthmentioning
confidence: 99%