Design of hard coating architecture for the optimization of erosion resistance

Hassani, Salim; Klemberg-Sapieha, J.E.; Bielawski, Mariusz; Bereś, W.; Martinů, L.; Balazinski, Marek

doi:10.1016/j.wear.2008.01.021

Cited by 66 publications

(44 citation statements)

References 28 publications

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“…Similar depths of penetration were also found by finite element modeling for a TiN coating on SS410 by Hassani et al [136]. …”

Section: A33 Vickers Micro-hardnesssupporting

confidence: 85%

“…In fact, Hassani et al [30] have shown by FEM simulation, that coatings with thicknesses below a critical value (8 µm for TiN on a stainless steel substrate) will exhibit enhanced erosion. They also predicted increasing maximum tensile stresses during impact with increasing substrate Young's Modulus [136].…”

Section: Spe Behaviormentioning

confidence: 92%

“…In fact, Hassani et al [135,136] showed by modeling different multilayer configurations by FEM that it was possible to reduce maximum tensile stresses during impact through load spreading and thus increase the velocity threshold at which cracking begins. However, their study was limited to small spherical particles and their proposed guidelines for improved performance cannot be generalized since it has been…”

Section: Spe Of Multilayer Coatingsmentioning

confidence: 99%

See 2 more Smart Citations

Solid particle erosion mechanisms of protective coatings for aerospace applications

Bousser

Martinů

Klemberg-Sapieha

2014

Surface and Coatings Technology

Self Cite

136

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“…Similar depths of penetration were also found by finite element modeling for a TiN coating on SS410 by Hassani et al [136]. …”

Section: A33 Vickers Micro-hardnesssupporting

confidence: 85%

Section: Spe Behaviormentioning

confidence: 92%

Section: Spe Of Multilayer Coatingsmentioning

confidence: 99%

See 1 more Smart Citation

Solid particle erosion mechanisms of protective coatings for aerospace applications

Bousser

Martinů

Klemberg-Sapieha

2014

Surface and Coatings Technology

Self Cite

136

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“…Hence, coating of metal components for improvement in engine lifetime as well as stable behavior of engines during operation is found to be a possible solution against erosion [4]. The use of single layer nitride coatings (TiN) has been a famous method for protection against erosion due to their high hardness [5,6]. In contrast, TiAlN coatings with comparatively higher hardness have been devised as a better alternative to TiN coatings [7,8].…”

Section: Introductionmentioning

confidence: 99%

Investigation of the Wear Resistance Properties of Cr/CrN Multilayer Coatings against Sand Erosion

Naveed

Obrosov

Weiß

2015

Conference Papers in Science

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The wear of metallic components used in gas and steam turbines due to erosive sand particles leads to a tremendous decrease in their lifetime. This wear can be reduced by the use of suitable erosion resistant coatings resulting in lower maintenance costs. In this context, multilayer Cr/CrN PVD coatings using an industrial coater were designed and applied on Inconel 718, a material which finds its application in gas turbines. A variation in the bimodal period has been induced in order to achieve an optimal coating architecture providing optimum properties needed for the erosion resistant coatings. The coating was deposited using a single Crtarget with an induction of N 2 during the nitriding phase at a temperature of 480-500 ∘ C and the coating thickness of 24-26 m was kept constant throughout. The erosion tests were conducted at angles of 30 ∘ , 60 ∘ , and 90 ∘ . The sand used for the test is an irregular shaped SiO 2 . The erosion tests were followed by a detailed microscopic examination of the eroded coating structure in combination with nanoindentation and scratch tests.

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“…This is very serious problem in gas turbines, pumps, thermal exchangers, and blades of helicopters, which causes premature failure and decreases service life of components [3][4][5][6][7]. There are three different ways to solve this issue; first, using of filtering systems to screen erodent particles for compressor of aircraft gas turbine engine.…”

Section: Introductionmentioning

confidence: 99%

Simulation of Erosion by Particle Impact on a Rough Surface

Anaraki

Kadkhodapour

Taherkhani

2014

J Fail. Anal. and Preven.

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In many industrial conditions, we deal with impact of particles on a surface that can cause premature failure. A series of studies have been conducted to investigate the effect of parameters on this phenomenon on smooth surfaces at micron-scale. But there is no ideally smooth surface at this micron level. Our study investigated the effect of particle parameters on erosion rate on rough surfaces and obtained their diagram in terms of erosion rate. The modeled particle velocity was in a range between 25 and 150 m/s, and particle diameter is in a range between 216 and 1080 lm. In our numerical study, an erosion model that is based on the impact of a single particle on a small area of surface was described. Then, in our experimental study, different zones that are created due to multiple particle impact on large area of surface were identified.

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Design of hard coating architecture for the optimization of erosion resistance

Cited by 66 publications

References 28 publications

Solid particle erosion mechanisms of protective coatings for aerospace applications

Solid particle erosion mechanisms of protective coatings for aerospace applications

Investigation of the Wear Resistance Properties of Cr/CrN Multilayer Coatings against Sand Erosion

Simulation of Erosion by Particle Impact on a Rough Surface

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