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  • Wiley  (4)
  • Zheng, Xuebin  (4)
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  • Wiley  (4)
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  • 1
    In: Journal of the American Ceramic Society, Wiley, Vol. 107, No. 1 ( 2024-01), p. 387-403
    Abstract: Yb 2 SiO 5 and Yb 2 Si 2 O 7 have been considered to be promising environmental barrier coatings (EBCs) materials for silicon‐based ceramics. Besides the various requirements EBCs must satisfy, it must be resistant to severe corrosion by high‐temperature water vapor as well as CMAS. In this work, the Yb 2 SiO 5 , Yb 2 Si 2 O 7 coatings and Yb 2 SiO 5 /Yb 2 Si 2 O 7 /Si, Yb 2 SiO 5 /Si EBCs were subjected to steam with alumina at 1400°C for 200 h. Results showed that Yb 3 Al 5 O 12 reaction layer and Yb 2 SiO 5 corrosion layer were formed on the Yb2SiO5 coating, while porous Yb 2 SiO 5 corrosion layer with Yb 3 Al 5 O 12 phase was formed on the Yb 2 Si 2 O 7 coating. By designing Yb 2 Si 2 O 7 as intermediate layer, the corrosion resistance of Yb 2 SiO 5 /Yb 2 Si 2 O 7 /Si EBCs was significantly improved. In addition to phase transition of β‐cristobalite to α‐phase, crystallization of amorphous SiO 2 also caused volume change, inducing longitudinal cracks through the TGO layer, which may lead to the failure of EBCs.
    Type of Medium: Online Resource
    ISSN: 0002-7820 , 1551-2916
    URL: Issue
    RVK:
    Language: English
    Publisher: Wiley
    Publication Date: 2024
    detail.hit.zdb_id: 2008170-4
    detail.hit.zdb_id: 219232-9
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  • 2
    Online Resource
    Online Resource
    Wiley ; 2023
    In:  Journal of the American Ceramic Society Vol. 106, No. 4 ( 2023-04), p. 2515-2528
    In: Journal of the American Ceramic Society, Wiley, Vol. 106, No. 4 ( 2023-04), p. 2515-2528
    Abstract: With the increasing service temperature of aeroengines, the development of thermal/environmental barrier coatings (T/EBCs) has been considered to be a great challenge, which requires high‐temperature stability and excellent thermal and mechanical properties. In this work, high‐entropy design was adopted to change the crystal structure of rare‐earth monosilicates used for T/EBCs. The microstructure evolution, thermal and mechanical properties of the plasma‐sprayed (Lu 0.25 Yb 0.25 Er 0.25 Y 0.25 ) 2 SiO 5 and (Lu 0.2 Yb 0.2 Er 0.2 Ho 0.2 Y 0.2 ) 2 SiO 5 coatings before and after thermal aging at 1350°C for 50 h were investigated. Results showed that the as‐sprayed coatings exhibited dense structure with amorphous and decomposed phases. The change of microstructure like amorphous crystallized and defect healing occurred after thermal aging, which had obvious influence on thermomechanical properties. Compared with single‐component RE 2 SiO 5 (RE = Yb, Er, Y) coatings, the thermal‐aged high‐entropy coatings exhibited lower thermal conductivity, similar thermal expansion coefficient, and better toughness. The work will provide a foundation for the design and application of T/EBCs materials.
    Type of Medium: Online Resource
    ISSN: 0002-7820 , 1551-2916
    URL: Issue
    RVK:
    Language: English
    Publisher: Wiley
    Publication Date: 2023
    detail.hit.zdb_id: 2008170-4
    detail.hit.zdb_id: 219232-9
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  • 3
    Online Resource
    Online Resource
    Wiley ; 2018
    In:  Journal of the American Ceramic Society Vol. 101, No. 10 ( 2018-10), p. 4743-4752
    In: Journal of the American Ceramic Society, Wiley, Vol. 101, No. 10 ( 2018-10), p. 4743-4752
    Abstract: A new tri‐layer Yb 2 SiO 5 /Yb 2 Si 2 O 7 /Si coating was fabricated on SiC, C/SiC, and SiC/SiC substrates, respectively, using atmospheric plasma spray (APS) technique. All coated samples were subjected to thermal shock test at 1350°C. The evolution of phase composition and microstructure and thermo‐mechanical properties of those samples before and after thermal shock test were characterized. Results showed that adhesion between all the 3 layers and substrates appeared good. After thermal shock tests, through microcracks which penetrated the Yb 2 SiO 5 top layer were mostly halted at the Yb 2 SiO 5 ‐Yb 2 Si 2 O 7 interface and no thermal growth oxide (TGO) was formed after 40‐50 quenching cycles, implying the excellent crack propagation resistance of the environmental barrier coating (EBC) system. Transmission electron microscopy analysis confirmed that twinnings and dislocations were the main mechanisms of plastic deformation of the Yb 2 Si 2 O 7 coating, which might have positive effects on crack propagation resistance. The thermal shock behaviors were clarified based on thermal stresses combined with thermal expansion behaviors and elastic modulus analysis. This study provides a strategy for designing EBC systems with excellent crack propagation resistance.
    Type of Medium: Online Resource
    ISSN: 0002-7820 , 1551-2916
    URL: Issue
    RVK:
    Language: English
    Publisher: Wiley
    Publication Date: 2018
    detail.hit.zdb_id: 2008170-4
    detail.hit.zdb_id: 219232-9
    Location Call Number Limitation Availability
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  • 4
    Online Resource
    Online Resource
    Wiley ; 2017
    In:  Journal of the American Ceramic Society Vol. 100, No. 5 ( 2017-05), p. 1896-1906
    In: Journal of the American Ceramic Society, Wiley, Vol. 100, No. 5 ( 2017-05), p. 1896-1906
    Abstract: Rare‐earth monosilicates (RE 2 SiO 5 , RE: rare‐earth elements), such as Yb 2 SiO 5 , have been developed for potential application as environmental barrier coating (EBC) materials. Yb 2 SiO 5 coating would experience microstructure evolution under high‐temperature environment and accordingly its thermomechanical properties would be altered. In this study, Yb 2 SiO 5 coating was fabricated by atmospheric plasma spray technique. The phase stability and microstructure change before and after thermal aging at 1300°C, 1400°C, and 1500°C were investigated. The changes in mechanical and thermal properties were characterized. The results showed that the as‐sprayed coating was mainly composed of Yb 2 SiO 5 with a small amount of Yb 2 O 3 and amorphous phase. Defects in the coating, including interfaces, pores, and microcracks, were greatly reduced with grain growth after thermal treatment. Thermal aging significantly modified the thermal and mechanical properties of the coating. The average CTE was increased by 13.1%, and the hardness and elastic modulus was increased by 42.4% and 49.4%, respectively, after thermal aging at 1500°C for 50 hour. The thermal conductivity of thermal‐aged coating was much higher than that of the as‐sprayed coating, which was still less than 2 W/(m·K). The influence of coating microstructure on the properties was analyzed and related to the failure mechanism of EBCs.
    Type of Medium: Online Resource
    ISSN: 0002-7820 , 1551-2916
    URL: Issue
    RVK:
    Language: English
    Publisher: Wiley
    Publication Date: 2017
    detail.hit.zdb_id: 2008170-4
    detail.hit.zdb_id: 219232-9
    Location Call Number Limitation Availability
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