A. N. Astapov, B. E. Zhestkov, I. V. Sukmanov, V. S. Terentieva
{"title":"ZrSi2-MoSi2-ZrB2-ZrC涂层在高速高焓空气等离子体流中抗氧化和烧蚀性能的提高","authors":"A. N. Astapov, B. E. Zhestkov, I. V. Sukmanov, V. S. Terentieva","doi":"10.1134/S0036029524701180","DOIUrl":null,"url":null,"abstract":"<p>The previously considered composition of the powder mixture in the ZrSi<sub>2</sub>–MoSi<sub>2</sub>–ZrB<sub>2</sub>–Si system is corrected toward decreasing the content of the relatively low-melting phases ZrSi<sub>2</sub> and MoSi<sub>2</sub> and increasing the fraction of the refractory phase ZrB<sub>2</sub>. A heat-resistant coating is formed on the C/C–SiC composite by the firing facing of the powder mixture at 1750°C under an argon expansion pressure of 150–200 Pa. The phase composition of the coating includes (mol %): 23.2 ZrSi<sub>2</sub>, 16.8 MoSi<sub>2</sub>, 46.0 ZrB<sub>2</sub>, and 14.0 ZrC. The synthesis of the secondary phase ZrC is carried out in situ by the reaction in the ZrSi<sub>2</sub>–C system. Oxidation and ablation resistance tests are carried out under flow at surface and surface heating conditions in a <i>T</i><sub>w</sub> temperature range of 1300–2350°C with an air plasma flow at a speed of 4.7–4.8 km/s and a stagnation enthalpy of 48–50 MJ/kg. The performed correction of the composition is shown to provide an enhancement of the protective ability of the coating at <i>T</i><sub>w</sub> = 2200°C by 2.5 times (up to 170 s), as well as an increase in the maximum permissible level of working temperatures from <i>T</i><sub>w</sub> = 2200 to 2350°C. At the same time, the average values of the specific mass loss and mass removal rate of the coating decrease by 23 and 14% and amount to 3.9 mg/cm<sup>2</sup> and 13.1 mg cm<sup>–2</sup> h<sup>–1</sup>, respectively. The rate constants of heterogeneous recombination of air plasma atoms and ions on the coating surface are estimated: <i>K</i><sub>w</sub> = 2 ± 1, 5 ± 2, 9 ± 3, 14 ± 3, and 19 ± 2 m/s at <i>T</i><sub>w</sub> = 1300–1450, 1500–1750, 1800–1950, 2000–2150, and 2200–2350°C, respectively. The spectral emissivity of the coating ε<sub>λ</sub> is found to decrease from 0.69 ± 0.02 in the initial state to 0.41 ± 0.02 after the fire tests in the wavelength range λ = 600–900 nm at room temperature. The main factors limiting the protection effect resource of the coating are shown to be the through oxidation of the ZrSi<sub>2</sub> matrix and evaporation of the zirconium-modified borosilicate glass leading to an increase in the fraction of the ZrO<sub>2</sub> phase with high anionic conductivity and catalytic activity in the oxide film.</p>","PeriodicalId":769,"journal":{"name":"Russian Metallurgy (Metally)","volume":"2024 3","pages":"727 - 733"},"PeriodicalIF":0.3000,"publicationDate":"2025-01-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Improvement of the Resistance of the ZrSi2–MoSi2–ZrB2–ZrC Coating to Oxidation and Ablation in a High-Speed High-Enthalpy Air Plasma Flow\",\"authors\":\"A. N. Astapov, B. E. Zhestkov, I. V. Sukmanov, V. S. Terentieva\",\"doi\":\"10.1134/S0036029524701180\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<p>The previously considered composition of the powder mixture in the ZrSi<sub>2</sub>–MoSi<sub>2</sub>–ZrB<sub>2</sub>–Si system is corrected toward decreasing the content of the relatively low-melting phases ZrSi<sub>2</sub> and MoSi<sub>2</sub> and increasing the fraction of the refractory phase ZrB<sub>2</sub>. A heat-resistant coating is formed on the C/C–SiC composite by the firing facing of the powder mixture at 1750°C under an argon expansion pressure of 150–200 Pa. The phase composition of the coating includes (mol %): 23.2 ZrSi<sub>2</sub>, 16.8 MoSi<sub>2</sub>, 46.0 ZrB<sub>2</sub>, and 14.0 ZrC. The synthesis of the secondary phase ZrC is carried out in situ by the reaction in the ZrSi<sub>2</sub>–C system. Oxidation and ablation resistance tests are carried out under flow at surface and surface heating conditions in a <i>T</i><sub>w</sub> temperature range of 1300–2350°C with an air plasma flow at a speed of 4.7–4.8 km/s and a stagnation enthalpy of 48–50 MJ/kg. The performed correction of the composition is shown to provide an enhancement of the protective ability of the coating at <i>T</i><sub>w</sub> = 2200°C by 2.5 times (up to 170 s), as well as an increase in the maximum permissible level of working temperatures from <i>T</i><sub>w</sub> = 2200 to 2350°C. At the same time, the average values of the specific mass loss and mass removal rate of the coating decrease by 23 and 14% and amount to 3.9 mg/cm<sup>2</sup> and 13.1 mg cm<sup>–2</sup> h<sup>–1</sup>, respectively. The rate constants of heterogeneous recombination of air plasma atoms and ions on the coating surface are estimated: <i>K</i><sub>w</sub> = 2 ± 1, 5 ± 2, 9 ± 3, 14 ± 3, and 19 ± 2 m/s at <i>T</i><sub>w</sub> = 1300–1450, 1500–1750, 1800–1950, 2000–2150, and 2200–2350°C, respectively. The spectral emissivity of the coating ε<sub>λ</sub> is found to decrease from 0.69 ± 0.02 in the initial state to 0.41 ± 0.02 after the fire tests in the wavelength range λ = 600–900 nm at room temperature. The main factors limiting the protection effect resource of the coating are shown to be the through oxidation of the ZrSi<sub>2</sub> matrix and evaporation of the zirconium-modified borosilicate glass leading to an increase in the fraction of the ZrO<sub>2</sub> phase with high anionic conductivity and catalytic activity in the oxide film.</p>\",\"PeriodicalId\":769,\"journal\":{\"name\":\"Russian Metallurgy (Metally)\",\"volume\":\"2024 3\",\"pages\":\"727 - 733\"},\"PeriodicalIF\":0.3000,\"publicationDate\":\"2025-01-08\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Russian Metallurgy (Metally)\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://link.springer.com/article/10.1134/S0036029524701180\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q4\",\"JCRName\":\"METALLURGY & METALLURGICAL ENGINEERING\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Russian Metallurgy (Metally)","FirstCategoryId":"5","ListUrlMain":"https://link.springer.com/article/10.1134/S0036029524701180","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"METALLURGY & METALLURGICAL ENGINEERING","Score":null,"Total":0}
Improvement of the Resistance of the ZrSi2–MoSi2–ZrB2–ZrC Coating to Oxidation and Ablation in a High-Speed High-Enthalpy Air Plasma Flow
The previously considered composition of the powder mixture in the ZrSi2–MoSi2–ZrB2–Si system is corrected toward decreasing the content of the relatively low-melting phases ZrSi2 and MoSi2 and increasing the fraction of the refractory phase ZrB2. A heat-resistant coating is formed on the C/C–SiC composite by the firing facing of the powder mixture at 1750°C under an argon expansion pressure of 150–200 Pa. The phase composition of the coating includes (mol %): 23.2 ZrSi2, 16.8 MoSi2, 46.0 ZrB2, and 14.0 ZrC. The synthesis of the secondary phase ZrC is carried out in situ by the reaction in the ZrSi2–C system. Oxidation and ablation resistance tests are carried out under flow at surface and surface heating conditions in a Tw temperature range of 1300–2350°C with an air plasma flow at a speed of 4.7–4.8 km/s and a stagnation enthalpy of 48–50 MJ/kg. The performed correction of the composition is shown to provide an enhancement of the protective ability of the coating at Tw = 2200°C by 2.5 times (up to 170 s), as well as an increase in the maximum permissible level of working temperatures from Tw = 2200 to 2350°C. At the same time, the average values of the specific mass loss and mass removal rate of the coating decrease by 23 and 14% and amount to 3.9 mg/cm2 and 13.1 mg cm–2 h–1, respectively. The rate constants of heterogeneous recombination of air plasma atoms and ions on the coating surface are estimated: Kw = 2 ± 1, 5 ± 2, 9 ± 3, 14 ± 3, and 19 ± 2 m/s at Tw = 1300–1450, 1500–1750, 1800–1950, 2000–2150, and 2200–2350°C, respectively. The spectral emissivity of the coating ελ is found to decrease from 0.69 ± 0.02 in the initial state to 0.41 ± 0.02 after the fire tests in the wavelength range λ = 600–900 nm at room temperature. The main factors limiting the protection effect resource of the coating are shown to be the through oxidation of the ZrSi2 matrix and evaporation of the zirconium-modified borosilicate glass leading to an increase in the fraction of the ZrO2 phase with high anionic conductivity and catalytic activity in the oxide film.
期刊介绍:
Russian Metallurgy (Metally) publishes results of original experimental and theoretical research in the form of reviews and regular articles devoted to topical problems of metallurgy, physical metallurgy, and treatment of ferrous, nonferrous, rare, and other metals and alloys, intermetallic compounds, and metallic composite materials. The journal focuses on physicochemical properties of metallurgical materials (ores, slags, matters, and melts of metals and alloys); physicochemical processes (thermodynamics and kinetics of pyrometallurgical, hydrometallurgical, electrochemical, and other processes); theoretical metallurgy; metal forming; thermoplastic and thermochemical treatment; computation and experimental determination of phase diagrams and thermokinetic diagrams; mechanisms and kinetics of phase transitions in metallic materials; relations between the chemical composition, phase and structural states of materials and their physicochemical and service properties; interaction between metallic materials and external media; and effects of radiation on these materials.