表面硅化对C／C复合材料组织结构的影响

采用表面固相渗硅工艺在Ｃ／Ｃ复合材料表面制备ＳｉＣ涂层,研究了制备工艺对涂层和Ｃ／Ｃ复合材料组织结构的影响。经瓜时间对Ｃ／Ｃ复合材料的ＳｉＣ涂层厚度影响不大;Ｃ／Ｃ复合材料组织中热解碳基体与碳纤维相比,更易与Ｓｉ反应生成ＳｉＣ说明碳纤维的稳定性热解碳,Ｓｉ通过界面和材料缺陷扩散深入基体内部。     

退火条件对超低碳2.3%Si-1.7%Mn钢二次再结晶行为的影响

退火条件对超低碳２．３％Ｓｉ－１．７％Ｍｎ钢二次再结晶行为的影响用０．００３６％Ｃ－２．３％Ｓｉ－１．７％Ｍｎ－０．０１５％Ａｌ－０．００４２％Ｎ、２．３ｍｍ厚的热轧板制作试样。试样酸洗后,在氩气中以４０℃／ｈ升温,并于６００～７５０℃保温１ｈ,随后...     

雾化沉积SiCp／2014复合材料的时效

研究了雾化沉积ＳｉＣｐ／２０１４复合材料的和行为，。结果表明，在ＳｉＣｐ／２０１４的时效过程中，峰值时效的主要强化相为β相（Ｍｇ２Ｓｉ），其最佳的时效工艺为５０２℃固溶４０ｍｉｎ，１７０℃时效４．５ｈ。     

热处理对C／C复合材料Mo-Si-N系涂层抗氧化性能的影响

以Mo粉和Si粉为原料，采用熔浆法在氮气环境中制备了C／C复合材料的Mo．Si—N系抗氧化涂层，并对涂层1400℃预氧化热处理前后的组织结构和氧化行为进行了研究。结果表明，Mo．Si—N涂层除具有与Mo．Si系涂层相同的SiC底层和MoSi2／Si主结构层外，还形成了厚度不均匀的Si3N4／SiC／Si表面层。Mo-Si—N系涂层具有1400℃稳定抗氧化能力和1450℃长时间氧化防护潜力；经1400℃预氧化热处理后，涂层的最高抗氧化温度达到了1500℃，氧化12小时后重量损失率小于1wt％。     

Al_2O_3／TiB_2和Al_2O_3／TiB_2／SiC_W陶瓷复合材料在

研究了热压烧结工艺制备的Ａｌ２Ｏ３／ＴｉＢ２和Ａｌ２Ｏ３／ＴｉＢ２／ＳｉＣＷ陶瓷复合材料在１３００℃的氧化行为用ＸＲＤ、ＳＥＭ、ＴＥＭ／ＥＤＳＡ分析了材料氧化后的相组成及显微结构．结果表明：两种材料在１３００℃空气中氧化３０ｈ内的氧化增重符合抛物线规律，ＳｉＣ晶须的加入可明显改善Ａｌ２Ｏ３／ＴｉＢ２材料的高温抗氧化性．     

Ni对C－B_4C－SiC复合材料显微结构与性能的影响

本文研究了烧结助剂Ｎｉ对Ｃ－Ｂ_４Ｃ－ＳｉＣ复合材料显微结构与性能的影响．Ｘ射线衍射表明Ｎｉ在烧结温度下与ＳｉＣ，Ｂ_４Ｃ人发生反应在晶界生成Ｎｉ_（４．６）Ｓｉ_２Ｂ，并产生液相，有效地促进了Ｃ－Ｂ_４Ｃ－ＳｉＣ复合材料的烧结，抑制了晶粒的长大，使复合材料密度与强度大幅度地增加，电阻率下降；同时Ｎｉ_（４．６）Ｓｉ_２Ｂ在氧化时生成致密的２ＮｉＯ·Ｂ_２Ｏ_３，包裹了易氧化的Ｂ_４Ｃ和Ｃ，有效地防止了复合材料的氧化，从而大大提高了制品的抗氧化性能．     

Al2O3／TiB2／SiCw陶瓷材料的高温氧化行为

采用热压烧结工艺制备了Ａｌ２Ｏ３／ＴｉＢ２／ＳｉＣｗ陶瓷复合材料，研究了ＳｉＣ晶须含量对其高温氧化行煌影响。用ＸＲＤ，ＳＥＭ，ＴＥＭ／ＥＤＳ分析了材料氧化后的相组成及显向结构，探讨了该材料的氧化机理。结果表明：不同ＳｉＣｗ含量的Ａｌ２Ｏ３／ＴｉＢ２／ＳｉＣｗ陶瓷材料在１４００℃空气中氧化３０ｈ的氧化增重符合抛物线规律。     

Si3N4／SiC复合陶瓷粉末的研制

研究了添加晶种的碳热还原ＳｉＯ２法制取Ｓｉ３Ｎ４／ＳｉＣ复合粉末的工艺。发现反应温度的升高、反应时间的延长、原料ＳｉＯ２粉比表面的增大、添加Ｓｉ３Ｎ４晶种以及提高Ｎ２流速，均有利于Ｓｉ３Ｎ４、ＳｉＣ相含量的增加。当ＳｉＯ２：Ｃ为１：２，加入１０Ｗｔ％Ｓｉ３Ｎ４品种时，在１３５０℃下于Ｎ２流速为０．４ｍ３·ｈ－１气氛下反应４ｈ，可得到平均粒度为０．４６ｍ，含Ｎ２３．９ｗｔ％、Ｃ６．２５Ｗｔ％、Ｏ２．９０ｗｔ％的Ｓｉ３Ｎ４／ＳｉＣ超细复合粉末。     

原位SiC颗粒增强MoSi_2基复合材料的显微组织和力学性能

本文研究了原位 ＳｉＣ颗粒增强 ＭｏＳｉ２基复合材料的组织结构和力学性能。结果表明：复合材料的组织为ｔ－ＭｏＳｉ２基体上均匀分布 β－ＳｉＣ等轴颗粒,数量很少的球形小孔隙主要分布在 ＳｉＣ颗粒内, ＳｉＣ颗粒尺寸为 ２－５ μｍ．复合材料界面为直接的原子结合,无非晶层存在．复合材料的室温维氏硬度、断裂韧性、抗压强度及高温流变应力明显高于单一ＭｏＳｉ２,随着ＳｉＣ体积分数的增加,维氏硬度、断裂韧性及高温流变应力提高,而抗压强度先增加后减少． ＳｉＣ体积分数从 １０％增加到 ４５％,ＫＩＣ从 ４．３４提高到 ５．７１ ＭＰａ·ｍ１／２;与单一 ＭｏＳｉ２相比提高了 ２５％－４６％; １４００℃时,σ０．２从 ２０％ＳｉＣ的 ２３０提高到 ４５％ＳｉＣ的 ２８５ ＭＰａ,比单一 ＭｏＳｉ２提高了 ９８％－１４６％．     

Ni_3Al基合金的初期氧化速率

用感量为２μｇ的Ｓｅｔａｒａｍ热天平研究了Ｎｉ３Ａｌ及Ｎｉ３Ａｌ－Ｃｒ基合金７００℃～１１００℃的初期氧化行为。Ｎｉ３Ａｌ合金在中温区（７０００℃～９００℃）的氧化,随温度升高初期氧化速率明显增加（氧化５ｍｉｎ）,８００℃及９００℃氧化０．５ｈ后试样的氧化增重低于７００℃的。在温度低于９００℃时,Ｎｉ３Ａｌ－Ｃｒ基合金的氧化增重明显小于Ｎｉ３Ａｌ基合金;高于１０００℃时,其氧化增重明显大于Ｎｉ３Ａｌ基合金的。ＥＤＳ分析表明Ｎｉ３Ａｌ－Ｃｒ基合金表面不出现纯ＮｉＯ相的氧化物区。加Ｃｒ可降低Ｎｉ３Ａｌ的晶格常数,增加原子密堆度,从而阻碍Ｎｉ原子的扩散,降低合金的氧化速率。     

Double SiC coating on carbon/carbon composites against oxidation by a two-step method

To improve the oxidation resistance of C/C composites, a double SiC protective coating was prepared by a two-step technique. Firstly, the inner SiC layer was prepared by a pack cementation technique, and then an outer uniform and compact SiC coating was obtained by low pressure chemical vapor deposition. The microstructures and phase compositions of the coatings were characterized by SEM, EDS and XRD analyses. Oxidation behaviour of the SiC coated C/C composites was also investigated. It was found that the double SiC coating could protect C/C composites against oxidation at 1773 K in air for 178 h with a mass loss of 1.25%. The coated samples also underwent thermal shocks between 1773 K and room temperature 16 times. The mass loss of the coated C/C composites was only 2.74%. Double SiC layer structures were uniform and dense, and can suppress the generation of thermal stresses, facilitating an excellent anti-oxidation coating.     

SiC nanowire-toughened SiC-MoSi2-CrSi2 oxidation protective coating for carbon/carbon composites

To prevent carbon/carbon (C/C) composites from oxidation, a dense SiC nanowire-toughened SiC-MoSi₂-CrSi₂ multiphase coating was prepared by the two-step technique composed of chemical vapor deposition (CVD) and pack cementation. The coatings were characterized by scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS) and X-ray diffraction (XRD). SiC nanowires could decrease the dimension of cracks and improve the oxidation and thermal shock resistance of SiC-MoSi₂-CrSi₂ multiphase coating. Oxidation test shows that, after introducing SiC nanowires, the weight loss of the coated sample can be reduced from 1.06% to 0.64% after oxidation at 1773 K for 155 h and decreased from 6.92% to 3.42% after thermal cycling between 1773 K and room temperature for 30 times.     

Effect of Thermal Shock and Oxidation on Mechanical Property of Carbon/Carbon Composites with a Silicide Coating

A SiC whisker-toughened MoSi2-SiC-Si coating was prepared on carbon/carbon (C/C) composites surface by a two-step technique of slurry and pack cementation, and the effects of thermal shock and oxidation on the mechanical property of the coated C/C were studied. The flexural strength of C/C composites was improved by 6.8% after coated by SiC whisker-toughened MoSi2-SiC-Si. After thermal cycle between 1773 K and room temperature in air for 10 times, the mass loss of the coated sample was 5.08% and the percent...     

Preparation and oxidation resistance of B2O3-coated boron-modified carbon foams

To improve the oxidation resistance of boron-modified carbon foams, the B₂O₃ coating was prepared on boron-modified carbon foams by low-cost slurry method. The microstructures and phase compositions of the coated carbon foams were characterized by scanning electron microscopy and X-ray diffraction, respectively. Oxidation resistances of uncoated and coated boron-modified carbon foams were investigated at 873 K in air. The results showed that as-received B₂O₃ coating could protect boron-modified carbon foams from oxidation at 873 K. B₂O₃-coated carbon foam doped with 7% B₂O₃ (mass fraction) (BO-7) had better oxidation resistance, exhibiting mass loss of 17.40% after oxidation at 873 K for 120 min. The melting glass layer formed on the surface of BO-7 could prevent oxygen from diffusing into boron-modified carbon foams substrate during oxidation to some extent.     

C/SiC/Si-Mo-B/glass multilayer oxidation protective coating for carbon/carbon composites

To prevent carbon/carbon (C/C) composites from oxidation, a self-sealing multilayer oxidation resistant coating including a C/SiC gradient inner layer, a Si-Mo-B middle layer and a glass exterior layer was prepared by pack cementation and slurry method. Scanning electron microscopy and X-ray diffraction were used to analyze the microstructure and phase composition of the as-prepared coating. The isothermal and thermal shock oxidation resistance of the coating was also investigated. The results showed that the multilayer coating exhibited excellent oxidation resistance from room temperature to 1873 K. It could effectively protect C/C composites for 100 h at 1173 K and 150 h at 1873 K, and endure 40 thermal cycles between 1873 K and room temperature. The excellent oxidation and thermal shock resistance could be attributed to the gradient structure and the self-sealing property of the multilayer coating.     

Oxidation protection of C/SiC coated carbon/carbon composites with Si–Mo coating at high temperature

To protect carbon/carbon (C/C) composites against oxidation, a Si–Mo coating was prepared on C/SiC-coated C/C composites by a simple slurry method. The microstructure of the coating was characterized by X-ray diffraction, scanning electron microscopy and Raman spectra. Results showed that the coating was mainly composed of SiC, MoSi₂ and Si. It could protect C/C composites from oxidation at 1873 K in air for 300 h and withstand 13 thermal cycles between room temperature and 1873 K. The excellent oxidation and thermal shock resistance of the coating was attributed to the formation of dense SiO₂ glass at high temperature. The volatilization of MoO₃ and SiO₂ at 1873 K was the main reason of the weight loss of the coated C/C composites.     

SiC/SiC–YAG–YSZ oxidation protective coatings for carbon/carbon composites

SiC/SiC–YAG–YSZ coatings were prepared by pack cementation, chemical vapor deposition and slurry painting on carbon/carbon (C/C) composites. The microstructures and oxidation behavior of coatings were investigated. The results show that the coatings displayed good oxidation and thermal shock resistance due to a dense glassy layer with silicates formed on the coating of SiC–YAG–YSZ. The weight gain rate of coated C/C composites was 1.77% after oxidation for 150 h at 1773 K. SiC in outer coating can promote the formation of oxygen diffusion barrier and lead to the optimum oxidation resistance for the coatings, compared with YSZ and YAG.     

A ZrSiO4/SiC oxidation protective coating for carbon/carbon composites

In order to improve the oxidation resistance of carbon/carbon (C/C) composites, a ZrSiO₄ coating on SiC pre-coated C/C composites was prepared by a hydrothermal electrophoretic deposition process. Phase compositions and microstructures of the as-prepared ZrSiO₄/SiC coating were characterized by X-ray diffraction (XRD), scanning electron microscopy (SEM) and energy dispersive spectrometer (EDS). The anti-oxidation property and failure mechanism of the multi-layer coating were investigated. Results show that hydrothermal electrophoretic deposition is an effective route to prepare crack-free ZrSiO₄ outer coatings. The multi-layer coating obviously exhibits two-layer structure. The inner layer is composed of SiC phase and the outer layer is composed of ZrSiO₄ phase. The bonding strength between the outer layer coatings and C/C–SiC substrate are 30.38 MPa. The ZrSiO₄/SiC coating displays excellent oxidation resistance and can protect C/C composites from oxidation at 1773 K for 332 h with a mass loss rate of only 0.48 × 10^− 4 g/cm²·h. The mechanical properties of the specimens are 84.36 MPa before oxidation and 68.29 MPa after oxidation. The corresponding high temperature oxidation activation energy of the coated C/C composites at 1573–1773 K is calculated to be 119.8 kJ/mol. The oxidation process is predominantly controlled by the diffusion rate of oxygen through the ZrSiO₄/SiC multi-coating. The failure of the coating is due to the formation of penetrative holes between the SiC bonding layer and the C/C matrix at 1773 K.     

Anti-oxidation properties of ZrB2 modified silicon-based multilayer coating for carbon/carbon composites at high temperatures

To improve the anti-oxidation ability of silicon-based coating for carbon/carbon (C/C) composites at high temperatures, a ZrB₂ modified silicon-based multilayer oxidation protective coating was prepared by pack cementation. The phase composition, microstructure and oxidation resistance at 1773, 1873 and 1953 K in air were investigated. The prepared coating exhibits dense structure and good oxidation protective ability. Due to the formation of stable ZrSiO₄–SiO₂ compound, the coating can effectively protect C/C composites from oxidation at 1773 K for more than 550 h. The anti-oxidation performance decreases with the increase of oxidation temperature. The mass loss of coated sample is 2.44% after oxidation at 1953 K for 50 h, which is attributed to the decomposition of ZrSiO₄ and the volatilization of SiO₂ protection layer.     

The oxidation behavior and mechanical properties of MoSi2–CrSi2–SiC–Si coated carbon/carbon composites in high-temperature oxidizing atmosphere

A MoSi₂–CrSi₂–SiC–Si multi-component coating was prepared on the surface of carbon/carbon (C/C) composites by a two-step pack cementation method. The microstructure, oxidation behavior and mechanical properties of the coating were studied. These results show that the multi-component coating could protect the C/C composites from oxidation in air at 1873 K for 300 h and withstand 30 thermal cycles between 1873 K and room temperature, respectively. The mass loss and mechanical property loss of the coated C/C composites are considered due to the worse fluidity of SiO₂ at intermediate temperatures and the thermal mismatch between the coating and C/C composites.