SiC-Si-ZrSiO_4 Multiphase Oxidation Protective Coating for Carbon/Carbon Composites

In order to improve the anti-oxidation property of carbon/carbon （C/C） composites, a novel SiC-Si-ZrSiO4 multiphase oxidation protective coating was produced on the surface of C/SiC coated carbon/carbon compo ites by a pack cementation technique. The phase composition and microstructure of the as-prepared coatings were characterized by XRD （X-ray diffraction）, SEM （scanning electron microscopy） and EDS （energy dispersive spectroscopy）. Oxidation behavior of the multiphase coated C/C composites was also investigated. It showed that the as-prepared coating characterized by excellent oxidation resistance and thermal shock re- sistance could effectively protect C/C composites from oxidation at 1773 K for 57 h in air and endure the thermal cycle between 1773 K and room temperature for 12 times, whereas the corresponding weight loss is only 1.47%. The excellent oxidation protective ability of the SiC-Si-ZrSiO4 coating could be attributed to the C/SiC gradient inner layer and the multiphase microstructure of the coating.     

Oxidation Protective C/SiC/Si-SiC Multilayer Coating for Carbon/Carbon Composites Applying at 1873 K

A C/SiC/Si-SiC multilayer coating for protecting carbon/carbon(C/C) composites against oxidation was prepared by slurry and pack cementation.X-ray diffraction(XRD) and energy dispersive spectroscopy(EDS) analysis showed that the inner coating obtained from the slurry and pack cementation was a C/SiC gradient layer acting as bonding layer,and the exterior coating formed in the second pack cementation was a Si-SiC double phase coating.Oxidation tests at 1873 K in air showed that the coating exhibited excellen...     

Oxidation and Mechanical Properties of SiC/SiC-MoSi2-ZrBa Coating for Carbon/Carbon Composites

To improve oxidation resistance of carbon/carbon （C/C） composites, a SiC/SiC-MoSi2-ZrB2 double-layer ceramic coating was prepared on C/C composites by two-step pack cementation. The phase compositions and microstructures of as-prepared multilayer coating were characterized by X-ray diffraction and scanning electron microscopy. The oxidation resistance at 1773 K and the effect of thermal shock between 1773 K and room temperature on mechanical performance of coated specimens were investigated. The results show that the SiC/SiC-MoSi2-ZrB2 coating exhibits dense structure and is composed of SiC, Si, MoSi2 and ZrB2. It can protect C/C composites from oxidation at 1773 K for more than 510 h with weight loss of 0.5%. The excellent anti-oxidation performance of the coating is due to the formation of SiO2-ZrSiO4 complex glassy film. The coating can also endure the thermal shocks between 1773 K and room temperature for 20 times with residual flexural strength of 86.1%.     

Oxidation and Mechanical Properties of SiC/SiC-MoSi_2-ZrB_2 Coating for Carbon/Carbon Composites

To improve oxidation resistance of carbon/carbon(C/C) composites,a SiC/SiC-MoSi_2-ZrB_2 double-layer ceramic coating was prepared on C/C composites by two-step pack cementation.The phase compositions and microstructures of as-prepared multilayer coating were characterized by X-ray diffraction and scanning electron microscopy.The oxidation resistance at 1773 K and the effect of thermal shock between 1773 K and room temperature on mechanical performance of coated specimens were investigated.The results show that the SiC/SiC-MoSi_2-ZrB_2 coating exhibits dense structure and is composed of SiC,Si,MoSi_2 and ZrB_2·It can protect C/C composites from oxidation at 1773 K for more than 510 h with weight loss of 0.5%.The excellent anti-oxidation performance of the coating is due to the formation of SiO_2-ZrSiO_4 complex glassy film.The coating can also endure the thermal shocks between 1773 K and room temperature for 20 times with residual flexural strength of 86.1%.     

Si-Al-Ir Oxidation Resistant Coating for Carbon/Carbon Composites by Slurry Dipping

A Si-Al-Ir oxidation resistant coating was prepared for SiC coated carbon/carbon composites by slurry dipping. The phase composition, microstructure and oxidation resistance of the as-prepared Si-Al-Ir coating were studied by XRD (X-ray diffraction), SEM (scanning electron microscopy), and isothermal oxidation test at 1773 K in air, respectively. The surface of the as-prepared Si-Al-Ir coating was dense and the thickness was approximately 100 μm. Its anti-oxidation property was superior to that of the inner...     

液相法制备碳－碳Si－Mo防氧化涂层

用液相法制备出Ｓｉ－Ｍｏ涂层防氧化Ｃ／Ｃ，并对Ｓｉ－Ｍｏ涂层的防氧化性能进行了测试。结果表明，Ｓｔ－Ｍｏ是一种性能优良的Ｃ／Ｃ防氧化涂层，可以在１６５０℃下工作１０小时以上。同时对氧化前后涂层的裂纹形貌进行了分析。     

C/C复合材料表面水热电泳沉积SiCn/SiC复合抗氧化涂层研究

采用水热电泳沉积法在SiC-C/C复合材料表面制备纳米碳化硅（SiC_n）涂层. 采用XRD和SEM对涂层的晶相组成、表面和断面的微观结构进行了表征. 主要研究了水热沉积温度对涂层的结构及高温抗氧化性能的影响, 并分析了涂层试样在1600℃的高温氧化气氛下失效行为. 结果表明：纳米碳化硅涂层主要由β-SiC组成. 涂层的致密程度和厚度随着水热沉积温度的升高而提高. 随着水热温度的提高, 涂层试样的抗氧化性能也有明显的提高. 在120℃水热沉积温度下制备的涂层试样可在空气气氛1500℃下有效保护C/C复合材料202h,而氧化失重仅为2.16×10^-3g/cm². 在1600℃下氧化64h后失重为3.7×10^-3g/cm². 其高温失效是由于长时间的氧化挥发后表面SiO2膜不能完全封填表面缺陷, 内涂层中产生了贯穿性的孔隙所致.     

炭/炭复合材料磷酸盐涂层的抗氧化性能研究

为防止飞机刹车副用炭/炭(C/C)复合材料在刹车过程中氧化失效,研究了以磷酸、氧化硅和磷酸盐等为原料所制备的磷酸盐涂层的抗氧化性能,结果表明:涂覆有涂层的C/C复合材料在700 ℃氧化66 h后,其氧化失重率仅为1.11%;涂层试样在1 200 ℃氧化5 min后,失重率不超过0.8%;经900 ℃、3 min←→室温、2 min 100次热震后,涂层试件失重率为1.6%.涂层与基体结合牢固,一直保持完好,没有剥落,说明该涂料具有耐高温、热稳定性好等优点,适合作为C/C复合材料表面防氧化涂层.     

炭/炭复合材料表面C/SiC/Si-Mo-Cr多层复合防氧化涂层研究(英文)

为提高炭/炭(C/C)复合材料的高温抗氧化性能,采用料浆涂刷法首先在C/C复合材料表面制备了预炭层,然后以Si粉及石墨粉(Si粉与石墨粉的质量配比为:60～80:10～25)为原材料采用包埋法经高温热处理获得C/SiC内涂层,最后在涂有C/SiC内涂层的C/C复合材料表面采用包埋法制备Si-Mo-Cr外涂层。借助扫描电镜、X射线衍射、电子能谱等分析测试手段对涂层试样的微观结构进行了分析,研究了涂层C/C复合材料在1 873 K和1 973 K下的氧化行为。结果表明:由于涂层氧化过程中表面生成了SiO2和Cr2O3复合玻璃层,其在1 873 K温度下表现出优异的防氧化性能,可以有效保护C/C复合材料达135 h。当氧化温度提高至1 973 K并氧化30 h后,该复合涂层氧化过程玻璃层完整性被破坏,涂层失效。     

C/C复合材料Ta2O5-TaC/SiC抗氧化抗烧蚀涂层研究

采用包埋法和低压化学气相沉积(CVD)法在碳/碳(C/C)复合材料表面依次制备了Ta2O5-TaC内涂层和SiC外涂层,用X射线衍射分析(XRD)、扫描电镜(SEM)及电子能谱(EDS)对涂层的相组成、微观形貌和元素组成进行了分析,研究了涂覆涂层后C/C复合材料在1 500℃静态空气中的防氧化性能及在氧-乙炔烧蚀中的抗烧蚀性能。结果表明:采用两步法制得的Ta2O5-TaC/SiC复合涂层结构致密,该复合涂层有效提高了C/C复合材料的抗氧化和抗烧蚀性能;Ta2O5-TaC/SiC复合涂层在1 500℃静态空气环境下可对C/C复合材料有效保护100 h以上;涂层试样在氧乙炔烧蚀环境中烧蚀60 s表明涂层可将C/C复合材料的线烧蚀率降低47.07%,质量烧蚀率降低29.20%。     

用气相反应法制备C/C复合材料的梯度SiC涂层

本文采用化学气相反应法（CVR）制备了C/C复合材料的梯度SiC涂层,对该梯度涂层的形成机理及抗氧化性能进行了试验研究.研究结果表明：Si渗入基体的速率对梯度涂层的形成产生直接的影响,当采用体密度较高的C/C基体时,得到了完整致密的梯度SiC涂层,生成的SiC为β-SiC,该涂层具有较好的高温抗氧化能力,在1500℃静态空气气氛中,氧化26小时后失重不超过2%.     

MSI工艺制备C/SiC复合材料的氧化动力学和机理

以针刺整体炭毡为预制体, 采用CVD+MSI工艺制备了C/SiC复合材料, 借助XRD和SEM研究材料的微观组织, 通过等温氧化失重和非等温热重分析研究材料的氧化反应动力学和反应机理. 结果表明: MSI工艺所制备的C/SiC材料致密度高, 物相组成为类石墨结构的C、反应生成的SiC和残留Si. 其等温氧化反应机理: 第Ⅰ阶段为反应控制, 第Ⅱ和Ⅲ阶段为扩散和反应共同控制; 材料的非等温氧化过程呈现自催化特征, 氧化机理为随机成核, 氧化动力学参数为: lgA=8.752min^-1, E_a=169.167kJ·mol^-1. 与C/C材料相比, C/SiC材料有较差的低温氧化性能和稳定的高温氧化性能, 这与MSI的工艺特征密切相关.     

Multi-layer CVD-SiC/MoSi2–CrSi2–Si/B-modified SiC oxidation protective coating for carbon/carbon composites

To further improve the oxidation resistance of coating for carbon/carbon (C/C) composites, a multi-layer CVD-SiC/MoSi₂–CrSi₂–Si/B-modified SiC coating was prepared on the surface of C/C composites by pack cementation and chemical vapour deposition method, respectively. The microstructures, oxidation and thermal shock resistance of the coating were studied. The influence of B content in pack powder on the microstructure and oxidation resistance of B-modified SiC coating was also investigated. The results show that the B-modified SiC coating prepared with 10 wt.% B exhibited the best oxidation protection ability for C/C composites at 1173 K. The multi-layer coatings could protect the C/C composites at 1173 K for 30 h and 1873 K for 200 h, and endure 30 thermal cycles between 1873 K and room temperatures. The oxidation resistance and thermal shock resistance is mainly attributed to their dense structure and self-sealing property.     

碳/碳复合材料SiC/Al-Si涂层微观结构及抗氧化性能研究

采用料浆法在碳/碳复合材料碳化硅(SiC)内涂层表面制备了Al-Si合金外涂层,采用XRD和SEM分析了涂层的微观结构,并测试了带有SiC/Al-Si复合涂层的碳/碳复合材料试样在1500℃静态空气中的抗氧化性能.结果表明:Al-Si合金外涂层主要成分为Al3.21Si0.47,含有少量Al2O3;SiC/Al-Si复合涂层厚度约为120μm,无穿透性裂纹;SiC/Al-Si复合涂层的抗氧化性能明显优于单一SiC涂层,氧化17h后涂层试样的质量损失未超过5%.     

SiC纤维表面碳涂层及其SiCf／SiC复合材料性能研究

采用先驱体转化法（PIP）以酚醛和沥青为先驱体在SiC纤维表面涂覆碳层，并制备SiCf／SiC复合材料；优化了两种碳涂层制备工艺；分析了涂层后纤维的表面形貌并测试涂层厚度；研究了两种碳涂层对两种SiC纤维（普通和含铝）及复合材料力学性能的影响。     

碳／碳复合材料的氧化与防护

碳/碳复合材料的氧化敏感性限制了它的应用,为满足未来宇航飞行器等对高温结构材料的需要,必须彻底解决碳/碳复合材料的氧化防护问题。本文在认真分析碳/碳复合材料氧化过程的基础上,全面总结了提高碳/碳复合材料的抗氧化途径,其具体方法包括:材料内部结构、纤维、基体的改进和用各种方法在其表面施加保护涂层。同时,进一步发现:一种包括硼酸盐玻璃作内涂层,以SiC、Si_3N_4、SiO_2等作为外涂层的多层涂层系统,能在1700℃以下对碳/碳复合材料提供较好的防护。     

A multilayer MoSi2-SiC-B coating to protect SiC-coated carbon/carbon composites against oxidation

To protect carbon/carbon (C/C) composites against oxidation, a multilayer MoSi₂-SiC-B coating was prepared on the SiC-coated C/C composites by a simple and low-cost slurry method. The phase, microstructure and element distribution of the as-received coating were analyzed using X-ray diffraction, scanning electron microscopy and energy dispersive X-ray spectroscopy. The as-received coating could effectively protect C/C composites against oxidation at 850 °C in air for 100 h without mass loss, which exhibits better oxidation protective ability than the multilayer MoSi₂-SiC coating prepared by the same method. At intermediate temperature (850 °C), the excellent oxidation protective ability of the coating is mainly attributed to the formation of the molten B₂O₃ for sealing the microcracks and preventing oxygen from attacking the C/C substrate.     

包埋浸渗/气相沉积二步法在C/C复合材料表面制备SiC涂层

采用包埋浸渗法和化学气相沉积(CVD)法相结合在炭/炭(C/C)复合材料表面制备了SiC涂层, 借助扫描电镜、能谱分析以及X射线衍射等检测手段对涂层的微观组织形貌、元素分布和物相组成进行了观察与分析. 结果表明:包埋法制备的SiC涂层与C/C复合材料基体的界面处形成了梯度过渡层, CVD法制备的涂层十分致密, 有效填充了包埋SiC涂层中的孔隙, 因此, 二步法制备的SiC涂层具有良好的防氧化性能, 涂层试样在1500℃静态空气中氧化60h失重率仅为2.01%. 试样失重的主要原因是其在高低温热循环过程中氧气从涂层中的微裂纹扩散至基体表面, 从而引起基体氧化所致.