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...     

W-Mo-Si/SiC Oxidation Protective Coating for Carbon/Carbon Composites

A W-Mo-Si/SiC double-layer oxidation protective coating for carbon/carbon （C/C） composites was prepared by a two-step pack cementation technique. XRD （X-ray diffraction） and SEM （scanning electron microscopy）results show that the coating obtained by the first step pack cementation was a thin inner buffer layer of SiC with some cracks and pores, and a new phase of （WxMo1-x）Si2 appeared after the second step pack cementation. Oxidation test shows that, after oxidation in air at 1773 K for 175 h and thermal cycling between 1773 K and room temperature for 18 times, the weight loss of the W-Mo-Si/SiC coated C/C composites was only 2.06%. The oxidation protective failure of the W-Mo-Si/SiC coating was attributed to the formation of some penetrable cracks in the coating.     

C/SiC/Si-Mo-Cr复合涂层碳/碳复合材料力学性能研究

采用包埋法和涂刷法在碳/碳复合材料表面制备了一种新型的C/SiC/Si-Mo-Cr复合高温抗氧化涂层. 借助XRD和SEM等测试手段对所制备复合涂层的微观结构进行了表征, 采用三点弯曲试验研究了涂层处理及热震试验对碳/碳复合材料力学性能的影响规律. 结果表明: 制备的多相涂层结构致密, 涂层后碳/碳复合材料弯曲强度有所增大, 断裂特征由假塑性向脆性转变. 涂层试样经1500℃至室温20次热震后, 涂层试样的弯曲强度降低, 塑性增强.     

高温氧化及热震对SiC/ZrB2-SiC/SiC涂层炭/炭复合材料力学行为的影响

为提高炭/炭(C/C)复合材料的高温抗氧化性能,同时分析涂层制备及高温氧化对涂层材料力学行为的影响,在C/C复合材料表面采用反应熔渗、料浆涂刷结合化学气相沉积工艺制备了SiC/ZrB2-SiC/SiC三层高温抗氧化涂层。利用SEM和XRD分析复合涂层的微观结构和相组成,考察涂层复合材料1500℃高温抗氧化和1500℃-室温的抗热震性能,研究高温氧化及热震对涂层C/C复合材料力学行为的影响。结果表明,复合涂层试样1500℃静态空气环境下具有优异的抗氧化及抗热震性能:1500℃氧化20 h后试样保持增重,1500℃至室温热震50次后增重为0.69%。因涂层制备过程中粉料的渗入反应,复合材料弯曲强度增长了7.08%。在经历1500℃氧化20 h和1500℃至室温50次热震后,涂层复合材料弯曲强度有所下降,且因材料界面结合力的减弱使得纤维拔出特征明显,材料塑性断裂特征增强。     

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。     

Y_2Si_2O_7晶须增强MoSi_2复合涂层的制备及性能

采用水热电泳沉积法在C/C-SiC复合材料表面制备了Y2Si2O7晶须增强MoSi2复合抗氧化外涂层。采用X射线衍射仪(XRD)和扫描电子显微镜(SEM)对涂层的相组成和显微结构进行了表征。研究了Y2Si2O7晶须对复合涂层显微结构和抗氧化性能的影响。结果表明:Y2Si2O7晶须对复合涂层的显微结构和抗氧化性能有较大的影响。与MoSi2/SiC涂层相比,Y2Si2O7-MoSi2/SiC复合涂层均匀、致密,无显微裂纹。在静态空气氧化过程中,Y2Si2O7晶须有效阻止了外涂层的开裂,提高了涂层的抗氧化性能。该复合涂层试样在1773 K下氧化100 h,失重仅为0.73%,相应的失重速率仅为1.48×10-5g.cm-2.h-1。     

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.     

Influence of Thermal Shock on the Mechanical Behavior of Si-SiC Coated Carbon/Carbon Composites

Si-SiC coating was prepared on the surface of carbon/carbon (C/C) composites by a two-step technique of pack cementation, and the influences of thermal shock between 1773 K and room temperature in air on the mechanical property and fracture behavior of the coated C/C were studied. The results show that, after thermal shock between 1773 K and room temperature for 5, 10 and 15 times, the flexural strength of coated composites increases by 4.29%, 15.00% and 24.20%, respectively. The toughness of the coated C/C enhances gradually during the thermal shock test. The improvement of the mechanical property after the thermal shock test is primarily caused by the weakening of the fiber-matrix interface and the reduction of residual thermal stresses by thermal shock.     

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.     

AlPO_4晶相结构对复合涂层显微结构及抗氧化性能的影响

采用包埋法和水热电泳沉积法相结合的组合工艺在C/C复合材料表面制得SiC/AlPO4复合涂层.借助X射线衍射仪(XRD)和扫描电镜(SEM)对该复合涂层的晶相组成和显微结构进行了表征,重点研究了AlPO4晶相结构对复合涂层显微结构及抗氧化性能的影响.结果表明:AlPO4晶相结构对复合涂层的显微结构及抗氧化性能有较大的影响.采用石英型磷酸铝(B-AlPO4)晶相粉体所制备的涂层比较疏松,涂层自身的内聚力较差且涂层内部存在较多缺陷,采用磷石英型磷酸铝(T-AlPO4)晶相粉体所制备的涂层的致密性和均匀性相比于B-AlPO4有很大的提高,但是表面存在一些小孔且涂层与基体间存在裂纹,采用方石英型磷酸铝(C-AlPO4)晶相粉体所制备的涂层最致密且无明显的裂纹,与基体结合良好.C-AlPO4晶相粉体所制备的涂层具有较好的抗氧化性能,涂层试样在1500℃的空气气氛下氧化21h后失重仅为0.41wt%.     

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%。     

Preparation and Microstructure of a Si-Mo Fused Slurry Coating on Carbon/Carbon Composites for Oxidation Protection

A coating of composition Si-40Mo (wt pct) was prepared by fused slurry coating method on the two-dimensional carbon/carbon (2D-C/C) composite to improve oxidation resistance. In the procedure of the fabrication, pure St slurry inner layer in the pre-coating was necessary to apply because of infiltration of liquid Si into the substrate during the sintering. The coating consists of Si continuous phase and MoSi2 particles. In addition, the infiltration of Si into the substrate and the SiC reaction layer between the coating and the C/C composite were observed. Oxidation resistance and the thermal shock resistance of the Si-Mo fused sluury coating were quite excellent at 1730℃     

MoSi2-SiC 抗氧化涂层对碳/碳复合材料弯曲性能的影响

在C/C 复合材料表面制备了MoSi₂-SiC 抗氧化涂层, 分析了涂层工艺对C/C 复合材料组织的影响, 测试了材料的室温弯曲力学性能。结果表明, 该工艺在C/C 复合材料表面生成抗氧化涂层的同时, 基材内部的层间和纤维束界面, 以及孔隙周围也被硅化。C/C 复合材料经涂层工艺处理后, 弯曲断裂行为发生改变, 弯曲强度明显升高,塑性有一定程度的降低。      

Multi-composition oxidation resistant coating for SiC-coated carbon/carbon composites at high temperature

This work proposes a multi-composition oxidation resistant coating for SiC-coated carbon/carbon (C/C) composites by slurry method using the mixture of Y₂O₃, ZrO₂, Al₂O₃, Si and C. XRD analysis shows that the phases of the composite coating are composed of SiC, Al₂O₃, Y₂O₃, ZrO₂, Al₄SiC₄ and Y₃Al₂(AlO₄)₃. SEM analysis of the cross section of the coating displays the microstructure with 500 μm thickness which filled the porous SiC. Oxidation test shows that, after 19 h oxidation in air at 1873 K, the weight loss of the coated SiC-C/C is only 1.76%. The oxidation of the coated C/C composites was primarily due to the reaction of C/C matrix and oxygen diffusing through the penetrable cracks and bubble holes in the coating.     

炭/炭复合材料表面预炭层的制备及其性能研究

为在炭/炭复合材料表面制备C/SiC浓度梯度高温抗氧化涂层,预先用料浆涂刷-高温处理工艺在其表面制备了预炭层.借助XRD、Raman和SEM等测试手段对所制备预炭层的组织结构和微观形貌进行了表征,讨论了不同的原料配比和炭化温度对预炭层结构的影响,并对预炭层与基体的结合性能进行了测定.研究结果表明：制备的预炭层结构致密,与基体具有较好的结合性能,其结合强度可达10.95MPa.不同的原料配比和炭化温度影响了炭层序态结构的形成,最终形成了不同结构的预炭层.     

C/C复合材料SiC-MoSi2-TiSi2涂层的设计与性能

为了提高C/C复合材料的高温抗氧化性能,设计了网状的SiC填充高性能的MoSi2和微量的TiSi2涂层。用包埋法制备了C/C复合材料SiC-MoSi2-TiSi2复相陶瓷单层涂层,对制备涂层的化学形成机理进行了分析。结果表明,在选择的实验条件下,制备设计的涂层是完全可行的,实验制备的涂层在1773K有氧环境下具有良好的抗氧化性能。涂层抗氧化性能的提高是因为在高温氧化下涂层表面产生了致密、连续、稳定的玻璃质氧化物。     

SiC/PyC复合涂层碳纤维微观结构及氧化行为研究

采用两步法在碳纤维表面制备了碳化硅/热解碳(SiC/PyC)复合涂层,PyC内涂层的制备采用等温化学气相渗透法,SiC外涂层的制备采用碳热还原法.借助X射线衍射、场发射扫描电镜、透射电镜分析了SiC/PyC复合涂层碳纤维的物相组成以及微观结构,利用热重分析研究了SiC/PyC复合涂层、PyC涂层以及无涂层碳纤维的氧化行为.结果表明,在碳纤维表面制备的SiC/PyC复合涂层连续致密、厚度均匀,PyC内涂层厚度约为200nm,SiC外涂层厚度约为160nm,SiC层中存在大量孪晶面高度有序的SiC孪晶.SiC/PyC复合涂层能够有效地改善碳纤维的抗氧化性能,较无涂层碳纤维起始氧化温度提高了近250℃.     

Oxidation behavior and mechanical properties of C/SiC composites with Si-MoSi2 oxidation protection coating

A new kind of oxidation protection coating of Si-MoSi₂ was developed for three dimensional carbon fiber reinforced silicon carbide composites which could be serviced upto 1550 °C. The overall oxidation behavior could be divided into three stages: (i) 500 °C < T < 800 °C, the oxidation mechanism was considered to be controlled by the chemical reaction between carbon and oxygen; (ii) 800 °C < T < 1100 °C, the oxidation of the composite was controlled by the diffusion of oxygen through the micro-cracks, and; (iii) T > 1100 °C, the oxidation of SiC became significant and was controlled by oxygen diffusion through the SiC layer. Microstructural analysis revealed that the oxidation protection coating had a three-layer structure: the out layer is oxidation layer of silica glass, the media layer is Si + MoSi₂ layer, and the inside layer is SiC layer. The coated C/SiC composites exhibited excellent oxidation resistance and thermal shock resistance. After the composites annealed at 1550 °C for 50 h in air and 1550 °C 100 °C thermal shock for 50 times, the flexural strength was maintained by 85% and 80% respectively. The relationship between oxidation weight change and flexural strength revealed the criteria for protection coating was that the maximum point of oxidation weight gain was the failure starting point for oxidation protection coating.     

热压制备碳化硼涂层碳纤维增强碳化硅复合材料

采用聚对亚苯基硼的甲苯溶液为前驱体,并制得碳纤维增强碳化硅陶瓷基复合材料,初步探索了该工艺的可行性,同时对复合材料的结构与性能进行了表征。结果表明,所采用的碳纤维碳化硼涂层对复合材料的性能有很大的影响。     

ZrB2 coating for the oxidation protection of carbon fiber reinforced silicon carbide matrix composites

In order to improve the anti-oxidation performance of carbon fiber reinforced silicon carbide matrix (C/SiC) composites, ZrB₂ coating was prepared on the surface of C/SiC composites by a two-step technique of pack cementation method. The anti-oxidation properties of coated composites were investigated. The results showed that ZrB₂ coating was obtained by the method, which was homogenous and dense. The weight loss percentage of the coated composites was only 1.52 after oxidation in air at 1500 °C for 30 min, which exhibited excellent oxidation resistance.