Jianfeng Huang Wendong Yang Liyun Cao
材料科学技术（英文）
In order to improve the oxidation resistance of carbon/carbon (C/C) composites, a SiC/C-AlPO4 multi-layer coating was fabricated on the C/C composites by a simple and low-cost method. The internal SiC bonding layer was prepared by a two-step pack cementation process and the external C-AlPO4 coating was deposited by hydrothermal electrophoretic deposition process. Phase compositions and microstructures of the as-prepared multi-layer coating were characterized by X-ray diffraction (XRD), scaning electron microspocy (SEM) and energy dispersive spectrometer (EDS). Anti-oxidation properties, oxidation behavior and the failure behavior of the coated composites were investigated. The results indicate that the multi-layer coating exhibits obviously two-layer structure. The inner layer is composed of β-SiC, α-SiC phase with a scale of silicon phase. The outer layer is composed of cristobalite aluminum phosphate (C-AlPO4) crystallites. The SEM observation shows the good bonding between the inner and outer layers. The multi-layer coating displays an excellent oxidation resistance in air in the temperature range from 1573 to 1773 K, and the corresponding oxidation activation energy of the coated C/C composites is calculated to be 117.2 kJ/mol. The oxidation process is predominantly controlled by the diffusion of O2 through the C-AlPO4 coating. The failure of the multi-layer coating results from the generation of the microholes that may be left by the escape of the oxidation gases.
关键词:
Carbon/carbon composites
,
磷酸铝
,
水热电泳沉积
,
涂层
,
氧化
Yulei ZHANG
,
Hejun LI
,
Qiangang FU
,
Kezhi LI
,
Dangshe HOU
,
null
材料科学技术（英文）
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 composites 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 resistance 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.
关键词:
Carbon/carbon composites
,
null
,
null
Xin Yang
材料科学技术（英文）
Oxidation protective MoSi2-Mo5Si3/SiC multi-coatings for carbon/carbon composites were prepared by chemical vapor reaction and slurry-sintering method. The influence of preparation technology on the structure and phase composition of the coating was investigated by scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS) and X-ray diffraction (XRD) analyses, and then their relationship was discussed. The results indicate that the Si/Mo ratio of the slurry and sintering processing were two main factors that significantly affected the structure and phase composition of the multi-coating. Appropriate sintering process and relatively high Si/Mo ratio were essential for preparing the multi-coating with dense structure and favorable phase composition. After being sintered at 1723 K for 2 h and with the Si/Mo ratio of the slurry being 4.5 (weight ratio), a dense structure accompanied by favorable phase composition of the coating can be obtained. When heat treated at 2373 K for 1 h, this coating became more compact and continuous. Oxidation tests (performed at 1623 and 1823 K) demonstrated that both of these two obtained multi-coatings exhibited better anti-oxidation property than single layer SiC coating.
关键词:
Carbon/carbon composites
,
null
,
null
苏君明
,
肖志超
,
刘勇琼
,
孟凡才
,
彭志刚
,
谷立民
,
李国峰
,
邢如鹏
新型炭材料
doi:10.1016/S1872-5805(09)60037-8
以针刺炭纤维准三向结构整体毡为预制体,经丙烯气体狭缝定向流的"外热内冷"、"内热外冷"径向热梯度CVI工艺致密技术,优化组合的热解炭/树脂炭双元炭基体技术,通过调控高温处理技术等三大关键技术制备了A320系列飞机炭刹车盘材料.与现用的A320系列飞机进口炭刹车盘进行了地面台架对比试验和装机应用.结果表明:自主开发的炭刹车盘其设计着陆能量和超载着陆能量的摩擦特性与国外相当,但在高能载(RTO)刹车时,其摩擦系数提高了21%～48%,静摩擦系数提高了28%;装机应用寿命平均达到2700次以上,比国外产品寿命提高了23%,凸现出长使用寿命和高摩擦特性的特色.
关键词:
飞机
,
炭刹车盘
,
炭/炭复合材料
,
摩擦系数
乔淑欣
宇航材料工艺
以美国航天用C/C复合材料专利申请为蓝本,研究了当前C/C复合材料及其应用中存在的技术问题、采用的技术手段,剖析了提高C/C复合材料抗氧化、耐高温、致密化、防裂解等性能的重点工艺.为进一步推动C/C复合材料在航天领域的应用提供专利情报参考.
关键词:
C/C复合材料
,
制备工艺
,
抗氧化
,
致密化
侯振华
,
郝名扬
,
罗瑞盈
,
向巧
,
杨威
,
商海东
,
许怀哲
新型炭材料
doi:10.1016/S1872-5805(15)60196-2
分别采用H2和CO2作为载气,CH4为前躯体,通过等温化学气相渗积制备炭/炭复合材料,通过偏光显微镜、拉曼光谱、X射线衍射和透射电镜对材料微观结构表征以及渗积过程密度变化,研究载气对沉积速率、体密度和微观结构的影响规律。结果表明：在渗积前50 h,CH4-H2体系的沉积速率明显大于CH4-CO2体系,但在其余渗积时间里,CH4-H2体系的沉积速率小于CH4-CO2体系。当载气从H2变成CO2时,复合材料的体密度从1.626 g/cm3增加到1.723 g/cm3,最大径向密度梯度从0.074 g/cm3减小到0.056 g/cm3。同时,基体炭从纯的粗糙体炭转变为杂化粗糙体炭含有过度生长锥,且平均石墨化度从62.7%下降到50.8%。这些显著的变化是由于CO2的氧化作用降低了表面沉积速率,却没有降低孔内沉积速率,同时大量的缺陷形成于层状石墨烯结构中导致形成过度生长锥,降低了热解炭织构。
关键词:
炭/炭复合材料
,
微观结构
,
化学气相渗积
,
载气
王向辉
,
翁力
,
张伟刚
新型炭材料
doi:10.1016/S1872-5805(14)60130-X
为了提高炭/炭(C/C)复合材料的高温抗氧化性能,应用多相反应技术在C/C复合材料表面制备SiC/Mo(Six、Al1-x )2复合涂层。利用扫描电镜、电子能谱、X射线衍射仪等测试手段对涂层材料的微观结构和物相组成进行分析,同时研究涂层C/C复合材料在超音速气流中的抗氧化性能。结果表明,C/C复合材料表面形成的抗氧化涂层显示出明显的双层结构,从外向内分别为Mo(Six、Al1-x)2与SiC的复合层和纯SiC层,同时有少量的Mo4.8Si3C0.6存在于涂层中。在温度为1800K、气体速率1500m/s的超音速气流中氧化冲刷96s,以及在2550K和室温下热循环24次的测试条件下,制备的SiC/Mo(Six、Al1-x )2涂层材料均未发生破坏现象。涂层材料优良的抗氧化性能和抗热震性能主要归因于基体C/C复合材料的高强度以及在氧化过程中材料表面形成的连续稳定的SiO2和Al2 O3玻璃相。
关键词:
SiC/Mo(Six,Al1-x)2涂层
,
炭/炭复合材料
,
多相反应技术
,
氧化行为
,
抗热震性能
李克智
,
李伟
,
新型炭材料
doi:10.1016/S1872-5805(14)60132-3
采用液相浸渍炭化技术,在压力为75 MPa下制备出4D-C/C复合材料,并进行高温热处理。研究静态和动态加载条件下,材料沿厚度方向的弯曲性能及断裂行为。结果表明,循环次数达到10×105次、频率为10 Hz时,材料的临界弯曲疲劳极限是静态弯曲强度的80%。静态弯曲加载情况下,C/C复合材料失效机制取决于试样底层炭纤维的取向。循环疲劳载荷作用下,其失效机制包括基体开裂、纤维-基体界面弱化及纤维断裂。复合材料在循环加载过程中界面结合强度降低,并释放内应力,故增强了纤维拔出以及复合材料的假塑性,疲劳加载后其剩余弯曲强度增加10%左右,而模量降低。疲劳载荷引起材料基体缺陷和裂纹数量的增加及纤维断裂,削弱了长度方向上的热膨胀,使材料热膨胀系数降低。
关键词:
C/C复合材料
,
疲劳
,
抗弯强度
,
微观结构
,
热膨胀
