首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >MONITORING DAMAGE IN NON-OXIDE COMPOSITES AT HIGH TEMPERATURES USING CARBON-CONTAINING CVD SIC MONOFILAMENT FIBERS AS EMBEDDED ELECTRICAL RESISTANCE SENSORS
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MONITORING DAMAGE IN NON-OXIDE COMPOSITES AT HIGH TEMPERATURES USING CARBON-CONTAINING CVD SIC MONOFILAMENT FIBERS AS EMBEDDED ELECTRICAL RESISTANCE SENSORS

机译:使用含碳的CVD SiC单丝纤维在嵌入式电阻传感器中监测在高温下的非氧化物复合材料的损伤

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Electrical resistance has become a technique of interest for monitoring SiC-based ceramic composites. The typical constituents of SiC fiber-reinforced SiC matrix composites. SiC, Si and/or C, are semi-conducive to some degree resulting in the fact that when damage occurs in the form of matrix cracking or fiber breakage, the resistance increases. For aero engine applications, SiC fiber reinforced SiC, sometimes Si-containing, matrix with a BN interphase are often the main constituents. The resistivity of Si and SiC is highly temperature dependent. For high temperature tests, electrical lead attachment must be in a cold region which results in strong temperature effects on baseline measurements of resistance. This can be instructive as to test conditions: however, there is interest in focusing the resistance measurement in the hot section where damage monitoring is desired. The resistivity of C has a milder temperature dependence than that of Si or SiC. In addition, if the C is penetrated by damage, it would result in rapid oxidation of the C, presumably resulting in a change in resistance. One approach considered here is to insert carbon "rods" in the form of CVD SiC monofilaments with a C core to try and better sense change in resistance as it pertains to matrix crack growth in an elevated temperature test condition. The monofilaments were strategically placed in two non-oxide composite systems to understand the sensitivity of ER in damage detection at room temperature as well as elevated temperatures. Two material systems were considered for this study. The first composite system consisted of a Hi-Nicalon woven fibers, a BN interphase and a matrix processed via polymer infiltration and pyrolysis (PIP) which had SCS-6 monofilaments providing the C core. The second composite system was a melt-infiltrated (MI) pre-preg laminate which contained Hi-Nicalon Type S fibers with BN interphases with SCS-Ultra monofilaments providing the C core. The two composite matrix systems represent two extremes in resistance, the PIP matrix being orders of magnitude higher in resistance than the Si-containing pre-preg MI matrix. Single notch tension-tension fatigue tests were performed at 815°C to stimulate crack growth. Acoustic emission (AE) was used along with electrical resistance (ER) to monitor the damage initiation and progression during the test. Post-test microscopy was performed on the fracture specimen to understand the oxidation kinetics and carbon recession length in the monofilaments.
机译:电阻已成为监测基于SiC的陶瓷复合材料的感兴趣技术。 SiC纤维增强SiC基复合材料的典型成分。 SiC,Si和/或C,是半有用的,导致某种程度导致的是,当损坏以基质裂化或纤维破裂的形式发生时,电阻增加。对于Aero发动机应用,SiC纤维增强SiC,有时含Si,具有BN界性的基质通常是主要的成分。 Si和SiC的电阻率依赖于温度。对于高温测试,电引线连接必须处于寒冷区域,导致对电阻的基线测量的强烈效应强。这可以是有益的测试条件:然而,有兴趣将希望在需要损坏监测的热部分中的电阻测量。 C的电阻率与Si或SiC的电阻率依赖。另外,如果C被损坏渗透,则会导致C的快速氧化,可能导致阻力发生变化。这里考虑的一种方法是将CVD SiC单丝的形式用C核心插入碳“棒”,以尝试更好的抗性变化,因为它涉及升高的温度试验条件的基质裂纹生长。单丝对两种非氧化物复合系统进行策略性地放置在两个非氧化物复合体系中,以了解ER在室温下损伤检测中的敏感性以及升高的温度。考虑了这项研究的两种材料系统。第一复合系统由高核编织纤维,BN差异和通过聚合物渗透和热解(PIP)加工的基质,其具有提供C芯的SCS-6单丝。第二复合体系是熔融渗透(MI)预先预涂层压材料,其含有Hi-Nicalon型S纤维,其具有BN差异与提供C芯的SCS-Ultra Monofilamentes。两种复合矩阵系统代表两个极端的电阻,PIP矩阵是含量高于含Si的Preg Mi矩阵的级别较高的级。在815℃下进行单个凹口张力张力疲劳试验以刺激裂纹生长。声发射(AE)与电阻(ER)一起使用,以监测测试期间的损伤启动和进展。在裂缝试样上进行测试后显微镜,以了解单丝中的氧化动力学和碳衰退长度。

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