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IMPROVED QUALITY ASSESSMENT FOR TURBINE ENGINE COMPONENTS WITH POTENTIAL APPLICATIONS TO CERAMIC MATRIX COMPOSITE (CMC) MATERIALS

机译:提高涡轮发动机部件的质量评估,具有潜在应用的陶瓷基质复合材料(CMC)材料

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Demand for improved power from turbine engines has resulted in the development of ceramic matrix composite (CMC) materials that can withstand extreme temperature environments and maintain the damage tolerance required for space vehicles and next generation turbine engines. CMC components allow higher temperature operation and increased power over nickel-based superalloy components due to their reduced weight and temperature stability. The use of CMCs allows a potential increase in turbine engine temperatures to above 1400°C. This temperature increase results in improved performance, which translates into increased efficiency, better power to weight ratios, and improved reliability with both significant fuel savings and reduced life cycle costs. Evaluating CMC component quality is difficult due to variations in the fiber/matrix properties and variations in fabrication related parameters. Further, there is limited information on operational and remaining life characteristics. These factors produce significant challenges to existing inspection methods. Determining the reliability of CMC components is a complex process and requires an understanding of both manufacturing variability and damage effects that can occur throughout the life of the component. Consequently, a nondestructive inspection capability is required that can reliably evaluate CMC components during manufacturing, provide acceptance/rejection criteria for determining "fitness for use" and be useful for assessing operational damage effects. New nondestructive testing capabilities, Photon Induced Positron Annihilation (PIPA) and Distributed Source Positron Annihilation (DSPA), have demonstrated the potential ability to detect and quantify fabrication flaws and manufacturing quality for metallic, composite and ceramic components that are used to improve performance and power to weight ratios in high temperature turbine engine applications.
机译:从涡轮发动机提高功率的需求导致陶瓷基质复合材料(CMC)材料的开发,其能够承受极端温度环境,并保持太空车辆和下一代涡轮发动机所需的损坏公差。由于其重量和温度稳定性,CMC部件允许更高的温度操作和基于镍的超合金组分的功率增加。 CMC的使用允许涡轮发动机温度的潜在增加至于1400°C以上。这种温度升高导致改进的性能,这转化为提高效率,更好的重量比率,并提高了具有显着燃料节省和降低生命周期成本的可靠性。由于光纤/矩阵特性的变化和制造相关参数的变化,评估CMC分量质量很难。此外,有关操作和剩余寿命特征的信息有限。这些因素对现有的检查方法产生了重大挑战。确定CMC组件的可靠性是复杂的过程,并且需要了解在整个部件的整个寿命中发生的制造变异性和损伤效果。因此,非破坏性的检查能力,需要在制造过程中可以可靠地评估CMC部件,用于确定“适合使用”提供接受/拒绝标准和对于评估操作伤害效果是有用的。新无损检测能力,光子诱导正电子湮没(PIPA)和分布式源正电子湮没(DSPA),已经证明,以检测用于改善性能和功率的潜在能力和量化制造缺陷和制造质量为金属,复合材料和陶瓷部件高温涡轮发动机应用中的体重比。

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