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Creep performance of oxide ceramic fiber materials at elevated temperature in air and in steam.

机译:氧化物陶瓷纤维材料在高温下在空气和蒸汽中的蠕变性能。

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摘要

Structural aerospace components that operate in severe conditions, such as extreme temperatures and detrimental environments, require structural materials that have superior long-term mechanical properties and that are thermochemically stable over a broad range of service temperatures and environments. Ceramic matrix composites (CMCs) capable of excellent mechanical performance in harsh environments are prime candidates for such applications. Oxide ceramic materials have been used as constituents in CMCs. However, recent studies have shown that high-temperature mechanical performance of oxide-oxide CMCs deteriorate in a steam-rich environment. The degradation of strength at elevated temperature in steam has been attributed to the environmentally assisted subcritical crack growth in the oxide fibers. Furthermore, oxide-oxide CMCs have shown significant increases in steady-state creep rates in steam. The present research investigated the effects of steam on the high-temperature creep and monotonic tension performance of several oxide ceramic materials. Experimental facilities were designed and configured, and experimental methods were developed to explore the influence of steam on the mechanical behaviors of ceramic fiber tows and of ceramic bulk materials under temperatures in the 1100--1300°C range.;The effects of steam on creep behavior of Nextel(TM)610 and Nextel(TM)720 fiber tows were examined. Creep rates at elevated temperatures in air and in steam were obtained for both types of fibers. Relationships between creep rates and applied stresses were modeled and underlying creep mechanisms were identified. For both types of fiber tows, a creep life prediction analysis was performed using linear elastic fracture mechanics and a power-law crack velocity model. These results have not been previously reported and have critical design implications for CMC components operating in steam or near the recommended design limits. Predictions were assessed and validated via comparisons with experimental results. Additionally, the utility of the Monkman-Grant relationship to predicting creep-rupture life of the fiber tows at elevated temperature in air and in steam was demonstrated.;Furthermore, the effects of steam on the compressive creep performance of bulk ceramic materials were also studied. Performance of fine grained, polycrystalline alumina (Al2O3) was investigated at 1100 and 1300°C in air and in steam. To evaluate the effect of silica doping during material processing both undoped and silica doped polycrystalline alumina specimens were tested. Finally, compressive creep performance of yttrium aluminum garnet (YAG, Y3Al5O12) was evaluated at 1300°C in air and in steam. Both undoped and silica doped YAG specimens were included in the study. YAG is being considered as the next-generation oxide fiber material. However, before considerable funding and effort are invested in a fiber development program, it is necessary to evaluate the creep performance of YAG at elevated temperature in steam. Results of this research demonstrated that both the undoped YAG and the silica doped YAG exhibited exceptional creep resistance at 1300°C in steam for grain sizes ∼1 microm. These results supplement the other promising features of YAG that make it a strong candidate material for the next generation ceramic fiber.
机译:在恶劣条件下(例如极端温度和有害环境)运行的结构性航空部件需要结构材料具有出色的长期机械性能,并且在广泛的使用温度和环境范围内具有热化学稳定性。在恶劣环境下具有出色机械性能的陶瓷基复合材料(CMC)是此类应用的主要候选产品。氧化物陶瓷材料已被用作CMC中的成分。但是,最近的研究表明,在富蒸汽环境中,氧化物-氧化物CMC的高温机械性能会下降。蒸汽中高温强度的降低归因于氧化物纤维中环境辅助的亚临界裂纹的增长。此外,氧化物-氧化物CMC已显示出蒸汽中稳态蠕变速率的显着提高。本研究研究了蒸汽对几种氧化物陶瓷材料的高温蠕变和单调张力性能的影响。设计和配置了实验设备,并开发了实验方法以探索蒸汽在1100--1300°C温度范围内对陶瓷纤维丝束和陶瓷散装材料的力学行为的影响;蒸汽对蠕变的影响检查了Nextel TM 610和Nextel TM 720纤维束的行为。两种类型的纤维在高温下在空气和蒸汽中的蠕变速率均获得了。对蠕变速率与施加应力之间的关系进行了建模,并确定了潜在的蠕变机理。对于两种类型的纤维束,均使用线性弹性断裂力学和幂律裂纹速度模型进行了蠕变寿命预测分析。这些结果以前没有被报道过,对于在蒸汽中或接近建议的设计极限下运行的CMC组件具有关键的设计意义。通过与实验结果进行比较来评估和验证预测。此外,还证明了Monkman-Grant关系在预测纤维束在空气和蒸汽中在高温下的蠕变断裂寿命时的实用性;此外,还研究了蒸汽对散装陶瓷材料压缩蠕变性能的影响。在1100和1300°C下的空气和蒸汽中研究了细晶多晶氧化铝(Al2O3)的性能。为了评估材料加工过程中二氧化硅掺杂的效果,对未掺杂和二氧化硅掺杂的多晶氧化铝样品均进行了测试。最后,在1300℃下在空气和蒸汽中评估了钇铝石榴石(YAG,Y3Al5O12)的压缩蠕变性能。该研究包括未掺杂和二氧化硅掺杂的YAG标本。 YAG被认为是下一代氧化物纤维材料。但是,在投入大量资金和精力进行纤维开发计划之前,有必要评估蒸汽在高温下YAG的蠕变性能。这项研究的结果表明,未掺杂的YAG和二氧化硅掺杂的YAG都在1300°C的蒸汽中表现出优异的抗蠕变性,晶粒尺寸约为1微米。这些结果补充了YAG的其他有希望的特性,使其成为下一代陶瓷纤维的强大候选材料。

著录项

  • 作者

    Armani, Clinton j.;

  • 作者单位

    Air Force Institute of Technology.;

  • 授予单位 Air Force Institute of Technology.;
  • 学科 Engineering Aerospace.;Engineering Materials Science.;Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2011
  • 页码 232 p.
  • 总页数 232
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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