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High Temperature Stability of Dissimilar Metal Joints in Fission Surface Power Systems

机译:裂变表面动力系统中异种金属接头的高温稳定性

摘要

Future generations of power systems for spacecraft and lunar surface systems will likely require a strong dependence on nuclear power. The design of a space nuclear power plant involves integrating together major subsystems with varying materia1 requirements. Refractory alloys are repeatedly considered for major structural components in space power reactor designs because refractory alloys retain their strength at higher temperatures than other classes of metals. The relatively higher mass and lower ductility of the refractory alloys make them less attractive for lower temperature subsystems in the power plant such as the power conversion system. The power conversion system would consist more likely of intermediate temperature Ni-based superalloys. One of many unanswered questions about the use of refractory alloys in a space power plant is how to transition from the use of the structural refractory alloy to more traditional structural alloys. Because deleterious phases can form when complex alloys are joined and operated at elevated temperatures, dissimilar material diffusion analyses of refractory alloys and superalloys are needed to inform designers about options of joint temperature and operational lifetime. Combinations of four superalloys and six refractory alloys were bonded and annealed at 1150 K and 1300 K to examine diffusional interactions in this study. Joints formed through hot pressing and hot isostatic pressing were compared. Results on newer alloys compared favorably to historical data. Diffusional stability is promising for some combinations of Mo-Re alloys and superalloys at 1150 K, but it appears that lower joint temperatures would be required for other refractory alloy couples.
机译:下一代用于航天器和月球表面系统的动力系统可能需要强烈依赖核动力。太空核电站的设计涉及将具有不同材料要求的主要子系统集成在一起。耐火合金被反复考虑用作空间动力反应堆设计中的主要结构部件,因为耐火合金在比其他金属类别更高的温度下仍能保持其强度。耐火合金的相对较高的质量和较低的延展性使得它们对电厂中较低温度的子系统(如电力转换系统)的吸引力较小。功率转换系统将更有可能由中等温度的镍基高温合金组成。关于在太空发电厂中使用耐火合金的许多未解决的问题之一是如何从结构耐火合金的使用过渡到更传统的结构合金。由于复杂的合金在高温下连接和操作时会形成有害相,因此需要对耐火合金和高温合金进行不同的材料扩散分析,以告知设计人员有关接头温度和使用寿命的选择。结合了四种高温合金和六种耐火合金的组合,并在1150 K和1300 K下进行了退火,以研究扩散相互作用。比较了通过热压和热等静压形成的接头。新型合金的结果优于历史数据。对于Mo-Re合金和超级合金在1150 K时的某些组合,扩散稳定性很有希望,但其他耐火合金对似乎需要较低的接头温度。

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