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Structural Benchmark Creep Testing for the Advanced Stirling Convertor Heater Head

机译:先进的斯特林换热器加热头的结构基准蠕变测试

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摘要

The National Aeronautics and Space Administration (NASA) has identified the high efficiency Advanced Stirling Radioisotope Generator (ASRG) as a candidate power source for use on long duration Science missions such as lunar applications, Mars rovers, and deep space missions. For the inherent long life times required, a structurally significant design limit for the heater head component of the ASRG Advanced Stirling Convertor (ASC) is creep deformation induced at low stress levels and high temperatures. Demonstrating proof of adequate margins on creep deformation and rupture for the operating conditions and the MarM-247 material of construction is a challenge that the NASA Glenn Research Center is addressing. The combined analytical and experimental program ensures integrity and high reliability of the heater head for its 17-year design life. The life assessment approach starts with an extensive series of uniaxial creep tests on thin MarM-247 specimens that comprise the same chemistry, microstructure, and heat treatment processing as the heater head itself. This effort addresses a scarcity of openly available creep properties for the material as well as for the virtual absence of understanding of the effect on creep properties due to very thin walls, fine grains, low stress levels, and high-temperature fabrication steps. The approach continues with a considerable analytical effort, both deterministically to evaluate the median creep life using nonlinear finite element analysis, and probabilistically to calculate the heater head s reliability to a higher degree. Finally, the approach includes a substantial structural benchmark creep testing activity to calibrate and validate the analytical work. This last element provides high fidelity testing of prototypical heater head test articles; the testing includes the relevant material issues and the essential multiaxial stress state, and applies prototypical and accelerated temperature profiles for timely results in a highly controlled laboratory environment. This paper focuses on the last element and presents a preliminary methodology for creep rate prediction, the experimental methods, test challenges, and results from benchmark testing of a trial MarM-247 heater head test article. The results compare favorably with the analytical strain predictions. A description of other test findings is provided, and recommendations for future test procedures are suggested. The manuscript concludes with describing the potential impact of the heater head creep life assessment and benchmark testing effort on the ASC program.
机译:美国国家航空航天局(NASA)已将高效斯特林放射性同位素发生器(ASRG)确定为可用于长期科学任务(例如登月应用,火星探测器和深空任务)的候选动力源。对于所需的固有长寿命,ASRG高级斯特林转换器(ASC)的加热器头组件在结构上的重大设计限制是在低应力水平和高温下引起的蠕变变形。证明在运行条件和MarM-247结构材料方面具有足够的蠕变变形和破裂余量,这是NASA格伦研究中心正在解决的挑战。分析和实验相结合的程序可确保加热器头在其17年的设计寿命中保持完整性和高可靠性。寿命评估方法始于在薄的MarM-247样品上进行的一系列广泛的单轴蠕变测试,这些样品的化学成分,微观结构和热处理工艺与加热头本身相同。这项工作解决了由于材料非常薄的壁,细晶粒,低应力水平和高温制造步骤而导致的材料缺乏可公开获得的蠕变特性以及几乎没有了解对蠕变特性的影响的问题。该方法继续进行大量的分析工作,既可以使用非线性有限元分析确定性地评估中值蠕变寿命,也可以概率性地更高程度地计算加热器头的可靠性。最后,该方法包括大量的结构基准蠕变测试活动,以校准和验证分析工作。最后一个元素提供原型加热器头测试物品的高保真度测试;测试包括相关的材料问题和基本的多轴应力状态,并应用原型和加速温度曲线,以便在高度受控的实验室环境中及时获得结果。本文侧重于最后一个要素,并提出了蠕变速率预测的初步方法,实验方法,测试挑战以及MarM-247加热器头部试验文章的基准测试结果。结果与分析应变预测相比具有优势。提供了其他测试结果的描述,并建议了以后的测试程序。该手稿最后描述了加热器头蠕变寿命评估和基准测试工作对ASC程序的潜在影响。

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