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Stirling engine external heat system design with heat pipe heater

机译:带有热管加热器的斯特林发动机外部热系统设计

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摘要

This final report presents the conceptual design of a liquid fueled external heating system (EHS) and the preliminary design of a heat pipe heater for the STM-4120 Stirling cycle engine, to meet the Air Force mobile electric power (MEP) requirement for units in the range of 20 to 60 kW. The EHS design had the following constraints: (1) Packaging requirements limited the overall system dimensions to about 330 mm x 250 mm x 100 mm; (2) Heat flux to the sodium heat pipe evaporator was limited to an average of 100 kW/m and a maximum of 550 kW/m based on previous experience; and (3) The heat pipe operating temperature was specified to be 800 C based on heat input requirements of the STM4-120. An analysis code was developed to optimize the EHS performance parameters and an analytical development of the sodium heat pipe heater was performed; both are presented and discussed. In addition, construction techniques were evaluated and scale model heat pipe testing performed.
机译:这份最终报告介绍了用于STM-4120斯特林循环发动机的液体燃料外部加热系统(EHS)的概念设计和热管加热器的初步设计,以满足美国空军单位对空军移动电源(MEP)的要求。 20至60 kW的范围。 EHS设计具有以下限制条件:(1)包装要求将整个系统的尺寸限制为约330 mm x 250 mm x 100 mm; (2)根据以往的经验,流向钠热管蒸发器的热通量被限制为平均100 kW / m,最大550 kW / m。 (3)根据STM4-120的热输入要求,将热管的工作温度规定为800℃。开发了分析代码以优化EHS性能参数,并进行了钠热管加热器的分析开发;都介绍和讨论。此外,评估了施工技术并进行了比例模型热管测试。

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