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Startup Response for a Nuclear Brayton Power Conversion System

机译:核布雷顿电力转换系统的启动响应

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Dynamic power conversion technologies, like the closed Brayton cycle (CBC) power conversion system, are being considered for high power nuclear electric propulsion (NEP) missions to explore the outer planets and their moons under Project Prometheus. JIMO, the Jupiter Icy Moons Orbiter mission may require in the range of 100 kWe to the electric propulsion units to achieve reasonable mission timelines of 10 years or less. A key milestone in any NEP mission, besides launch, is the remote, on-orbit startup of the nuclear reactor unit and its progression to higher operating temperatures and thermal power levels. With dynamic power conversion units like CBC, the individual units can be motored up to operating speed within 60 seconds if the heat source is maintained at a high temperature (>950 K) during the engine startup sequence. However, thermal transients are introduced into the nuclear reactor heat source subsystem during this engine startup sequence through the fast reactor's negative temperature coefficient of reactivity. Therefore, the commanded reactivity insertion rate in a fast reactor, to increase its thermal power output during the CBC startup transient, must be limited to a fairly small step size over a controlled time period to provide for a safe operating envelope. The reactor thermal power level, coolant outlet temperatures and coolant flow rates are critical parameters that need to be addressed in the selection and design of the primary heat transport subsystem's components. The transient response of a liquid metal cooled fast reactor, a thermoelectric electromagnetic (TEM) pump, and a liquid metal heat transport loop were evaluated during the startup of a four-unit CBC power conversion subsystem. The goal of the analysis was to assess the minimum time period required, after initial reactor criticality, to reach full electrical power output from the power generating subsystem. The results indicate that an auto-start sequence controller can provide for a safe ascension to full power operation of a fast reactor-CBC space power system.
机译:像封闭的布雷顿周期(CBC)电源转换系统一样,动态电力转换技术正在考虑高功率核电推进系统(NEP)任务,探索项目普罗米修斯项目下的外部行星及其卫星。 Jimo,木星冰冷的Moons Orbiter Mission可能需要在100kWe到电动推进装置的范围内实现合理的任务时间表10年或更少。除了发射之外,任何NEP任务的关键里程碑是核反应器单元的远程,轨道启动及其对更高的操作温度和热功率水平的进展。利用动态电源转换单元如CBC,如果在发动机启动序列期间,如果热源在高温(> 950 k)处,则各个单元可以在60秒内移动到操作速度。然而,通过快速反应堆的负温度系数在该发动机启动序列期间将热瞬变引入核反应堆热源子系统中。因此,在快速反应器中的命令反应性插入速率,以增加CBC启动瞬态期间的热功率输出,必须限于受控时间段的相当小的步长,以提供安全的操作包络。电抗器热功率水平,冷却剂出口温度和冷却剂流量是需要在主要传热子系统组件的选择和设计中寻址的关键参数。在四单元CBC电力转换子系统的启动期间评估液态金属冷却快速反应器,热电电磁(TEM)泵和液态金属传热环的瞬态响应。分析的目标是评估初始反应堆临界性后所需的最短时间段,以从发电子系统到达全电力输出。结果表明,自动启动序列控制器可以提供安全提升到快速反应堆-CBC空间电力系统的全功率操作。

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