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High Temperature Heat Pipes for Space Fission Power

机译:用于空间裂变动力的高温热管

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Future space transportation and surface power applications will require small fission reactors for power generation. The fission reactors would generate up to 13kWt of power for the energy conversion system. The heat generated by the reactor would be collected and transferred by high temperature alkali metal heat pipes to a series of Stirling convertors or thermoelectric convertors for power generation. These heat pipes would be relatively long, 2 meters for a Stirling convertor design, and 4 m for a thermoelectric converter design. Previous alkali metal heat pipe designs for spacecraft have used arterial, annular, or crescent wicks. All of these wicks can be difficult to fabricate for long heat pipes. Two other wick designs were examined in this study, grooved wicks, and self-venting arterial wicks. Artery de-priming by trapped vapor or non-condensable gas in an artery has been a single point failure for traditional arterial heat pipes. A self-venting arterial heat pipe has a screen artery that contains small venting pores in the evaporator section that allow for any trapped vapor or non-condensable gas (NCG) to escape. A trade study was conducted to compare the maximum transport and specific power for the self-vented artery, arterial, and grooved heat pipe designs. In all cases for a given diameter, the self-vented artery design carried the highest power, and had the highest specific power. Two 1-m long heat pipes were fabricated and tested, a self-venting wick and a grooved wick. The 1m long, 0.75in. (1.91cm) outer diameter sodium self-venting arterial heat pipe is capable of carrying 3.4kW of power at adverse elevations of up to 3.0in (7.62cm) without drying out. At an elevation of 5.0in (12.7cm), the self-venting arterial heat pipe is capable of carrying a maximum transport power of 1.4kW. Grooved heat pipes are typically used for spacecraft thermal control, since any NCG in the grooves can easily escape. The 1m long, 0.75in (1.91cm) outer diameter sodium grooved heat pipe is capable of carrying 846W, 546W and 346W at adverse elevations of 0.1in (0.25cm), 0.6in (1.52cm) and 1.0in (2.54cm), respectively.
机译:未来的太空运输和地面动力应用将需要小型裂变反应堆来发电。裂变反应堆将为能量转换系统产生高达13kWt的功率。反应堆产生的热量将被收集,并通过高温碱金属热管传递给一系列斯特林转换器或热电转换器进行发电。这些热管相对较长,斯特林转换器设计为2米,热电转换器设计为4 m。先前用于航天器的碱金属热管设计已使用动脉,环形或月牙形芯。所有这些灯芯都很难为长热管制造。在这项研究中,还检查了其他两种灯芯设计,即带凹槽的灯芯和自动通风的动脉灯芯。对于传统的动脉热管来说,由滞留在动脉中的蒸气或不凝性气体引起的动脉消融已成为单点故障。自通风的动脉热管具有一个筛网动脉,该筛网动脉的蒸发器部分中包含小的通风孔,这些通风孔可使任何残留的蒸汽或不可冷凝的气体(NCG)逸出。进行了一项贸易研究,以比较自排气动脉,动脉和沟槽式热管设计的最大输送量和比功率。在所有情况下,对于给定的直径,自排气动脉设计具有最高的功率,并且具有最高的比功率。制作并测试了两个长度为1米的热管,一个自排气芯和一个带凹槽的芯。 1m长,0.75in。 (1.91cm)外径钠自动通风动脉热管能够在高达3.0英寸(7.62厘米)的不利海拔高度上承载3.4千瓦的功率,而不会变干。自通风的动脉热管在5.0英寸(12.7厘米)的高度上能够承载1.4kW的最大输送功率。凹槽式热管通常用于航天器的热控制,因为凹槽中的任何NCG都可以轻易逸出。 1m长,外径为0.75英寸(1.91厘米)的钠槽热管能够以0.1英寸(0.25厘米),0.6英寸(1.52厘米)和1.0英寸(2.54厘米)的不利仰角承载846W,546W和346W,分别。

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