在极冷空间环境下加热执行器的影响

J. Scheidler, Erik J. Stalcup, E. Montbach
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引用次数: 2

摘要

传统的、润滑脂润滑的空间机构执行器可以实现长寿命,但必须加热到213k或-60°C以上,才能在极冷的环境中工作。本文首先概述了一项新的NASA项目,该项目正在开发两种旋转致动器,可以在不需要补充加热的情况下实现长寿命。然后,研究了在月球永久阴影区域中加热传统油脂润滑致动器的影响。为了便于评估,引入了一种新的总效率度量,将平均输出功率与平均总输入功率(即发热功率加上驱动/旋转功率)联系起来。该评估采用了热分析,分析了将执行器从30k加热到213k所需的能量,以及随后在运行状态下保持213k所需的功率。考虑了执行器运行的两个概念,分别突出了预热加热能量和维护加热器功率的影响。研究表明,在实际情况下,当执行器具有100%的常规工作效率时,其感知效率可以达到10%或更低,特别是当执行器具有高发射率并且在较低占空比下运行持续时间小于10小时时。在某些应用中,还介绍了其他影响以及减轻影响的方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The Impacts of Heating Actuators in Extremely Cold Space Environments
Conventional, grease-lubricated actuators for space mechanisms can achieve long life but must be heated above about 213 K, or -60 °C, to function in extremely cold environments. This paper first overviews a new NASA project that is developing two rotational actuators that can achieve long life without the need for supplemental heating. Then, the impacts of heating conventional, grease-lubricated actuators are studied for operation in a lunar permanently shadowed region. To facilitate the assessment, a novel total efficiency metric is introduced that relates the average power output to the average total power input (i.e., the power to heat plus the power to actuate/rotate). The assessment employs a thermal analysis of the energy required to heat an actuator from a survival temperature of 30 K to 213 K as well as the power required to subsequently maintain 213 K while in an operational state. Two concepts of actuator operation are considered that separately highlight the impacts of warmup heating energy and maintenance heater power. It is shown that in practical situations, the perceived efficiency of an actuator with 100% conventional operating efficiency can reach 10% or lower, particularly when the actuator has a high emissivity and is operated at lower duty cycles for durations less than 10 hours. Other impacts are presented along with a method of mitigating the impacts in some applications.
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