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Columbus on orbit test: HCU set-point change

机译:粗略测试:HCU设定点变化

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This paper describes the test performed on orbit on Columbus on the Heater Control Unit (HCU), the unit that commands the temperature control of the module external shell. Nominally, the HCU on/off set points are 20°C/23°C, while the cabin set point is 23°C. In 2016, upon temporary cabin set point change (from 23 to 19°C), it was pointed out an increase of power consumption by the HCU-controlled heaters. Based on this observation, Flight Control Team (FCT) required to verify the relationship between HCU set points, cabin air temperature and heater power consumption. Since the latter cannot be exactly predicted analytically (too many variables should be considered, e.g. cabin temperature set point, internal power dissipation, beta angle, ISS attitude variation...), an on orbit test was proposed by Engineering Control board (ECB) to integrate the available data. The on orbit HCU limits have been decreased to 18°C (low) and 21°C (high) from beginning of June 2017 to mid of January 2018. This test allowed collecting data over a significant range of beta angles and provided the necessary information to decide how to proceed with the nominal HCU set points. Available operational products allowed to execute this test and to protect against condensation issue if needed. Prior to the test, it was not known whether after decreasing the HCU limits the cabin temperature set point could be guaranteed for any combination of on-orbit conditions (beta angle) and cabin temperature set points (crew preference), therefore the cabin temperature trend was carefully monitored throughout the whole test in order to restore the previous HCU limits, if needed. The test has been successfully completed and preliminary results confirm a remarkable heater power saving and some cabin temperature issues, while the potential condensation issue during Condensing Heat eXchanger (CHX) dry-out is avoided applying the available operational countermeasures.
机译:本文介绍了在加热器控制单元(HCU)上的哥伦布上的轨道上进行的测试,该单元命令模块外壳的温度控制。名义上,HCU开/关设定点为20°C / 23°C,而机舱设定点为23°C。 2016年,在临时机舱设定点(从23到19°C)后,有指出了HCU控制加热器的功耗增加。基于此观察,需要验证HCU设定点,机舱空气温度和加热器功耗之间的关系所需的飞行控制团队(FCT)。由于后者无法分析预测(应考虑太多变量,例如驾驶室温度设定点,内部功耗,β角,ISS态度变化......),通过工程控制板(ECB)提出了ON轨道测试。集成可用数据。从2017年6月到2018年1月开始,ON轨道HCU限制已减少到18°C(低)和21°C(高)。该测试允许在大量β角度上收集数据并提供必要的信息决定如何继续使用标称HCU设定点。可用的操作产品允许执行此测试,并在需要时防止冷凝问题。在测试之前,尚不清楚在减少HCU限制后,可以保证机舱温度设定点,以便任何单轨条件(β角)和舱室温度设定点(船员偏好)的任何组合,从而保证机舱温度趋势如果需要,在整个测试中仔细监测,以便恢复以前的HCU限制。该试验已成功完成,初步结果证实了一个显着的加热器省电和一些驾驶室温度问题,而避免了在可用的操作对策应用冷凝热交换器(CHX)干燥过程中的潜在冷凝问题。

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