Reduced Gravity and Ground Testing of a Two-Phase Thermal Management System for Large Spacecraft

1988 ◽  
Author(s):  
D. G. Hill ◽  
K. Hsu ◽  
R. Parish ◽  
J. Dominick
Keyword(s):  
Thermal Management ◽  
Management System ◽  
Reduced Gravity ◽  
Two Phase ◽  
Ground Testing ◽  
Thermal Management System

scholarly journals Thermal Performance of a Cylindrical Lithium-Ion Battery Module Cooled by Two-Phase Refrigerant Circulation

Energies ◽  
2021 ◽  
Vol 14 (23) ◽  
pp. 8094
Author(s):  
Bichao Lin ◽  
Jiwen Cen ◽  
Fangming Jiang
Keyword(s):  
Thermal Management ◽  
Management System ◽  
Cooling System ◽  
Maximum Temperature ◽  
Two Phase ◽  
Battery Thermal Management ◽  
Thermal Management System ◽  
Battery Thermal Management System ◽  
Li Ion ◽  
Battery Module

It is important for the safety and good performance of a Li-ion battery module/pack to have an efficient thermal management system. In this paper, a battery thermal management system with a two-phase refrigerant circulated by a pump was developed. A battery module consisting of 240 18650-type Li-ion batteries was fabricated based on a finned-tube heat-exchanger structure. This structural design offers the potential to reduce the weight of the battery thermal management system. The cooling performance of the battery module was experimentally studied under different charge/discharge C-rates and with different refrigerant circulation pump operation frequencies. The results demonstrated the effectiveness of the cooling system. It was found that the refrigerant-based battery thermal management system could maintain the battery module maximum temperature under 38 °C and the temperature non-uniformity within 2.5 °C for the various operation conditions considered. The experimental results with 0.5 C charging and a US06 drive cycle showed that the thermal management system could reduce the maximum temperature difference in the battery module from an initial value of 4.5 °C to 2.6 °C, and from the initial 1.3 °C to 1.1 °C, respectively. In addition, the variable pump frequency mode was found to be effective at controlling the battery module, functioning at a desirable constant temperature and at the same time minimizing the pump work consumption.

scholarly journals Favourably regulating two-phase flow regime of flow boiling HFE-7100 in microchannels using silicon nanowires

2021 ◽  
Vol 11 (1) ◽  
Author(s):  
Tamanna Alam ◽  
Wenming Li ◽  
Wei Chang ◽  
Fanghao Yang ◽  
Jamil Khan ◽  
...  
Keyword(s):  
Flow Regime ◽  
Thermal Management ◽  
Silicon Nanowires ◽  
Management System ◽  
High Speed ◽  
Flow Boiling ◽  
Flow Regimes ◽  
Phase Flow ◽  
Two Phase ◽  
Thermal Management System

AbstractHigh performance miniaturized electronic devices require enhanced, compact and reliable thermal management system. As an efficient compact space cooling technique, flow boiling in microchannels has recently gained wide acceptance. However, weak buoyancy effects and microgravity in avionics and numerous space systems operations hinder the performance of flow boiling microchannel thermal management system due to poor bubble departure capacity and unfavorable development of flow regimes. Here we report the flow boiling silicon nanowires (SiNWs) microchannels which can favorably regulate two-phase flow regimes by enhancing explosive boiling, minimizing bubble departure diameter, and smoothing flow regime transition. Extensive experimental investigations along with high speed visualizations are performed. The experiments are performed with the dielectric fluid HFE-7100 in a forced convection loop for wide range of heat and mass fluxes. High speed flow visualizations have been employed at up to 70 k frames per second (fps) to understand the boiling mechanism in terms of bubble dynamics, flow patterns, and flow regime developments for SiNWs microchannels. These studies show that SiNWs reduce intermittent flow regimes (slug/churn), improve rewetting and maintain thin liquid film at wall. Therefore, flow boiling in SiNW microchannels is promising to thermal management owing to its high heat transfer rate with low pressure drop and negligible microgravity sensitivity.

A Two-Phase Thermal Management System for the Space Station

1984 ◽  
Author(s):  
Timothy J. Bland ◽  
Robert S. Downing ◽  
David P. Rogers
Keyword(s):  
Thermal Management ◽  
Management System ◽  
Space Station ◽  
Two Phase ◽  
Thermal Management System

A Highly Stable Two-Phase Thermal Management System for Aircraft

2012 ◽  
Author(s):  
Weibo Chen ◽  
David W. Fogg ◽  
Michael Izenson ◽  
Cable Kurwitz
Keyword(s):  
Thermal Management ◽  
Management System ◽  
Two Phase ◽  
Thermal Management System
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