Steady-state modeling and analysis of a two-loop cooling system for high heat flux removal applications are studied. The system structure proposed consists of a primary pumped loop and a vapor compression cycle (VCC) as the secondary loop to which the pumped loop rejects heat. The pumped loop consists of evaporator, condenser, pump, and bladder liquid accumulator. The pumped loop evaporator has direct contact with the heat generating device and CHF must be higher than the imposed heat fluxes to prevent device burnout. The bladder liquid accumulator adjusts the pumped loop pressure level and, hence, the subcooling of the refrigerant to avoid pump cavitation and to achieve high critical heat flux (CHF) in the pumped loop evaporator. The vapor compression cycle of the two-loop cooling system consists of evaporator, liquid accumulator, compressor, condenser and electronic expansion valve. It is coupled with the pumped loop through a fluid-to-fluid heat exchanger that serves as both the vapor compression cycle evaporator and the pumped loop condenser. The liquid accumulator of the vapor compression cycle regulates the cycle active refrigerant charge and provides saturated vapor to the compressor at steady state. The heat exchangers are modeled with the mass, momentum, and energy balance equations. Due to the projected incorporation of microchannels in the pumped loop to enhance the heat transfer in heat sinks, the momentum equation, rarely seen in previous refrigeration system modeling efforts, is included to capture the expected significant microchannel pressure drop witnessed in previous experimental investigations. Electronic expansion valve, compressor, pump, and liquid accumulators are modeled as static components due to their much faster dynamics compared with heat exchangers. The steady-state model can be used for static system design that includes determining the total refrigerant charge in the vapor compression cycle and the pumped loop to accommodate the varying heat load, sizing of various components, and parametric studies to optimize the operating conditions for a given heat load. The effect of pumped loop pressure level, heat exchangers geometries, pumped loop refrigerant selection, and placement of the pump (upstream or downstream of the evaporator) are studied. The two-loop cooling system structure shows both improved coefficient of performance (COP) and CHF overthe single loop vapor compression cycle investigated earlier by authors for high heat flux removal.
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ASME 2009 International Mechanical Engineering Congress and Exposition
November 13–19, 2009
Lake Buena Vista, Florida, USA
Conference Sponsors:
- ASME
ISBN:
978-0-7918-4382-6
PROCEEDINGS PAPER
The Steady-State Modeling and Analysis of a Two-Loop Cooling System for High Heat Flux Removal
Rongliang Zhou,
Rongliang Zhou
Rensselaer Polytechnic Institute, Troy, NY
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Juan Catano,
Juan Catano
Rensselaer Polytechnic Institute, Troy, NY
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Tiejun Zhang,
Tiejun Zhang
Rensselaer Polytechnic Institute, Troy, NY
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John T. Wen,
John T. Wen
Rensselaer Polytechnic Institute, Troy, NY
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Greg J. Michna,
Greg J. Michna
Rensselaer Polytechnic Institute, Troy, NY
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Yoav Peles,
Yoav Peles
Rensselaer Polytechnic Institute, Troy, NY
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Michael K. Jensen
Michael K. Jensen
Rensselaer Polytechnic Institute, Troy, NY
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Rongliang Zhou
Rensselaer Polytechnic Institute, Troy, NY
Juan Catano
Rensselaer Polytechnic Institute, Troy, NY
Tiejun Zhang
Rensselaer Polytechnic Institute, Troy, NY
John T. Wen
Rensselaer Polytechnic Institute, Troy, NY
Greg J. Michna
Rensselaer Polytechnic Institute, Troy, NY
Yoav Peles
Rensselaer Polytechnic Institute, Troy, NY
Michael K. Jensen
Rensselaer Polytechnic Institute, Troy, NY
Paper No:
IMECE2009-11500, pp. 1345-1356; 12 pages
Published Online:
July 8, 2010
Citation
Zhou, R, Catano, J, Zhang, T, Wen, JT, Michna, GJ, Peles, Y, & Jensen, MK. "The Steady-State Modeling and Analysis of a Two-Loop Cooling System for High Heat Flux Removal." Proceedings of the ASME 2009 International Mechanical Engineering Congress and Exposition. Volume 9: Heat Transfer, Fluid Flows, and Thermal Systems, Parts A, B and C. Lake Buena Vista, Florida, USA. November 13–19, 2009. pp. 1345-1356. ASME. https://doi.org/10.1115/IMECE2009-11500
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