Session: 17-01-01: Research Posters

Paper Number: 148867

148867 - Experimental Characterization of High-Surface Area Thermal Energy Storage 

There is growing interest in energy storage technologies due to the expansion of renewable energy sources that are inherently intermittent and the increasing frequency of extreme weather events that disturb the power grid. Power consumption in buildings makes up approximately 76% of all electricity usage on the grid and is primarily used for thermal applications such as space conditioning, hot water, and cooking. This makes thermal energy storage (TES) an ideal solution for many of these applications. Many TES technologies rely on latent energy storage, which utilizes the melting/solidification of phase change materials (PCM) to store energy. Typically, TES designs suffer from low power density due to the low inherent thermal conductivity of many PCMs. This limitation makes the deployment of TES in active applications difficult as the ease of access to energy is essential for effective use. Common routes for improving power density include high thermal conductivity additives or extended features such as fins that increase cost. This study presents an alternative approach to improving performance through increasing the overall surface area to volume ratio of the device, to increase the available area for convection to occur between the working fluid and PCM.  

In the study a commercial PCM was selected with a transition temperature ideal for space heating applications. The heat exchanger design utilizes a unique application of triply periodic minimal surfaces (TPMS) for macro-encapsulation of the PCM. The use of TPMS for heat exchangers has been growing in interest due to their high-surface area to volume ratios, which were previously unmanufacturable until the development of additive manufacturing. A modular system was designed and manufactured with a stereolithography resin printing system that is then backfilled with PCM. An experiment test set-up is designed to test the charge and discharge performance of the thermal storage using a conditioned air stream.  

The pressure drop of the design is tested across a variety of flow rates. When compared to existing experimental data within literature, there is excellent agreement based on the Reynolds number at similar hydraulic diameters. Several inlet temperatures are tested at consistent temperature differences from the phase change temperature for both charging and discharging. Additionally, the volumetric flow rate is varied for each temperature set point. It was found that increasing flow rate had diminishing returns in reducing the overall charge time of the TES. The temperature delta from the melting temperature was the primary contributor to the change in average heat flux, with limited variation in average heat transfer rate between charging and discharging at similar temperature deltas and flow rates. The TPMS heat exchanger design has a high air-side pressure drop but it provides high heat transfer rates. This helps maintain a high outlet temperature during discharge, which is important to thermal comfort applications. The design, manufacturing, and experimental characterization of the TES device will be presented as part of this study. 

Presenting Author: Casey Troxler Embry-Riddle Aeronautical University

Presenting Author Biography: Casey Troxler received his bachelor's and master's degree in mechanical engineering from Embry-Riddle Aeronautical University in 2019 and 2022, respectively. He is currently pursuing his Ph.D. as a member of the Thermal Science Laboratory at the MicaPlex Research Park. Casey was an honorable mention for the Department of Energy, Innovations in Buildings (IBUILD) Fellowship in 2022 and a recipient of the ASHRAE Graduate Grant-in-aid award in 2023.

Authors:

Casey Troxler Embry-Riddle Aeronautical University
Thomas Freeman National Renewable Energy Laboratory (NREL)
Karl Morgan Embry-Riddle Aeronautical University
Adewale Odukomaiya National Renewable Energy Laboratory (NREL)
Sandra Boetcher Embry-Riddle Aeronautical University