Submitted:
07 December 2023
Posted:
07 December 2023
You are already at the latest version
Abstract
Keywords:
1. Introduction
2. Development of simulation modelling and the experimental setup
2.1. Cycle description and refrigerant flow state based on DE-VCR
2.2. Development of BTMS based on the direct refrigerant cooling
2.3. Developing the BTMS model for simulation
2.3.1. Modelling assumptions and working conditions
2.3.2. Geometries and grid
2.3.3. Heat transfer modeling and boundary conditions
2.4. Experimental setup
3. Results and discussions
3.1. Validations of the results and proof of temperature uniformity of BTMS-DRC
3.2. Influence of heat generations
3.3. Influence of the thermal conductivity
3.4. Influence of the convective heat transfer coefficients
3.5. Effect of refrigerant saturation temperature
4. Conclusions
- The simulated results (the module temperature) via the simulation agreed well with the experimental results. It was also found that the simulated results remained close to that experimental results when varying the operating conditions. The error from validation was around 2.9 – 7.2%.
- The simulated results also agreed well with the experimental results when focusing on the temperature uniformity of the module. The difference in temperature in the module did not exceed 5 °C (both simulations and experiments). This has shown that the BTMS-DRC is an alternative way to achieve the sufficient temperature uniformity. This is due to the advantages of the two-phase flow evaporation.
- For the parametric investigation via simulations, an increase in the battery heat generation caused the module temperature to increase. Therefore, the heat generation for indicating the working capacity of the BTMS must be consistent with the appropriate working temperature for Li-ion battery.
- For emphasizing the heat transfer mechanism, it was evident that the change in the convection heat transfer coefficient significantly affected the module temperature. Using a too low href resulted in producing a quite high module temperature. On the other hand, using a too high href has less impact on producing the lowest module temperature. This has shown that the href for design the BTMS-DRC must be carefully considered.
- Additionally, the change in the refrigerant saturation temperature significantly affected the module temperature even when the href was held constant. The investigation indicated that for a certain heat generation and href, the refrigerant saturation temperature should be as high as possible. This can provide an advantage to the refrigeration system.
Author Contributions
Funding
Data Availability Statement
Acknowledgments
Conflicts of Interest
Nomenclature
| AC | Alternating current |
| ARAC | Advanced refrigeration and air conditioning laboratory |
| BC | Boundary conditions |
| BTMS | The battery thermal management system |
| BHS | Battery heat simulator |
| COP | Coefficient of performance |
| DC | Direct current |
| DE-VCR | Dual-evaporator based vapour compression refrigeration system |
| DRC | Direct refrigerant cooling |
| EEV | Electric expansion valve |
| EVs | Electric vehicles |
| href | Convection heat transfer coefficient at the refrigerant side |
| k | Thermal conductivity |
| PID | Proportional integral derivative |
| RH | Relative humidity |
| Texp | Experimental temperature |
| Tmax | Maximum temperature |
| Tmid | Middle temperature |
| Tmin | Minimum temperature |
| Tsim | Simulation Temperature |
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| Point | Heat generation 100 W | Heat generation 200 W | Heat generation 300 W | ||||||
|---|---|---|---|---|---|---|---|---|---|
| Tsim | TEXP | %error | Tsim | TEXP | %error | Tsim | TEXP | %error | |
| a | 10.5 | 10.2 | 2.9 | 17.6 | 16.8 | 4.5 | 26.7 | 25.8 | 3.4 |
| b | 11.1 | 10.4 | 6.3 | 18.8 | 17.6 | 6.4 | 28.5 | 26.7 | 6.3 |
| c | 11.3 | 10.5 | 7.1 | 19.2 | 18.4 | 4.2 | 29.1 | 27.2 | 6.5 |
| d | 11.1 | 10.3 | 7.2 | 18.8 | 17.5 | 6.9 | 28.5 | 26.6 | 6.7 |
| e | 10.5 | 10.1 | 3.8 | 17.6 | 16.7 | 5.1 | 26.7 | 25.8 | 3.4 |
| f | 11.2 | 10.4 | 7.1 | 19.0 | 18.2 | 4.2 | 28.8 | 26.9 | 6.6 |
| g | 11.2 | 10.4 | 7.1 | 19.0 | 18.2 | 4.2 | 28.8 | 26.9 | 6.6 |
| h | 11.4 | 10.8 | 5.3 | 19.3 | 18.7 | 3.1 | 29.2 | 28.3 | 3.1 |
| i | 11.4 | 10.7 | 6.1 | 19.3 | 18.6 | 3.6 | 29.2 | 28.3 | 3.1 |
| j | 10.1 | 9.5 | 5.9 | 17.0 | 16.3 | 4.1 | 25.9 | 24.3 | 6.2 |
| k | 10.1 | 9.4 | 6.9 | 17.0 | 16.2 | 4.7 | 25.9 | 24.3 | 6.2 |
| Materials | k (W/m·K) | Tmid | Tmin | ∆Tmid/min |
|---|---|---|---|---|
| Silver | 430 | 28.5 | 26.4 | 1.9 |
| Copper | 390 | 28.6 | 26.8 | 1.8 |
| Aluminum Alloy-1060 | 215 | 29.2 | 25.9 | 3.3 |
| Brass | 110 | 30.2 | 25.1 | 4.1 |
| Steel | 45 | 34.5 | 21.1 | 13.4 |
| Stainless Steel | 15 | 38.2 | 18.4 | 19.8 |
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