Design of a Compact Thermal Management System for a High-Power Silicon Carbide Traction Inverter

2021 ◽  
Author(s):  
Jigar Mistry ◽  
Yicheng Wang ◽  
Peter Azer ◽  
Berker Bilgin
Heliyon ◽  
2021 ◽  
pp. e07773
Author(s):  
Danial Karimi ◽  
Md Sazzad Hosen ◽  
Hamidreza Behi ◽  
Sahar Khaleghi ◽  
Mohsen Akbarzadeh ◽  
...  

2021 ◽  
Vol 183 ◽  
pp. 116240 ◽  
Author(s):  
Hamidreza Behi ◽  
Mohammadreza Behi ◽  
Danial Karimi ◽  
Joris Jaguemont ◽  
Morteza Ghanbarpour ◽  
...  

2021 ◽  
Vol 185 ◽  
pp. 116449
Author(s):  
Danial Karimi ◽  
Hamidreza Behi ◽  
Md Sazzad Hosen ◽  
Joris Jaguemont ◽  
Maitane Berecibar ◽  
...  

2015 ◽  
Vol 8 (1) ◽  
pp. 60-71
Author(s):  
Charles E. Oberly ◽  
Michelle Bash ◽  
Benjamin R. Razidlo ◽  
Travis E. Michalak ◽  
Fernando Rodriguez

1988 ◽  
Author(s):  
J. KU ◽  
E. KROLICZEK ◽  
M. MCCABE, JR. ◽  
S. BENNER

2014 ◽  
Vol 556-562 ◽  
pp. 265-269
Author(s):  
Bo Wang ◽  
Yu Ming Nie ◽  
Zhan Ji Yin ◽  
Zhi Tong He

According to the operating characteristics of high-power battery pack in practical application, the effects of four factors, which include operating load, state of charge (SOC), ambient temperature and operating temperature, on the temperature uniformity and rising rate of battery pack under natural convection were studied based on Arbin test bench. The results indicate that: the operating load and SOC of battery pack doesn’t affect its temperature uniformity, which was deteriorated as the increasing of operating temperature of battery pack, or improved as the increasing of ambient temperature when the other factor is kept constant. The increment of operating load or ambient temperature could result in a higher temperature rising rate, while the increasing of SOC or operating temperature could lead to a lower temperature rising rate, when the other three factors are kept constant. When the operating temperature or temperature differences achieved threshold value, thermal management system should choose proper extent of forced flow and flow field in accordance with the battery pack’s current operating conditions, in order to ensure the economy of the thermal management system.


Energies ◽  
2020 ◽  
Vol 13 (9) ◽  
pp. 2177 ◽  
Author(s):  
Miao Zhao ◽  
Liping Pang ◽  
Meng Liu ◽  
Shizhao Yu ◽  
Xiaodong Mao

With the continuous application of high-power electronic equipment in aircraft, highly efficient heat transfer technology has been emphasized for airborne applications. In this paper, a thermal management system based on an antifreeze liquid cooling loop and a vapor compression refrigeration loop is presented for high-power airborne equipment in a helicopter. The simulation models of the thermal management system are built in order to study its control strategy for the changing flight conditions. The antifreeze-refrigerant evaporator and air-refrigerant condenser are specially validated with the experimental data. A dual feedforward proportion integration differentiation and expert control algorithm are adopted in the inlet temperature of the cold plate and sub-cooling control of the refrigerant by regulating the compressor speed and the fan speed, respectively. A preheating strategy for antifreeze is set up to decrease its flow resistance in cold day conditions. The control strategy for the thermal management system is finally built based on the above control methods. In this paper, two extreme conditions are discussed, including cold and hot days. Both the simulation results show that the superheated, sub-cooling and antifreeze inlet temperature of the cold plate can be controlled at 3 to8 °C, −10 to −3 °C and 18 to22 °C, respectively. Under the same changing flight envelope, the coefficient of performance of the vapor compression refrigeration loop is relatively stable on the cold day, which is about 6, while it has a range of 2.58–4.9 on the hot day.


2008 ◽  
Author(s):  
Kimberly R. Wrenn ◽  
David A. Wolf ◽  
Mohamed S. El-Genk

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