Search

Against the backdrop of "carbon peak and carbon neutrality," the hydrogen and fuel cell vehicle industry are rapidly developing. Within the on-board hydrogen supply system, the hydrogen circulation pump serves as an essential component of the hydrogen fuel cell system. The spiral disk, as a core part of the hydrogen fuel cell system's vortex hydrogen circulation pump (VHCP), plays a crucial role in determining the performance of the hydrogen circulation system in hydrogen fuel cell vehicles. To meet the requirements for high-performance and high-reliability development of the hydrogen circulation pump, the VHCP scheme is adopted as the choice for the hydrogen pump solution. Through the magnetic suspension and no connection shaft structural design, the feasibility of applying the high speed and high flow hydrogen turbine was initially validated. Utilizing Fluent analysis software and high precision performance test bench, a comprehensive three-dimensional numerical simulation of the turbine design under various operating conditions was conducted and performance test verification, demonstrating that the performance meets the required specifications. By conducting research in both strength optimization design and performance requirement, two major technical challenges in turbine pump application were overcome. Combined with the experimental results of the turbine medium, it is concluded that the vortex pump can meet the flow and pressure rise under the premise of low power consumption in the hydrogen circulation system so as to perfectly increase the hydrogen return amount. Based on these findings, recommendations are proposed for the future development direction of hydrogen supply systems in hydrogen fuel cell vehicles. [ABSTRACT FROM AUTHOR]

The fast refueling of compressed hydrogen has an important influence on the efficiency and safety of the filling process. Precision measurements of the thermodynamic characteristics of hydrogen under the filling process are becoming more important as hydrogen energy is developed and used. One of the key elements of hydrogen fuel cell vehicles is the on-board hydrogen storage cylinder (HSC). Due to the compression of the hydrogen during filling, there could be a fast increase in temperature. The tank's maximum temperature and maximum fueling pressure are both restricted to less than 358.15 K and 125% of the tank's design pressure for safety reasons. This study revealed the hydrogen temperature rise during refueling and developed a theoretical model for computing the temperature rise in the HSC during the high-pressure refueling procedure. The HSC filling procedure was examined using a theoretical approach. Also, the relationship between the refueling procedure and the temperature change of hydrogen in the type IV tank was investigated. The temperature evolution mechanism of various HSCs was explained, and predictions were made for the minimum precooling temperature needed for hydrogen under various filling scenarios. The results of the theoretical analysis gave a theoretical foundation to the present method for controlling the hydrogen temperature of the gas source in the hydrogenation station, which then enables us to determine the optimum amount of energy needed for cooling hydrogen in the hydrogen refueling station. [ABSTRACT FROM AUTHOR]