Battery preheating and cooling integrated design system and method for electric aircraft
By designing the integrated battery preheating and cooling design system for electric aircraft, the battery temperature is dynamically controlled in real time, the thermal management problems arising from electric aircraft batteries during high-power charging are solved, the battery temperature is uniformized and the available energy is maximized, and the battery service life is extended.
Patent Information
- Application Number
- CN202210582168.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2022-05-26
- Publication Date
- 2025-03-25
- Estimated Expiration
- 2042-05-26
AI Technical Summary
During the high-power charging process of electric aircraft, the power battery module generates a lot of heat, resulting in an increase in the temperature difference between the inside and outside, affecting the battery performance, and uneven temperature distribution, resulting in battery life attenuation and inconsistent capacity, reducing available energy.
Design an integrated battery preheating and cooling design system, including a control unit, a heating unit, an air inlet regulation unit, a temperature detection unit and an air outlet regulation unit, and adjust the battery temperature through real-time dynamic control of heating or cooling, so as to achieve temperature uniformity and maximize available energy.
By achieving uniformization of battery temperature and dynamic optimization control, the available energy of the battery can be maximized and the service life of the battery can be extended.