An aircraft power battery, an aircraft, and an aircraft power battery integrated power supply method are provided. One battery box is accommodated in each separate compartment. The battery boxes in each row or column of separate compartments being connected in series and then being connected to a battery management system (BMS) module, forming a plurality of battery paths which are then connected in parallel, before supplying power to the aircraft. The method ensures power supply reliability and achieving the integrated arrangement of the limitation and integration of battery packs and battery management system, avoiding the occurrence of high working current and overheating of wire harness caused by scattered layout of each battery pack in the cabin, and is conducive to installation and maintenance. In addition, a cooling bottom plate is equipped for the power battery to ensure heat dissipation performance.
AIRCRAFT POWER BATTERY, AIRCRAFT, AND AIRCRAFT POWER BATTERY INTEGRATED POWER SUPPLY METHOD
2025-05-29
Patent
Electronic Resource
English
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