Low-Altitude Flight Cell (50Ah)
Key Characteristics:
Single Cell Energy Density: 310Wh/kg
System-level Energy Density: 270wh/kg
Cell Chemistry: High-nickel NCM
Ultra-High Energy Density
Single-cell energy density: 310 Wh/kg; System-level energy density:270Wh/kg
Significantly surpasses the average energy density of automotive-grade batteries
Enables eVTOL aircraft to achieve a range of up to 300 kilometers
Supports long-distance missions and prolonged airborne operations
Enhances the practicality and flexibility of aerial vehicles
High Discharge Rate
Designed to meet the stringent power demands of emergency maneuvers and rapid ascents
Supports a continuous 6C discharge rate
Capable of sustaining 120 seconds of discharge at 30% State ofCharge (Soc)
Provides robust and immediate power support for eVTOL operations
Safety and Reliability
Incorporates three innovative technologies to enhance ion mobility and reduce battery failure risks
Facilitates compliance with rigorous aviation airworthiness certifications
Employs advanced low-impedance solid-liquid interface and high-safety high-nickel chemistry technologies
Lightweight Design
Addresses the critical weight sensitivity of low-altitude aircraft
Utilizes a novel lightweight metal casing combined with a thickness-gradient top cover design
Achieves a structural weight reduction of 60 grams
Results in an overall battery weight decrease of approximately 40%
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