EMP600-T2000
EMP600-T2000can output360 kW continuous power and600 kW peak power. Its continuous torque reaches1400 Nm, with a peak torque of2000 Nm.The weight of this integrated unit includes the motor, inverter, and cooling systemWeight only70 kg, with a compact size of 30cm (diameter)×28cm (length). This unit featuresEM-power's patent-pending unique architecture, equipped with EASA and CAAC certified aviation standardsand equipped with high-density patented winding technology, achieving aviation safetydual redundant power electronics system, usingliquid cooling.A summary of the performance parameters for the EMP600-T2000 isuppershown in the table.
EMP600-T2000The motor control system with integrated inverter provides dual redundancy for aviation safety. This integrated system features a design with minimal distance between the motor and integrated control electronics, minimizing losses and maximizing efficiency. Additionally, the use of fast-switching silicon carbide(SIC) technology's scalable modular electronics, combined with short shielded current paths, can achieve the highest performance required for high-torque aircraft propulsion systems
EMP600-T2000 and the aircraft system are equipped withFive interfaces for connection. Two of these interfaces are for the DC bus power lines, corresponding to positive and negative poles respectively.; The other two interfaces are for connecting the coolant inlet and outlet systems.
system.TheFive interfaces for data lines.
In summary,EMP600-T2000The system's main advantages lie in its high power density, high efficiency, and high volumetric power density, which result in lower aerodynamic drag for the aircraft, thus saving extra energy for range or payload.!
Contact InformationConnectConnection method:Mona (Mengna) Li / Li Mengna
tel: +86-13761171363, email: Mona@EMP-aviation.com