EMP300-T1000
EMP300-T1000 can output 150 kW continuous power and300 kW peak power. Its continuous torque reaches 600 Nm, and its peak torque is 1000 Nm.The weight of this integrated unit includes the motor, inverter, and cooling systemweight of only40 kg, with a compact size of 30cm (diameter)x28cm (length). This unit adoptsEM-power's patent-pending unique architecture, equipped with EASA and CAAC certified aviation standardsand incorporates high-density patented winding technology to achieve aviation safety.dual redundant power electronics system, adoptingliquid cooling.EMP30The performance parameters of the 0-T1000 are summarized asonshown in the table.
EMP300-T1000The integrated inverter motor control system provides dual redundancy for aviation safety. This integrated system adopts a design with minimal distance between the motor and integrated control electronics, minimizing losses and improving efficiency. Furthermore, it utilizes fast-switching Silicon Carbide (SiC) technology's scalable modular electronics, combined with short shielded current paths, achieve the highest performance required for high-torque aircraft propulsion systems.
EMP30between the 0-T1000 and the aircraft system.fifth interfaces. Two of these interfaces are for the DC bus power lines, corresponding to the positive and negative poles respectively.; The other two interfaces are for connecting the coolant inlet and outlet system.
system.theFiveinterfaces for data lines.
In summary,EMP300-T1000The system's main advantages lie in its high power density, high efficiency, and high volumetric power density, which results in lower aerodynamic drag for the aircraft, thus saving extra energy for range or payload.!
Contact Informationconnectedsystem connection:Mona (Mengna) Li / Li Mengna
tel: +86-13761171363, email: Mona@EMP-aviation.com