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 system.weight only40 kg, compact size is 30cm (diameter)x28cm (length). The unit featuresEM-power patent-pending unique architecture, equipped with aviation standard (EASA and CAAC certified)and equipped with high-density patented winding technology, achieving aviation safetydual redundant power electronics system, usingliquid cooling.EMP30The performance parameters of the 0-T1000 are summarized asupshown in the table.

EMP300-T1000The motor control system with integrated inverter 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. In addition, the use of fast-switching silicon carbide(SiC) technology scalable modular electronics, combined with short shielded current paths, can achieve the highest performance required for high-torque aircraft propulsion systems.

EMP300-T1000 and aircraft systems are equipped withFive interfaces for connection. Two of these interfaces are for DC bus power cables, corresponding to positive and negative poles respectively.; The other two interfaces are for connecting the coolant inlet and outlet systems.system.Five interfaces for data cables.

In summary,EMP300-T1000The biggest advantage of the system lies in its high power density, high efficiency, and high volumetric power density, which allows the aircraft to have less aerodynamic drag, thereby saving extra energy for range or payload.!

Contact Informationintegratedconnection method:Mona (Mengna) Li / Li Mengna
tel: +86-13761171363, email: Mona@EMP-aviation.com