EMP600-T2000
The EMP600-T2000 is capable of producing 360 kW continuous power and 600 kW peak power. It generates a Torque of 1400 Nm continuous and 2000 Nm peak. The weight of this integrated unit consists of motor, inverter and cooling system is 70kg, and its compact volume is 30 cm (diameter) by 37.5 cm (length). Configured in the EM-POWER patent-pending unique architecture with power-electronics satisfying aviation standards (certifiable by EASA and CAAC), complete with high-density proprietary winding technology, designed with triple redundancy. This unit is liquid cooled. The performance specs summary of this integrated system is shown below.
EMP600-T2000can output360kwcontinuous power and600kwPeak power. Its continuous torque reaches1400Nm, peak torque is2000Nm.The weight of this integrated device includes the motor, variable frequency drive, and cooling systemWeight only70Kg, compact size of30cm(diameter)×37.5cm(length). This unit adoptsEM-POWERPatent-pending unique architecture, equipped with aviation standards (EASA and CAAC certified)and equipped with high-density proprietary winding technology to achieve aviation safetyoftripleredundant power electronic system, usingliquid cooling.Summary of EMP600-T2000 performance parameters is asupas shown in the table.
The EMP600-T2000 electric machine with integrated inverter for motor control offers triple redundancy for aviation safety. The integrated system is designed with minimum distance between the electric machine and the integrated control electronics which minimizes loss and maximizes efficiency. Further, the scalable modular electronics with fast switching Silicon Carbide (SIC) technology combined with short shielded current paths yield highest performance required for high torque aircraft propulsion.
EMP600-T2000The motor control system with integrated inverter provides aviation safetythreeheavy redundancy. The integrated system adopts a design with the minimum distance between the motor and the integrated control electronics, minimizing losses and improving efficiency. In addition, it uses fast-switching silicon carbide (SIC) technology's scalable modular electronics, combined with short shielded current paths, enable the highest performance required for high-torque aircraft propulsion systems.
There are five interface connections from the EMP600-T2000 to the aircraft system. Two of them are for DC BUS power cables, one positive and one negative. Two of them are for cooling fluid connections in- or out- to the system. The fifth connection is for the data cable.
Between the EMP600-T2000 and the aircraft system, there isfiveinterface connections. Among them, two interfaces are used for the DC bus power lines, corresponding to the positive and negative poles respectively; The other two interfaces are used to connect the coolant inlet and outlet system.No.fiveinterfaces for data cables.
For a 500 to 600KW-level system, EM-POWER solution is 55% less weight / KW, 75% lower volume / KW, 40% less energy loss / KW! for500 - 600KW class system, EM-POWER solution reduces weight by 55%, volume by 75%, and energy loss by 40% per kilowatt compared to competitors!
In summary, the core advantage of the EMP600-T2000 system is in its high power density, efficiency, and the high volumetric power density which translates to less aerodynamic drag, saving additional energy for range or payload!
In summary,EMP600-T2000The system's greatest advantage lies in its high power density, high efficiency, and high volumetric power density, which reduces the aircraft's aerodynamic drag, thereby saving additional energy for range or payload!
Contact Informationconnectionconnection method:Mona (Mengna) Li / Li Mengna
tel: +86-13761171363, email: Mona@EMP-aviation.com