EMP300-T1000
The EMP300-T1000 is capable of producing 150 kW continuous power and 300 kW peak power. It generates a Torque of 600 Nm continuous and 1000 Nm peak. The weight of this integrated unit consists of motor, inverter and cooling system is 40kg, and its compact volume is 30 cm (diameter) by 25.5 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.
EMP300-T1000 can output 150kwcontinuous power and300kwpeak power. Its continuous torque reaches600Nm, with a peak torque of1000Nm.The weight of the integrated device includes the motor, inverter, and cooling systemweighing only40kg, with a compact size of30cm(diameter)×25.5cm (length). The unit adoptsEM-POWERpatent-pending unique architecture, equipped with aviation standards (EASA and CAAC certification)and is equipped with high-density proprietary winding technology, achieving aviation safetyoftripleredundant power electronics system, usingliquid cooling.EMP30Summary of 0-T1000 performance parametersonas shown in the table.
The EMP300-T1000 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.
EMP300-T1000the motor control system with integrated inverter provides for aviation safetythreetriple redundancy. The integrated system uses a design with minimal distance between the motor and the integrated control electronics, minimizing losses and improving efficiency. In addition, it uses fast-switching silicon carbide (SIC) technology scalable modular electronics, combined with short shielded current paths, achieve the highest performance required for high torque aircraft propulsion systems.
There are five interface connections from the EMP300-T1000 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.
EMP300-T1000 and the aircraft system are provided withfiveinterface connections. Two of them are for DC bus power cables, corresponding to positive and negative poles respectively; The other two interfaces are for connecting the cooling fluid in and out of the system.No.fiveinterfaces for the data cable.
In comparison with the EMRAX348 specs, the EMP300-T1000 shows advantages in weight, size, and performance leading to more payload and range performance for the aircraft. It should also be noted that the EMP300-T1000 has integrated triple redundant control vs the (extra) external control (i.e., inverter) needed for EMRAX348. In summary, the core advantage of the EMP300-T1000 system is in its high power density and efficiency, saving additional energy which would be needed for aircraft range and/or payload!
andEMRAX348compared to the specs ofEMP300-T1000It demonstrates advantages in weight, size, and performance, thereby bringing greater payload and range performance to the aircraft. It should also be noted thatEMP300-T1000integrated triple redundant control, whileEMRAX348requirestoexternal control (i.e., inverter). In summary,EMP300-T1000The core advantage of the system lies in its high power density and efficiency, saving aircraft range and/or additional energy required for payload!
Contact InformationUnioncontact method: Mona (Mengna) Li / Li Mengna
tel: +86-13761171363, email: Mona@EMP-aviation.com