Electric Propulsion for Air Mobility

Case History

High performance propulsion drivetrains for all electric, hybrid and eVTOL future aircrafts

FULL ELECTRIC PROPULSION MOTOR

The ET-6 high-density electric propulsion motor, engineered by PMC, matches the power output of a PT6 turboshaft with only 115 kg of mass. It maintains the same propeller interface and reaches speeds of up to 2200 rpm, with peak power exceeding 750 kW.

Thanks to its direct connection to the propeller, the ET-6 eliminates the need for a gearbox. The only components requiring maintenance are grease-lubricated hybrid bearings, inspected after 5000 hours of operation.

The rotor uses permanent rare-earth surface magnets, secured by a preloaded carbon fibre ring. This ensures constant compression, even under overspeed conditions, increasing safety and durability.

Additionally, the titanium alloy shaft reduces weight while maintaining strength. Its hollow structure houses the governor mechanism, optimizing space. To minimize lubrication needs, the ET-6 uses hybrid angular contact preloaded ball bearings.

The high-efficiency liquid cooling system surrounds the stator, while the rotor remains uncooled, simplifying thermal management. Moreover, all structural components are made of high-strength light alloys, precisely machined from solid blocks without welds or castings.

From an electrical perspective, civil aviation adopts automotive-grade standards with battery voltages ranging from 850 to 650 VDC. This approach leverages the wide availability of optimized semiconductors. However, a 2000 VDC standard for large aircraft may emerge in the future.

To enhance safety and system availability, the ET-6 divides its motor winding into four independent sections. Each section operates as a separate motor, limiting current to 400 A per unit. Consequently, this design improves redundancy and optimizes drive size for better reliability.

Electric propulsion for air mobility
Electric propulsion for air mobility

PARALLEL HYBRID PROPULSION MOTOR

Frameless hybrid permanent magnet motors are specifically designed for direct installation on the propeller axis, which connects to an IC or turboshaft engine. During take-off, the combined power of the IC engine and the electric motor—fed by a compact battery—delivers the necessary starting force.

The motor features a slim ring design without bearings and uses external cooling. Permanent FeNdB magnets sit on the rotor’s surface, firmly held by a preloaded carbon fibre ring. The stator includes two independent windings, enabling control through two separate drives.

Electric propulsion for air mobility
Electric propulsion for air mobility

COMPACT DRIVES FOR AVIONICS PROPULSION

High-Power Inverter for Electric Propulsion

  • Three-phase inverter, capable of 400 A continuous at 800 VDC.
  • Water/ethylene glycol cooling (maximum 50% ethylene glycol) with a nominal flow rate of 10 L/min.
  • SiC MOSFET technology, optimized for high efficiency at high switching frequencies.
  • Integrated current sensors for precise power management.
  • Modular and synchronized drives, enabling high-power applications.
  • Weight: 10 kg (TBC)Dimensions: 250x150x250 mm (TBC).
  • Power management: Handles 370 kVA at 800 VDC (typically 340 kW if cos-phi ≥ 0.9).
  • Power density: 117 kW/kg and 90 kW/dm³.
  • Advanced safety features, including dual-channel Safe Torque Off and overtemperature, overvoltage, and overcurrent protections.
  • Selectable PWM frequencies: 2 kHz to 64 kHz for flexible control.
  • Supports multiple motor control interfaces, including CAN, CANOpen, EtherCAT, and proprietary EtherPMC.
AXS Series
AxS 500