AIAA Propulsion and Energy 2019 Forum · 2019 · 31 citations · 6 references
EngineeringElectrical EngineeringMechanical EngineeringElectric MachinesMachine DesignPropulsionDirect Current MachinesElectric MotorsLosses In Electric MachinesMachine CoolingMachine WindingsSuperconducting MaterialsCryogenic CoolingCryogenic Cooling SystemsCryogenic EngineeringCryogenic SystemsElectric Motor CoolingElectrical LossesMechanical LossesRotor Cooling
Some of the challenges associated with developing electric aircraft propulsion systems include developing powertrain components that are both efficient and light-weight. In particular, electric motors must simultaneously achieve high efficiency by minimizing electrical and mechanical losses while also achieving high specific power by increasing the torque and/or speed. Normally, increasing torque or speed will increase electrical and mechanical losses. The High Efficiency Megawatt Machine (HEMM) minimizes electrical losses by incorporating a superconductor to enable increased current on the rotor. The rotor spins in a vacuum to minimize thermal and mechanical losses. Some organizations have been developing superconducting rotors for similar reasons using either cryogenic fluid transfer systems, fully immersed cryogenic cooling, and in a few cases, built-in cryogenic cooling on the rotor using a Brayton or Stirling system; however, the implementation was too large or inefficient for effective motor integration. Instead, a new approach for cryogenically cooling the superconducting rotor coil with an embedded rotating cryocooler is presented that fits completely within the rotating shaft.
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High Efficiency Megawatt Motor Preliminary Design
Ralph Jansen, Peter Kascak, Rodger Dyson et al. · AIAA Propulsion and Energy 2019 Forum · 2019 · 52 citations · Full text
Engineering, Aerospace Engineering, Electrical Engineering +16