I think you should read more, it is available online, you are missing the point.
Superconductor stacks are used instead of permanenet magnets in rotor, not as storage/battery, but compared to conductor coils, dissipation is reduced. Stator coils are also exchanged with supercondutive coils to reduce dissipation compared to conductor coils. In addition to increased efficiency, torque density is increased (i.e. motor size reduced for the same torque):
Superconductivity above room temperature is also not possible, the motor was build for the temperature range of 20K to 40K and tested at 30 K (-243 C), so I do not see how it could be done without cryogenics. And they call this high temperature superconductor (HTS) because it is not required to go close to absolute zero (-273 C), which would be even more complicated.
Battery/storage is independent topic. This team assumed that aircrafts start at first as hybrids with this motor and jet/turbine generator and then later as fully electric (i.e. on battery):
Superconductor stacks are used instead of permanenet magnets in rotor, not as storage/battery, but compared to conductor coils, dissipation is reduced. Stator coils are also exchanged with supercondutive coils to reduce dissipation compared to conductor coils. In addition to increased efficiency, torque density is increased (i.e. motor size reduced for the same torque):
Superconductivity above room temperature is also not possible, the motor was build for the temperature range of 20K to 40K and tested at 30 K (-243 C), so I do not see how it could be done without cryogenics. And they call this high temperature superconductor (HTS) because it is not required to go close to absolute zero (-273 C), which would be even more complicated.
Battery/storage is independent topic. This team assumed that aircrafts start at first as hybrids with this motor and jet/turbine generator and then later as fully electric (i.e. on battery):