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Development of a 8 kW HTS Axial Flux Machine for Electric Aircraft Propulsion*
Min Zhang1, Jie Sheng1, Jay Patal1, Weijia Yuan1, Fred Eastham1, Xing Dong1, Frederick Berg2
1University of Bath, United Kingdom, 2Airbus Group Innovations, United Kingdom
This work is supported byunder grant: developing fully HTS machines for future electric aircraft
Short term:
• AC loss in rotational magnetic fields has a significant impact on the weight and cost of cooling system
• Experimental and numerical tools required
• AC loss minimization
Long term:
• Flight profile affects machine design
• Impact of air turbulence
……
Challenges for fully HTS machines
Three objectives:
1. To characterise AC losses in a machine environment
2. To investigate new ways to reduce AC losses
3. To study the impacts of flight profile to the machine performance
8 kW HTS Axial Flux Machine project
8 kW HTS Axial Flux Machine project
Strucutre Performance
Rotor diameter 187.5mm Peak phase current 30A
Air gap 60mm Average phase current 21.21A
Stator inner diameter 175mm Maximum torque 32Nm
Turns per coil 60 Speed 1500RPM
Coil per phase 2 Average power 8kW
Width of tape 4mm Air-gap field 0.4T
Total length 20m Volume 0.15m3
2G HTS double pancake stator coils:Material 4 mm 2G HTS
Self field Ic 120 A
Total turns 60
Total length 20 m
Inner diameter 175 mm
Coil Ic 71 A
Insulation Heat shrink tube
Calculated coil Ic under 0.5 T field is 44.4 AMeasured coil Ic without external field is 71 A
8 kW HTS Axial Flux Machine project
NdFeB rotor design:
60 mm airgap, peak airgap field is about 0.4 T
8 kW HTS Axial Flux Machine project
AC loss measurement: Calorimetric chamber
8 kW HTS Axial Flux Machine project
• Measuring the boil-off rate of LN2• Background flow is minimised by a
double-cryostat design
Glass-metal sealing test:
N Grease + Indium
AC loss test steps:1. Heater calibration2. Background flow rate determination3. Transport loss measurement 4. Magnetization loss with rotational magnetic fields5. Total loss with AC current and rotational fields
8 kW HTS Axial Flux Machine project
Base Frame
Speed
Pickup10 kW Dynamometer
DC power supply
Real time digital simulator
Rotor position
Power
ABB drive
*Superconductor Science and Technology 28 (11), 115011
AC loss reduction investigation:1. Striated 2G HTS* coil2. Roebel cable coil
8 kW HTS Axial Flux Machine project
*AC loss comparison between multifilament and nonstriated YBCO coils designed for HTS propulsion motors, IEEE Transactions on Applied Superconductivity, 27 (4), 5203005
Aircraft propulsion hardware-in-the-loop test:
8 kW HTS Axial Flux Machine project
Base Frame
Speed
Pickup10 kW Dynamometer
DC power supply
Dynamic torque
simulation
Real time digital simulator
Wind turbulence
model
Propeller model
Measured
Speed/torque
Simulated
torque
Hardware-in-loop test
Flight profile
Power
Rotor position
ABB drive
A new 3D 2G HTS model using T-A formula*:
*Huiming Zhang et al 2017 Supercond. Sci. Technol. 30 024005
HTS machine modelling
A fast 3D HTS coil model using T-A formula*:
20 turns double racetrack coil
NoD: 786245
Time: 4 hours
CPU: i7-4790@ 3.6GHz
*An efficient 3D finite element method model based on the T–A formulation for superconducting coated conductors, 2017 Supercond. Sci. Technol. 30 024005
Six filament roebel cable
NoD: 58440
Time: 20 mins
CPU: i7-4790@ 3.6GHz
HTS machine modelling
Shaft design:
8 kW HTS Axial Flux Machine project
Deflection at bearing points < 0.5 degrees
• PM force exceeding 2.5kN• Necessary to ensure shaft
bending does not interfere with cryogenic bearing operation
Calculated total AC losses:
(Angle is the phase difference
between the applied current and
magnetic field)
HTS machine modelling