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Figure 1. Axial-flux and radial-flux electrical machine topologies considered Figure 2 Project work package structure a) Double air gap axial-flux topology, 4 rotor discs b) 4 x 3-phase phase modular wound radial-flux topology Laminated stator Stator coils Magnet array Rotor backiron

Stator Laminated stator ·  · 2016-11-16Winding hotspot Average winding Lowest winding Magnet Stator back iron Housing 0 1800 3600 5400 7200 9000 20 40 60 80 100 120 140 Time [secs]]

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Figure 1. Axial-flux and radial-flux electrical machine topologies considered

Figure 2 Project work package structure

a) Double air gap axial-flux topology, 4 rotor discs b) 4 x 3-phase phase modular wound radial-flux topology

Laminated stator

Stator coils

Magnet array

Rotor backiron

a) Radial-flux topology model in MOTORCAD software b) Axial-flux topology thermal analysis tool

Figure 4 Developed lumped parameter thermal models for fault-tolerance electrical machine

topologies considered

`

Figure 3 Software suite sub-elements and interactions

a) Experiment b) Model

Figure 5 Initial validation of modelling software against test data from a fault tolerant machine

ETR-ES Evaluation Software ETR-MDS Motor Design Software Suite

(MATLAB)

(MATLAB, Motor-CAD)

a) Example test motorettes used, before and after life testing

b) End of life criteria established from accelerated ageing tests

Figure 6 Accelerated ageing testing of high temperature class insulation systems

Figure 7 Computational fluid dynamics studies used to analyse convective heat transfer

a) Heat transfer test bench b) Example winding assembly used in thermal tests

Figure 8 Experimental investigation of conductive heat transfer from the winding

Temperature controlled cooling unit

DC power supply

Data acquisition system

Thermally insulated testing chamber

Power loss measurement

a) Investigation of tail rotor cooling b) Cooling fin profile optimisation

Figure 9 Example model based comparison of axial-flux and radial-flux designs over a mission cycle

a) Flux model b) Winding AC loss study c) Rotor eddy current loss study

Figure 10 Example electro-magnetic finite element analyses undertaken during the design development

TABLE I PERCENTAGE WEIGHT BREAKDOWN OF

ACTIVE MATERIAL USED IN THE TWO PROTOTYPE

DESIGNS

Active component Axial-

flux

Radial-

flux

Stator core 40 % 34 %

Winding copper 36 % 32 %

Permanent magnet 24 % 25 %

Rotor back iron N/A 9 % a) Axial-flux housing b) Radial-flux assembly

Figure 11 Axial-flux and radial-flux motor concepts

0

20

40

60

80

100

120

140

160

180

0 1500 3000 4500 6000 7500 9000

Tem

per

atu

re [o

C]

Time [secs]

Winding hotspot

Average winding

Lowest winding

Magnet

Stator back iron

Housing

0 1800 3600 5400 7200 900020

40

60

80

100

120

140

Time [secs]

Te

mp

era

ture

[o

C]

Max winding

Mid slot

Min winding

End winding

Tooth tip

Tooth body

Back iron

Rotor

Case

a) Full assembly mounted on plinth b) Stator lamination pack and winding

Figure 12 Axial-flux prototype

a) Full machine mounted on plinth b) Wound stator assembly c) Rotor assembly

Figure 13 Radial-flux prototype

4 quadrant dynamometer Inverter supplies

Torque (pk.) 2000 Nm Channels 4

Speed 4500 rpm Cont. ratings

250 Arms

Cont. power 225 kW 130 kVA

Peak power 340 kW Peak rating 350 Arms

Electrical supply system PWM frequency

2-16 kHz

Voltage 48-380 Vdc

Current 1000 Adc

Cont. power 350 kW

a) Test rig schematic b) System specifications

Figure 14 Test rig schematic and specification

Figure 15 Photograph of integrated test installation in dedicated laboratory

a) Control room dashboard b) Accuracy of installed instrumentation

Figure 16 Control and instrumentation of test facility

Electrical measurement cluster

Inverter drive control dashboard

Camera display of test cell

Central data acquisition and control panels

Equipment Channels Function Accuracy

HBM T40B 3000 Nm torque transducer

1 Shaft torque and speed

0.05 %

LEM LF505 500 A current transducers

12 Current measurement

0.6 %

HBM Genesis 7TA data acquisition system

24

Isolated voltage channels

0.05 %

3-phase power 0.2 %

Agilent 34980A data acquisition unit

80 Temperature from thermocouples (K)

<1oC

48-380 V 1000 A DC

supply motor-generator set

2000 Nm, 4500 rpm

dynamometer load

machine

Motor

under test

Inverter supply to

motor under test

Instrumentation

cabinet

Cooling

air supply

a) Axial-flux prototype b) Radial-flux prototype

Figure 17 Open circuit loss characteristics and breakdown

a) Recorded temperatures b) Loss breakdown

Figure 18 Example continuous sustained output measurement on radial-flux prototype

a) Plot of slot temperatures

b) Balance of phase currents and voltages

Figure 19 Mission cycle test Figure 20 Analysis of sustained faulted operation

a) Model b) Test

Figure 21 Example comparison of calibrated electrical machine model with test measurements

0 1800 3600 5400 7200 90000

20

40

60

80

100

120

140

160

Time [secs]

Te

mp

era

ture

[o

C]

Max winding

Winding front of slot

Winding back of slot

End winding

Tooth tip

Tooth body

Back iron

Rotor

Case