KGPS KGPS M2Or2A-02 [Invited] Design of MW-Class Ship Propulsion Motors for US Navy by AMSC Swarn S. Kalsi Kalsi Green Power Systems Princeton, NJ, USA 2019 ICMC Superconducting Rotating Machines 1
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Design of MW-Class Ship Propulsion Motors for US Navy by AMSC
Swarn S. KalsiKalsi Green Power Systems
Princeton, NJ, USA
2019 ICMC Superconducting Rotating Machines 1
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List of Published Reference
THIS PRESENTATION IS BASED ON THE FOLLOWING AMSC (AND OTHERS) PUBLIC INFORMATION• Kalsi, S.S. ,”Applications of High Temperature Superconductors to Electric Power Equipment”, IEEE/Wiley, ISBN 978-0-470-16768-7, 2011 • B. Gamble , G. Snitchler and T. MacDonald, “Full Power Test of a 36.5 MW HTS Propulsion Motor”, IEEE Transactions on Applied Superconductivity (
Volume: 21 , Issue: 3 , June 2011 ), pages:1083-1088• S.S. Kalsi, D. Madura, G. Snitchler, M. Ross, J. Voccio and M. Ingram, “Discussion of Test Results of a Superconductor Synchronous Condenser on a Utility
Grid”, Applied Superconductivity, IEEE Transactions on , Volume: 17 , Issue: 2 , Year 2007• S. S. Kalsi, D. Madura, M. Ross, M. Ingram, R. Belhomme, P. Bousseau and J-Y. Roger, ‘Operating Experience of a Superconducting Dynamic Synchronous
Compensator’, Paper No. A1-108, CIGRE Session 2006 in Paris • Kalsi, S.S.; Gamble, B.B.; Snitchler, G.; Ige, S.O.; “The status of HTS ship propulsion motor developments”, Power Engineering Society General Meeting,
2006. IEEE, 18-22 June 2006 Page(s):5 pp. , Digital Object Identifier 10.1109/PES.2006.1709643• Kalsi, S.; Madura, D.; MacDonald, T.; Ingram, M.; Grant, I.; “Operating Experience of Superconductor Dynamic Synchronous Condenser”, PES TD 2005/2006,
May 21-24, 2006 Page(s):899 – 902• Kalsi, S.S.; Henderson, N.; Gritter, D.; Nayak, O.; Gallagher, C.; “Benefits of HTS technology to ship systems”, Electric Ship Technologies Symposium, 2005
IEEE, 25-27 July 2005 Page(s):437 – 443, Digital Object Identifier 10.1109/ESTS.2005.1524712• Snitchler, G.; Gamble, B.; Kalsi, S.S.; “The performance of a 5 MW high temperature superconductor ship propulsion motor”, Applied Superconductivity,
IEEE Transactions on, Volume 15, Issue 2, Part 2, June 2005 Page(s):2206 – 2209, Digital Object Identifier 10.1109/TASC.2005.849613 • Haran, K.; Kalsi, S.S.; Arndt, T.; Karmaker, H.; Badcock, R.; Buckley, R.; Haugan, T.; Izumi, M.; Loder, D.; Bray, J.; Masson, P.; Stautner, W.; “High Power Density
Superconducting Rotating Machines – Development Status and Technology Roadmap”, Supercond. Sci. Technol. 30, (2017) 123002 (41pp)• Kalsi, S.S., Hamilton, K.A. and Badcock, R.A., “Superconducting rotating machines for aerospace applications”, Presented at AIAA Conference, Cincinnati,
OH, 2018
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Superconducting Rotating MachinesOUTLINE• Possible applications• Superconductors• SC Machine Configurations• Low Speed SC Machines• Outlook
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POSSIBLE SUPERCONDUCTORS FOR APPLICATIONS
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Types of Superconductors
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• LTS – NbTi and Nb3Sn• Operate at ~ 5 K• Cooled with liquid helium• Moderate field• Low cost
• HTS – BSCCO and ReBCO
• Operate at ~ 20 – 77 K• Cooled with LH2, LNe, LN2 and Refrigerators• Very high fields• High Cost
Bi2 Sr2 Ca2 Cu
3 O
LTS HTS
LTS are used in MRI and High Field Magnets
YBa2Cu3O7
HTS have still to find a niche application
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SC MACHINE CONFIGURATIONS
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SuperconductingConventional
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Superconducting (SC) Machine Configuration
• Majority of machines are synchronous type employing SC for the DC field winding• Until the nineties, most machines were built with NbTi (low temperature
superconductors – LTS)• Nineties onwards, High Temperature Superconductors (HTS) became favorite• Majority of the SC machines have DC excitation winding on the rotor• In a few applications, DC excitation winding is on the stator and rotor carries AC
armature winding• Low speed machines are used for Ship Propulsion and Wind Turbine applications
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Only HTS based machines are discussed in this presentation
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Key Components of HTS Rotating Machines
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Back Iron
Exciter
HTS Rotor Coil
Copper Stator Coil,
Connected to Terminals
E-M shield
Most commonly used configurations: HTS field winding and Copper armature winding
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What makes HTS Machines attractive?
Features making such machines attractive are;• Compact size• Light weight• Ability to supply reactive power (MVARs) up
to full MVA rating (both leading and lagging)• Virtually no harmonics in the terminal
voltage• Improved rotor life – elimination of thermal
load cycling of field winding current changes• Higher efficiency – under partial and full-load
operations• Lower vibrations and noise
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Ability to operate over the whole dynamic range of P and Q powers enhances dynamic stability of the machine and the system
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What makes HTS Machines attractive?Harmonics generated inside an HTS synchronous machine are extremely small as shown below;
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Harmonics generated byfield winding in stator
Harmonics generated by stator AC windingon the rotor surface
Lower harmonic content eases machine component design and simplifies external control systems
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LOW SPEED SC MACHINES
Ship Propulsion – AMSC5 MW, 230 RPM Motor
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Ship Propulsion Motor Features
• Low speed machines for direct coupling with the propeller• Synchronous machines with high pole count• Sub-power frequency machines needing electric power converter
for operation
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Direct drive motors are preferred because gearbox is eliminated
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Conventional Motor
Superconducting Motor
Superconducting Motor Advantages
Superconducting Motor Advantages for Ship Propulsion• Less than 1/2 the size• Less than 1/3rd the weight• Higher Net Efficiency• Lower Operating costs• Equivalent prices• Inherently quieter• Design flexibility for the ship
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5 MW motor was built as a technology demonstrator
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5 MW HTS Motor Specification
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• Application: Ship propulsion• Type: Synchronous• Output: 5,000 kW at 230 RPM• Rated torque: 207,000 Nm
– Comparisons AMSC 5,000 hp HTS motor: 19,800 NmSiemens 400 kW HTS motor: 2,500 Nm
• Rotor: With cryostat containing high temperature superconducting field coils (BSCCO-2223)
• Stator: Normal temperature, liquid cooled, air-gap copper winding
Both rotor and stator windings employed air-core technologies – no magnetic iron
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5 MW Motor Component Development
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Rotor
Excitation
Refrigeration
HTS Coils
All subsystems were tested prior to assembling in the motor
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5 MW, 230 RPM Motor Rotor Testing
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The rotor with associated hardware was tested at AMSC including:• Excitation up to full current• Refrigeration operating
temperature in full and degraded modes
• Field winding up to full design current
• Rotor balanced in cold state at ALSTOM
Successful rotor field winding testing validated HTS field winding and its cooling system
Rotor
Refrigerator
BrushlessExciter
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Stator Design
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• Air-gap winding– Enables operation at higher flux density than a
winding with iron teeth - hence larger output– Stator coils made from transposed Litz wire for
minimizing eddy current losses– Torque is exerted on the stator conductors
rather than iron teeth - this torque must be supported and transmitted to the stator frame
• Liquid dielectric cooled– Good heat transfer for high power density– Good electrical insulation performance
Key Features:• Class F insulation • 4160 V line voltage• Field at stator bore 1.6 T
Air-core windings enable higher voltage stator as there in no need for insulating coils for line voltages
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Stator Manufacture at ALSTOM
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Stator assembly was designed, fabricated and tested by ALSTOM
Completed StatorStator Coils
Coils employed Litz cable with small strands transposed into a flat cable
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Assembling the Motor
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• Motor assembly and testing at ALSTOM Electrical Machines, Rugby UK
• Assembly completed January 2003
Stator and rotor were mated without any problem –smooth surface of rotor was very helpful.
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Factory Testing the 5 MW Motor
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• Extensive factory testing between February and June 2003
• No load open circuit and short circuit testing– Standard synchronous motor
testing to IEEE 115– Load testing with VDM 5000
drive up to rated motor torque• Testing carried out at ALSTOM,
Rugby by a joint ALSTOM and AMSC team
Test results were consistent with the design values
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Factory Testing – No-Load
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• Open Circuit and Short Circuit testing to IEEE 115– Determine motor parameters– Determine motor efficiency
under full load and part load conditions
– Determine motor temperature rise under full load conditions
• Motor achieved or exceeded design targets
• Completed March 2003
Very successful testing
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Factory Test Results - Parameters
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Parameter Value Units
Nominal rating 5 MW
Rated line voltage 4160 V (rms)
Rated phase current 722 A (rms)
Power factor at rated load 1
Rated speed 230 RPM
Frequency at rated speed 11.5 Hz
D-axis synchronous reactance 0.32 pu
D-axis transient reactance 0.24 pu
D-axis sub-transient reactance 0.16 pu
Testing confirmed the accuracy of AMSC design algorithms
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Factory Testing – Part Load
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• No-Load IEEE 115– Motor Parameters– Efficiency
• Full torque at ½ speed• Limited Structureborne Noise
Data• Operation on a Drive
5 MW HTS Motor 2.5 MW Load Motor
Full-load testing was not possible due to ½ size load machine
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Factory Testing – Part Load
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• Demonstrated operation of the HTS marine motor and drive system• Due to limitation of load machine (2.5 MW), tested HTS motor to;
– Up to rated torque at ½ rated speed – Up to ½ load at rated speed
• Performed thermal (torque) and speed cycles • Stray flux levels comparable with conventional motors• ONR witnessed testing completed June 2003
Customer (ONR) accepted the motor
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Factory Testing Summary
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• Heat Run at rated torque, rated stator current concluded motor will deliver the rated torque with temperature rise predicted from no load tests
• Demonstrated mechanical capability of rotor and stator construction to deliver continuous rated torque
• 5 MW Motor and Drive were delivered to ONR at the Center for Advanced Power Systems (CAPS) on 22 July 2003
• Later, Full-load testing was conducted at the CAPS
Motor met or exceeded all design goals
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5 MW Motor Testing at CAPS, Florida
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• Motor was delivered to CAPS in July 2003.
• Motor was coupled to a pair of 2.5 MW squirrel cage induction motor dynamometers
• Motor load test results were reported ASC-2004 conference at the end of September 2004
5 MWHTS
Motor
2.5 MW Induction
Motor
2.5 MWInduction
Motor
Full-load testing was conducted by simulating ship propulsion load
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CAPS Testing - Open-Circuit Testing
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0
0.5
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2.5
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0 20 40 60 80 100 120 140 160 180
Rotor current (A)
LIn
eV
olts
(kV
)
230 rpm183 rpm115 rpm60 rpm
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Rotor current (A)
LIn
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olts
(kV
)
230 rpm183 rpm115 rpm60 rpm
230 rpm183 rpm115 rpm60 rpm
0.0
5.0
10.0
15.0
20.0
25.0
30.0
35.0
40.0
45.0
0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 5Line Volts (kV)
Los
s (k
W)
230 rpm183 rpm115 rpm60 rpm
0.0
5.0
10.0
15.0
20.0
25.0
30.0
35.0
40.0
45.0
0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 5Line Volts (kV)
Los
s (k
W)
230 rpm183 rpm115 rpm60 rpm
230 rpm183 rpm115 rpm60 rpm
• Open-circuit characteristics at different speeds
• No saturation effect
• Open-circuit losses at different speeds and field excitation levels
• Losses are proportional to field current, i.e. eddy-current dependent
Armature coil, made of copper Litz wire, experience eddy-current losses
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CAPS Testing - Short-Circuit Testing
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100
200
300
400
500
600
700
800
0 5 10 15 20 25 30 35 40 45 50Field current (A)
Sta
tor
curr
ent (
A)
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100
200
300
400
500
600
700
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0 5 10 15 20 25 30 35 40 45 50Field current (A)
Sta
tor
curr
ent (
A)
0.0 0.2 0.4 0.6
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-1
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2
Time (s)
Cur
rent
(kA
)
0.0 0.2 0.4 0.6
0
-1
1
2
Time (s)
Cur
rent
(kA
)• Short-circuit characteristics at
rated speed (230 RPM)• No saturation effect
• Sudden short-circuit test from 15% rated voltage
• Time constants consistent with analysis
No Saturation, but Short-circuit current decays with sub-transient time constant
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CAPS Testing - Load Testing
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0
10
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0 0.5 1 1.5 2 2.5 3 3.5 4 4.5
Time (hours)
Te
mpe
ratu
re (
Ce
lsiu
s)
Start of full load heat run
End of full load heat run
• Initial heat run conducted on September 19, 2004• Motor delivered 5 MW at 230 RPM • Stator attained steady-state temperature
CAPS testing confirms performance of HTS Motor under loadand simulated mission conditions
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LOW SPEED SC MACHINES
Ship Propulsion – AMSC36.5 MW, 120 RPM Motor
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HTS Ship Propulsion Motor Advantages
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• Inherently quieter• Higher net efficiency• Lower operating cost• Smaller volume• Lighter
36 MW HTS36 MW Conventional *
* Scale derived from GEC ALSTOM FSAD 19 MW @150 RPM propulsion motor
0
200
400
600
800
1000
1200
1400
1600
0 20 40 60 80 100
Pow er (MW)
Ma
inte
na
nc
e V
olu
me
(M3)
HTS
Source: MSCL
Actual Conventional Motor Envelope
HTSAdvantage
Volume Comparison: HTS versus Conventional
0
100
200
300
400
500
600
0 10 20 30 40 50 60 70 80 90 100
Power (MW)
Wei
gh
t (M
etri
c T
on
s)
HTS
QE2
GRANDEUR
CRYSTAL
Actual Conventional M
otor Envelope
Source: MSCL
HTSAdvantage
Weight Comparison: HTS versus Conventional
HTS motor volume advantages are impressive over a broad range of ratings
300 tonnes
75 tonnes
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Built 36.5 MW Based on 5 MW Experience
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• Designed and built the motor to power the next generation of Navy ships
• ONR contracted AMSC to deliver the 36.5 MW, 120 RPM motor, integrated with a commercial Variable Frequency Drive
• Attractive Feature: For the same torque, the motors are compared on basis of weights;- 75 tonnes HTS motor, - 280 tonnes1 for an advanced induction motors- 400 tonnes2 for a QE2 synchronous motor
• 36.5 MW motor design was based on the 5 MW motor technology.
1 Scaled from ALSTOM IPS Induction Motor
2 http://www.qe2.org.uk/engine.htmlThis 36.5 MW motors still holds world record for being the largest capacity motor ever built in a single frame
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36.5 MW Motor Calculated Parameters
• This 36.5 MW motor was designed based on the analysis codes used for the 5,000 HP and 5 MW motors
• Calculated parameters were validated by no-load testing according to IEEE 115
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Parameter Value
Rating 36.5 MW
Line Voltage 5.8 kV
Speed 120 RPM
Synchronous reactance, Xd 0.37 pu
Transient reactance, Xd’ 0.32 pu
Sub-transient reactance, Xd” 0.24 pu
Efficiency 97.1%
Parameters above are typical for an air-core machine
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36.5 MW Motor Components
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• AMSC built a 36.5 MW, 120-RPM HTS ship propulsion motor for ONR
• Motor weighs 75-tonnes, including stator and rotor cooling systems
• Delivered to ONR in 2007
HTS Field Coil
Rotor End Ring
Shaft
Stator
Refrigerator
Rotor Under Test
All components were tested/inspected carefully before releasing them for final assembly
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36.5 MW Motor Components
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Stator
Rotor Rotor and stator construction proceeded without any major problem.
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Complete Stator and Rotor Assemblies
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Stator and rotor assemblies prior to joining to form the motor
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36.5 MW Motor Under No-load Testing
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Motor undergoing no-load testing at Northrup Grumman facility in California
No-load testing for measuring parameters and for conducting heat run
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36.5 MW Motor System Layout – No-load Testing
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Arrangement of all sub-systems for no-load testing
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36.5 MW Motor – Open-circuit Testing
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Less than 2% saturation at rated field current
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36.5 MW Motor – Short-circuit Testing
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Short-circuit test shows linear behavior – confirming ability to operate at rated current
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36.5 MW Motor – Design vs. Measurements
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Close agreement between design and measured parameters
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36.5 MW Motor – Stator Heat Run
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Measured Average (55C) and Maximum (91C) stator temperature for about 5-hr run with 1274 A
Water inlet temperature 18C
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36.5 MW Variable Speed Drive
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• Motor system’s variable speed drive (VSD) was installed and commissioned by the Navy
• The drive was a standard industrial drive – a Perfect Harmony™ model provided by Siemens-Robicon
• The drive system consisted of three 3-phase 14 MW drives which were connected to the three 3-phase motor stator winding groups
No issues were noticed between the motor and drive during load testing
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36.5 MW No-Load Testing Conclusions
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• The design, development and manufacture of this large direct-drive ship propulsion motor was validated by the successful factory testing.
• All key design predictions were confirmed; the ability to withstand excess voltage and rated current without problem certainly proved the readiness of this full-scale demonstrator motor for full-load testing.
• Also confirmed both the design codes and the power dense benefit of HTS technology as did its precursor, the equally successful 5 MW HTS motor also developed under ONR sponsorship.
• Because the 36.5 MW HTS motor has passed all the factory acceptance tests and validated that the design should be capable of producing full rated power and torque, the next step for this motor system development was to conduct full power load testing.
• Following this, full power testing of the 36.5 MW HTS motor system was conducted by the Navy operated land-based test site in Philadelphia
• Test results reported: See Reference below
The motor was successfully load tested by the Navy satisfying all design requirements
Ref: Bruce Gamble , Greg Snitchler and Tim MacDonald, “Full Power Test of a 36.5 MW HTS Propulsion Motor”, IEEE Transactions on Applied Superconductivity ( Volume: 21 , Issue: 3 , June 2011 ), pages:1083-1088
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36.5 MW Motor Stator Arrive in Philadelphia
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Leaving Factory Arriving in Philadelphia
Stator and Rotor were shipped separately to the load test site in Philadelphia
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36.5 MW Motor Load Testing
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HTS Motor LoadingBrake
The motor was successfully tested to full-load by US Navy - met all design objectives
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3.6 MW Wind Turbine Generator
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Probably the same size as the NSWC ship propulsion motor
3.6 MW, 12 RPMGeneratorby ECO 5
Source: IEEE Spectrum, Aug. 2018
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HTS Pole for a Wind Turbine Gnerator• A pole made for a 10 MW class wind
turbine generator by AMSC• Employed 2G ReBCO wire• The pole was built and tested in 2011• Demonstrates feasibility of building large
magnets with ReBCO coated conductors
Ref: G. Snitchler et al., “10 MW class superconductor wind turbine generators,” IEEE Trans Applied Superconductivity, vol. 21, no. 3, p. 1089, June 2011
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Made by
AMSC
Coil manufacturing technology demonstratorfor building large HTS pole with ReBCO wire
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What’s will make HTS Machines Attractive• HTS technology amply demonstrated – need for economic viability:
– Low-cost HTS wire and – Reliable and affordable cooling system
• MUST: Improve wire performance (e.g., extended window of operation in terms of higher temperature and magnetic field and lower cost)
• Building HTS machines by leveraging synergies of off-the-shelf-components• Designing machines by including dynamic variation of operating parameters (e.g.,
temperature, excitation, amount of fuel and environment)• HTS machines may have sweet applications where other technologies are not
feasible; Example: > 20 MW wind power generators• An affordable and reliable HTS technology may extend its applications to central
power stations, wind turbine generators, ship propulsion and industrial motors
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Future of the HTS technology looks very promising