the status of hts ship propulsion motor...
TRANSCRIPT
The Status of HTS The Status of HTS Ship Propulsion Motor DevelopmentsShip Propulsion Motor Developments
S. Kalsi, B. Gamble, G. Snitchler and S. Ige AMSC
Panel: Superconductor Rotating Machines for Ship and Aircraft Panel: Superconductor Rotating Machines for Ship and Aircraft ApplicationsApplications
IEEE PES Meeting, Montreal, CanadaIEEE PES Meeting, Montreal, Canada20 June 2006
OutlineOutline
Introduction Wire technology
BackgroundPrior machines
36.5 MW36.5 MW basic characteristicsSubsystem descriptionsProgress and status
Other Opportunities CondensersGeneratorsDegaussing
Summary and Power Density Comparison
36.5 MW HTS Propulsion Motor Development36.5 MW HTS Propulsion Motor DevelopmentIntroduction Introduction –– Machine TopologyMachine Topology
Multiphase Synchronous MachineMedium voltageConventional driveAdjustable excitationLarge airgapLow synchronous reactanceEfficient
RotorHTS field windingVacuum insulatedCooling in stationary reference frameCOTS rotor cooling hardware
StatorDielectric oil coolingLitz copper coilsComposite teethBack-iron return flux path
BearingsRotor poles
Back iron
Stator coils
Vacuumchamber
Housing
EM shield
Brushlessexciter
Heliumtransfercoupling
BearingsRotor poles
Back iron
Stator coils
Vacuumchamber
Housing
EM shield
Brushlessexciter
Heliumtransfercoupling
36.5 MW HTS Propulsion Motor Development36.5 MW HTS Propulsion Motor DevelopmentIntroduction Introduction –– High Temperature Superconductor WiresHigh Temperature Superconductor Wires
0.2mm0.2mm
BiBi22SrSr22CaCa22CuCu33OO YY11BaBa22CuCu33OO
4.4mm4.4mm
First generation (1G) HTS wire Second generation (2G) HTS wire - 344 Superconductors
344 superconductors are designed to be a low cost, form-fit-function replacement For 1G wire – both available for sale
36.5 MW HTS Propulsion Motor Development36.5 MW HTS Propulsion Motor DevelopmentIntroduction Introduction –– High Temperature Superconductor WiresHigh Temperature Superconductor Wires
2G Wire (344): 125A, 4.4 mm width1G Wire: 125A, 4.4 mm width
0 2 4 6 81
10
100
1G-64K1G-77K
1G-35K
2G-40K
2G-65K
2G-77KCrit
ical
Cur
rent
(A)
Applied Field (T)
H//c
2G wire performance in applied field equals or exceeds 1G wire
36.5 MW HTS Propulsion Motor Development36.5 MW HTS Propulsion Motor DevelopmentBackground Background –– Prior HTS Electric MachinesPrior HTS Electric Machines
Early MachinesAMSC and RockwellFractional HP through 1000 HP at 1800 rpm LN2 and helium gas coolingAir cooled armatures
5,000 HP MotorAMSC fabricated rotor tested at Electric MachinesWater-cooled Litz ArmatureNeon-cooled rotor
5 MW MotorAMSC and ALSTOMDielectric oil cooled Litz ArmatureHelium gas cooled rotorExtensively tested by CAPS for ONR
3,000 ft-lbf
15,000 ft-lbf
150,000 ft-lbf
Developments led to the 2,100,000 ft-lbf 36.5MW ONR Motor
36.5 MW HTS Propulsion Motor Development36.5 MW HTS Propulsion Motor Development5 MW AMSC/ONR Subscale Demonstration5 MW AMSC/ONR Subscale Demonstration
Joint AMSC/ALSTOM project sponsored by ONRAMSC
Rotor Cryorefrigeration systemExcitation system
ALSTOM in Rugby, UK & Nancy, FranceStatorMotor assembly & FAT
FAT completed 2003—50% power, 100% torqueIEEE-115 testingValidated armature temperature riseDemonstrated mechanical capability
Full-power testing at Florida State University Center for Advanced Power Systems (CAPS)
5 MW demonstrated at 230 rpmLoad & ship mission profile simulation Motor to NAVSSES, Philadelphia in 2005
Power: 5 MW Torque: 153,000 ft-lbsSpeed: 0-230 rpm Volts: 4160, 3Ø, 0-11.5 HzField: 137 A, 30K Refrigeration: Gaseous HeArmature: Liquid cooled
5 MW Motor Testing At CAPS5 MW Motor Testing At CAPS
2.5 MW Load Motors
5 MW HTSMotor
5 MW HTS Motor delivered rated power and torque
36.5 MW HTS Propulsion Motor Development36.5 MW HTS Propulsion Motor DevelopmentONR ProgramONR Program
Objective: Develop a Full Scale, High Power Density, Lightweight, Advanced 36.5 MW Propulsion Motor and Drive System compatible with naval applications Contract Awarded to AMSC February 2003Design Drivers: Low Weight, High Power Density, Improved Efficiency and Low Noise Detail Design Completed October 2004 –Design meets MIL-S-901D Shock and DD(X) AcousticsFactory Acceptance Testing (Marine Systems) completed in 4th Quarter 2006
4 5 6 7 8 9 10 11 12 1 2 3 4 5 6 7 8 9 10 11 12 1 2 3 4 5 6 7 8 9 10 11 12 1 2 3 4 5 6 7 8 9
Phase A - Preliminary Design
Phase B - Detailed Design
Phase C - Manufacture and FAT
2003 2004 2005 2006
DDR Motor
Delivery
Design leverages features successfully tested on 5 MW HTS motor
10
PDR
36.5 MW HTS Propulsion Motor Development36.5 MW HTS Propulsion Motor DevelopmentSubsystemsSubsystems
Drive – Robicon/Siemens
MotorRotor – AMSCStator – Electric MachinesFrame – NGES-MS
Rotor Cooling - AMSC
Stator Cooling Skid NGSS
Stator Lube Skid - NGSS
System Controller - AMSC
36.5 MW HTS Propulsion Motor Development36.5 MW HTS Propulsion Motor DevelopmentComponents during ManufactureComponents during Manufacture
Rotor Complete and Delivered to NGC Motor Assembly Site
Refrigerator Complete and Delivered
Stator Winding Process Nearing Completion
Frame is Currently Being Installed at NGC Philadelphia Test Facility
Many components have already passed factory acceptance tests
36.5 MW HTS Propulsion Motor Development36.5 MW HTS Propulsion Motor DevelopmentCalculated Characteristic ParametersCalculated Characteristic Parameters
• 36.5MW motor was designed based on the analysis codes used for the 5,000 HP and 5 MW motors.
• Calculated parameters will be validated in testing later this year per IEEE 115 no-load test procedures at NGC Philadelphia
Rating 36.5 MW
Vphase 5.8 kV
Speed 120 rpm
Xd 0.368 pu
Xdstr 0.32 pu
Xdstr 0.243 pu
η (motor) 97.1 %
η (w ancillaires) 96.9 %
Factory testing will occur over the summer with a September completion
36.5 MW HTS Propulsion Motor Development36.5 MW HTS Propulsion Motor DevelopmentInitial Factory Test ResultsInitial Factory Test Results
• Integrated Rotor Field Winding Test
- Rotor- Exciter- Refrigeration
• Integrated Test Results- Thermal Steady State- Temperature Below Design
Point- Exciter Tests Included
• Active Field Adjustment
• Operation to 113% current
Rotor+HTS Poles+Rotor Cooler+Exciter designs verified in factory testing
Time (hrs)
Fiel
d C
urre
nt (p
.u.)
Tem
pera
ture
(K)
Other HTS Technology ApplicationsOther HTS Technology ApplicationsCondensers, GeneratorsCondensers, Generators
6.0 m3.7 m
4.4
m
1
Conventional
HTS
• Two power ranges of interest:- 40 – 50 MW to package with either LM6000
or RR MT-30 uprated turbines for main turbine generator
- 14 MW to package with LM1600 gas turbine and up-rate the auxiliary GT capability
• Either program ~30 month development• Permits transformerless drive systems
saving several times the generator weight
SuperVARSuperVAR®® Installation Installation on TVA Gridon TVA Grid
HTS generator technologies build on utility grid experience
40 MW HTS GeneratorCompared to
DD(X) 36 MW Generator
DD(X) EDM Generator @ 82 TonsHTS Generator @ 37 Tons
HTS Generators offer impressive weight and size advantage
36.5 MW HTS Propulsion Motor Development36.5 MW HTS Propulsion Motor DevelopmentSummary and Power Density ComparisonSummary and Power Density Comparison
HTS Motors are multi-phase synchronous machines with active field control, large airgap, and the flexibility to utilize a variety of drives.HTS wire used in the actively cooled rotor is presently 1G; starting migration to 2G wireThe 36.5 MW motor is based on experience from multiple HTS electric machines.The ONR 5 MW motor provided the basis for the components used in the 36.5 MW motor.The program is on track to deliver a high power density75 metric ton motor to the Navy in September of this year.The rotor has been tested and the stator assembly is almost complete.No load testing at the NGC Philadelphia facility this summer.HTS is also applicable to generators.
0204060
80100120140160180200
0.010 0.100 1.000 10.000Torque (MN-m)
Wei
ght (
Tonn
e)
40 MW HTS Generator Estimate
HTS 5 kHP1800 rpm HTS 5 MW 230 rpm
HTS 36.5 MW 120 rpm
AIM
36 MW 2-pole Conv. Generator
HTS motors offer the next generation in power density for naval propulsion
TM