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7/28/2019 Recent Developments in Room Temperature Active Magnetic Regenerative Refrigeration
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Recent Developments in Room
Temperature Active Magnetic RegenerativeRefrigeration
Kurt Engelbrecht, Nini Pryds, Christian Bahl
Ris DTU
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Magnetic Refrigeration Background
Alternative to vapor compression
Magnetic refrigeration used to first break 1Ktemperature barrier near 1935, but used a one shot
technique with a very low temperature span
Giauque awarded the Nobel Prize in chemistry in 1949
First regenerative magnetic refrigerator proof-of-
concept device built by Brown in 1976
Possible applications include residential/commercial
space cooling, refrigeration, hydrogen
liquefaction/storage
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Advantages of Magnetic Refrigeration
Environmentally friendly
no ozone depleting or direct global warming associated withthe refrigerant
Possibly more efficient than current technologies
no superheat or throttling loss
no compressor losses
nominally equivalent heat exchanger loss
relatively easy to achieve efficient part load operation
Quiet operation
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Room Temperature Magnetic Materials
The magnetocaloric effect is greatest at the Curie point of the magnetic
material, which can be adjusted by alloying
200 225 250 275 300 325 3500
2
4
6
8
10
12
Temperature (K)
AdiabaticT
emperatureC
hange(K)
0-5 Tesla
0-2 Tesla
Gadolinium (Gd) and
Erbium (Er) alloy
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Magnetic Refrigeration Concept
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MagnetizationHot-to-Cold FlowCold-to-Hot FlowDemagnetization
Cold
Reservoir
Hot
Reservoir
Heat
Rejection
Refrigeration
Active Magnetic Regenerative
Refrigerator Cycle (AMRR)
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Magnetic Refrigerator Design
Considerations
System configuration
rotary, reciprocating, etc.
Magnetocaloric material selection
Regenerator design
Magnetic field
Heat transfer fluid selection
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AMRR System Configurations
Stationary bed with an electromagnet
magnetic field is controlled by varying the current
to the electromagnet
QH QC
magnet
regenerator
displacer
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AMRR System Configurations
Reciprocating system
magnet
regenerator
displacer
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AMRR System Configurations
Rotary system magnet
regenerator
pump
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Permanent
Magnet
bed
rotation
Magnetization in a Rotary Bed
Magnetic field sweeps
through bed.
magnetized region
zero magnetic field
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Choosing Magnetocaloric Materials
Adiabatic temperature change
Isothermal entropy change
Thermal conductivity
Magnetic hysteresis
Practical issues cost, corrosion, toxicity,manufacturability
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Magnetocaloric Material Properties
Magnetic materials generally experience a phase
change from a ferromagnet to a paramagnet at the
Curie Point Second-order magnetic phase transitions (SOMT)
transition associated with the alignment of magnetic
moments in the material
effect is nearly instantaneous (order of nanoseconds)
generally reversible magnetization
First order-magnetic phase transitions (FOMT)
latent heat and large magnetocaloric effect associated with
transition
higher irreversibilities than second order
longer time associated with transition
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Summary of Magnetocaloric Material
Properties
1
3 (0-1.45
Tesla)30FOMT287x=0.1
6532FOMT318x=0
MnAs1-xSbx
17.128FOMT287LaFe11.7Si1.3H1.1
2727FOMT269Gd5Si3.5Ge0.5
~05.55.8SOMT294Gd
(K)(K)(J/kg-K)(K)
HysteresisTad
-sM
TypeTCurieMaterial
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AMRR Loss Mechanisms
Heat transfer / regeneration losses
Pumping / viscous dissipation losses
Axial conduction
Eddy current heating
Heat exchanger and motor losses nominally equivalent to vapor compression
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Regenerator Design
Packed regenerator
packed sphere, packed powder, etc.
relatively easy to achieve high surface area fluid flow profile is generally well-distributed
high pressure drop
Flat plate regenerator
low pressure drop
requires small dimensions to achieve high heat
transfer performance
theoretically best regenerator performance
performance highly dependent on geometry
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Prototype AMRR Performance Summary
540GdSiGeGa
100Gd5Si
2Ge
2
spheres (0.2mm)230Gd~2001.4 (P)Nanjing University
spheres (0.25-0.355mm)250Gd & GdEr
spheres (0.25-0.355mm)1427Gd & GdEr
spheres (0.43-0.5mm)1415Gd331.5 (P)
0600
spheres (0.15-0.3mm)38100Gd~6005 (S)Astronautics24402 (S)
spheres (0.3 mm)26100Gd4844 (S)Chubu Electri /
Tokyo University
47Gd252 (S)
(2004)
spheres (0.2mm)200Gd492 (S)
crushed part. (0.4mm)500Gd, GdTb & GdEr742 (S)
University ofVictoria (2006)
KWcm3Tesla
Regen typedTQCRegen materialVregen
oH
MaxSystem
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Promising AMRR Innovations
High performance magnetocaloric materials
with tunable Curie Temperatures
Layered regenerators
Rotary systems
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Efficiency Dependence on Regenerator Volume
Packed Sphere Regenerator8.76 kW Space Conditioning Application
5 10 15 20 25 30 352.75
3
3.25
3.5
3.75
4
4.25
4.5
4.75
Regenerator volume, L
C
oefficientof
performance
layered bed
non-layered bed
vapor compression
B
A
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AMRR Design Consideration
,
~
v refAMRR
vc f mc
hm
m c T
&
&
The mass flow rate of fluid in an AMRR is much
higher than an equivalent vapor compression
system
no phase change in the fluid
For a practical system, the fluid flow rate is ~20
times the refrigerant flow rate for vapor comp
Requires larger connecting piping to reduce
pressure drop
for equal refrigeration capacity
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Future Work at Ris
Currently designing next generationprototype AMRR
Project goal: 100W cooling at 40Ktemperature span
System should be practical and cost effective
Prototype will be built in 2009
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Conclusions
Improvements have been made to prototype AMRR
systems recently, but the technology is still not mature
Systems using a layered regenerator beds have been
shown higher performance over a relatively large
temperature span
New magnetocaloric materials have potential to
significantly improve AMRR performance
Gd remains
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Modeling Efforts
Developed a 1D AMRR model
used model to determine limits of AMRR technology
and investigate control techniquesK. L. Engelbrecht, G. F. Nellis, and S. A. Klein, 2006, Predicting the Performance
of an Active Magnetic Regenerator Refrigerator used for Space Cooling and
Refrigeration, HVAC&R Journal12(4):1077-1095
K. L. Engelbrecht, G. F. Nellis, and S. A. Klein, 2006, Modeling the Transient
Behavior of an Active Magnetic Regenerative Refrigerator, Proceedings of the
11th International Refrigeration and Air Conditioning Conference at Purdue,
West Lafayette, IN
Used the model to predict the performance of a
rotary AMRR prototype
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Model Verification Rotary Input Data
Modeling parameters - geometry
Parameter Value Parameter Value
regenerator type packed sphere maximum applied field 1.5 Tesla
regenerator material Gd sphere size for packing 0.425-0.5 mm
regenerator beds 6 porosity 0.362
regenerator height 6.6 mm motor efficiency N/S
regenerator width 15.9 mm dwell ratio 1/3
regenerator length 2.025 in magnet arc 120
regenerator volume 33 cm3
heat transfer fluid
90% water/10%
ethylene glycol
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Uncertainty in Model Inputs
x
( )m t&
heat transfer fluid properties:
cold end,fluid enters at TC
magnetic regenerator material properties:
( ) ( ) ( ) ( ), , , , , , , ,rr o r o r o
T
sk T x T x H c T x H x
H
( ) ( ) ( ), , ,f f f fc T k T T
( ),o x t
hot end,
fluid enters at TH
Tf(x,t)
Tr(x,t)
regenerator bed configurationAc, L, as, dh, , Nu(Re, Pr), f(Re), keff(Re, Pr,..)
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Modeling Error vs. Temperature Span
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FLUID PUMP
COLD HX
MAGNETOCALORIC
WHEEL
PERMANENT
MAGNET
DRIVE MOTOR
Example of a Prototype Rotary AMRR
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Reduction in Cooling Power at
Reduced Heat Transfer
25.4%39.10.674.017.48
17.1%22.40.344.011.8719.6%44.10.671.011.56
10.8%24.60.351.013.15
2.2%67.80.814.00.24
8.3%35.40.354.00.83
0.3%53.20.671.00.32
1.0%35.70.341.00.21
WLiter/minHzK
Cooling
Power Loss
Predicted
Cooling Power
Fluid Flow
Rate
Cycle
FrequencyTCase
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Determining Actual Magnetic Field
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Governing Equations
( ) ( )( ) ( )
( ) ( )
2
2
f f f f
f f f s c f r f f f c f
h
rdisp c
Nu Re ,Pr k Tm t c T T a A T T c T A T
x d t
enthalpy flow capacity of heat transfer toentrained fluidregenerator material
Tk A
x
axialdispersion
+ +
&
144424443 144424443144444424444443
1 2
( )
f
m tp
x
viscous
dissipation
=
&
4 43
14243
( ) ( )( ) ( ) ( )
2
21 1
f f f f r rs c f r c o eff c r c
h
Nu Re ,Pr k T T ua A T T A H k A A
d t x t
axialmagnetic work energy stored heat transfer from fluidconduction
in matrix
+ + = 144424443 14243 1442443144444424444443
Fluid:
Regenerator:
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Modeling Efforts
Developed a 1D AMRR model flexible design tool
capable of predicting the performance of an AMRRsystem
Verify the model experimentally
Make the model publicly available
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Representative Experimental Cases
xxx8
xxx7xxx6
xxx5
xxx4xxx3
xxx2
xxx1highlowhighlowhighlow
Fluid Flow RateCycle FrequencyTemperature SpanCase
M d l S iti it t H t T f C ffi i t i th
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Model Sensitivity to Heat Transfer Coefficient in the
Regenerator
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bed
rotation
mass flow inmass flow out
Cold to Hot Flow in a Rotary Bed
flow activated as
bed moves over
cold check-valve
flow activated as
bed moves over
hot check-valve
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Numerical Verification: Schumann Solution
Solid and fluid in a regenerator are initially at a uniform temperature of
0 K and fluid at temperature THenters at t=0
Analytical solution for transient temperature profiles of the fluid and
solid exists Shitzer, A. and M. Levy, 1983, Transient Behavior of a Rock-Bed Thermal Storage Sytem
Subjected to Varibable Inlet Air Temperatures: Analysis and Experimentation, Journal of Solar
Engineering, vol 105: p. 200-206
Solution assumes constant material properties, no axial conduction,
and uniform heat transfer between fluid and solid
The temperature profiles predicted by the numerical model can beverified against this analytical solution
M d l V ifi ti Si l Bl
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fluid temp
Model Verification Single Blow
NTU=50
regenerator
temp