Smart Materials and Structures 5. Shape Memory Alloy Materials
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5. Shape Memory Alloy Materials
• Introduction and History
• How SMA Works
• Transformation Hysteresis
• Stress-Strain Relationship
• Superelasticity
• Types of Shape Memory Alloy Materials
• Shape Memory Alloy Properties
• A Constitutive Model of SMA
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Introduction
Example of Shape Memory Alloys (SMA's)
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Introduction
• Shape Memory Alloys (SMA's) are novel metal materials
which have the ability to return to a predetermined shape
when heated.
• When an SMA is cold, or below its transformation
temperature, it has a very low yield strength and can be
deformed quite easily into any new shape. However, when
the material is heated above its transformation temperature
it undergoes a change in crystal structure which causes it to
return to its original shape.
• If the SMA encounters any resistance during this
transformation, it can generate extremely large forces. This
phenomenon provides a unique mechanism for remote
actuation.
SMA Spring
After being Elongated at Cold
SMA Spring
After being heated
For example, the SMA spring shown in the figures can be
easily elongated when it is cold, but the SMA spring
returns to its original shape once heated.
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History
• 1932 Chang and Read noticed reversibility of transformation in gold-
cadmium (AuCd alloy).
• 1938 The transformation was observed in brass (copper-zinc).
• 1951 Read and co-workers observed Shape Memory Effect (SME) in
bent bar of gold-cadmium (AuCd).
• 1962 Buehler and coworkers at Naval Ordnance Laboratory (NOL)
discovered SME in Ni-Ti alloys (NiTiNOL).
• 60’s-70’s many other types of SMAs were found and several products
hit market.
• 80’s – 90’s “Smart” and “Intelligent” materials become a developing
research and development area. SMA materials in various shapes are
commercially available. SMA are utilized in medical applications.
DARPA setup programs to demonstrate capacity of smart materials for
military applications. SMA micro devices emerge.
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How SMA Works
Shape Memory Effect (SME) (One Way)
The shape memory effect is a unique property of certain alloys exhibiting
martensitic transformations. These materials can be deformed in the low
temperature phase, and they will recover their original shape by the reverse
transformation upon heating to a critical temperature called the reverse
transformation temperature. This shape change is due to a change in the atomic
crystal structure of the alloy.
Heat
High Temperature
Cool
Remove Force
Force Force
Low Temperature
Deformed SMA Spring Deformed SMA Spring
SMA Spring
Deform
One Way Shape
Memory Effect of a
SMA Spring.
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Austenite and Martensite:
The high temperature crystal structure is called austenite and is cubic and strong. When cooled,
the material transforms to a structure called martensite, with a monoclinic lattice structure
which looks like a parallelogram in two dimensions and it is weak.
High Temperature
Cubic Structure
- Austenite
Low Temperature
Structure
- Martensite
How SMA Works (con’t)
Nitinol Crystal Structures: Austenite and Martensite
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How SMA Works (con’t)
Twinning Process:
When a piece of shape memory material containing many atoms is cooled below a
transformation temperature, the atoms do not all tilt in the same direction. Instead, the atoms
form alternating rows of atoms tilting either left or right (shown in the figure). Any four atoms
in the low temperature structure have the martensite parallelogram shape. The alternating rows
in the figure is called twinning, because the atoms form mirror images of themselves, or twins,
through a plane of symmetry.
High Temperature Low Temperature
Twinned Martensite
Twinning Process: Nitinol Atomic Rearrangement upon Cooling
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De-twinning Process:
When a stress is applied to the twinned low temperature SMA, the stress will
deform, or accumulate strain, as the twins are reoriented so they all lie in the
same direction. This is called de-twinning, and in shape memory alloys, the
stress required to reorient twins is relatively low. This de-twinning process is
shown in the figure.
How SMA Works (con’t)
As Cooled Deformed by
Applied Force
Force
Force
De-twinning Process: Deformation of Low Temperature Nitinol Structure
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Return to Austenite Upon Heating
Heating the material above a certain temperature will cause the deformed martensite
to return to austenite and the original shape of the piece will be obtained. This occurs
because the original atomic positions are always maintained in the austenite phase.
How SMA Works (con’t)
Phase Transformation of Nitinol Shape Memory Alloy
High Temperature Austenite
Low Temperature Martensite
Twinned Structure
Deformed Low Temperature Martensite
Detwinned Structure
Deform
HeatingCooling
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Phase Transformation of the SMA Spring (Macro and Micro Views)
How SMA Works (con’t)
Heat
High Temperature
Cool
Remove Force
Force Force
Low Temperature
Deformed SMA Spring Deformed SMA Spring
SMA Spring
Deform
Cubic Form
Twinned
Parallelogram
Form
Detwinned
Parallelogram
Form
Detwinned
Parallelogram
Form
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Heat
High Temperature
Cool
Remove Force
Force Force
Low Temperature
Deformed SMA Wire Deformed SMA Wire
SMA Wire
Deform
Cubic Form
Twinned
Parallelogram
Form
Detwinned
Parallelogram
Form
Detwinned
Parallelogram
FormA
B
C
D
Phase Transformation of the SMA Wire (Macro and Micro Views)
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Two-Way Shape Memory Effect (SME)
Two-way shape memory effect: the shape memory
material will return to a low temperature shape on
cooling, as well as to a high temperature shape on
heating. But the recovery stress of a two-way SMA
is much lower than that of a one-way SMA.
In both the one-way and two-way shape memory
effects, only during heating work can be generated.
During cooling with the two-way effect, the material
simply recovers its low temperature shape and
cannot provide a force to external mechanical
components.
Heating Cooling
Deformation
One-Way SME
Cooling
Heating
Two-Way SME
The one-way shape
memory effect
requires a force to
deform the material
while it is cool, but
will recover its shape
when heated.
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Transformation Hysteresis of SMAs
• The phase transformation of SMAs exhibits hysteresis, i.e., transformations on heating and
on cooling do not overlap.
• Hysteresis, a nonlinearity, adversely affect precision control of the structures activated by
SMA actuators.
• To design control methods to compensate for the nonlinearities associated with SMA
actuators poses a challenge for control engineers and researchers.
Heating
Wire Contracts
Cooling
Wire Extends
Weight
Shape Memory Alloy Wire Actuator
C
ur
re
nt
C
ur
re
nt
C
ur
re
nt
An SMA Wire Actuator Temperature
L
en
gt
h
M
ar
te
ns
ite
%
100
0
Austenite
Start
Austenite
Finish
Martensite
Start
Martensite
Finish Transformation
Hysteresis
As
Af
Mf
Ms
Mf < Ms < As < Af
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Hysteresis of an SMA Wire Actuator
• A programmable current amplifier is used to electrically heat the SMA wire.
• A linear variable differential transformer (LVDT) is placed aganst the slider to detect the
actuator’s displacement.
• The electrical heating of the wire causes a phase transformation, which is seen as a contraction
of the wire. The wire’s contraction places additional tension on the spring. Once the current is
cut off and heat is removed, the bias spring will pull the SMA wire actuator back to its cold
length.
Shape Memory Alloy Wire Actuator
LVDT Position
Sensor
Current Amplifier
Bia Spring
Linear
Bearing
• A Nickel-Titanium shape memory
alloy wire (30.48 cm in length and
0.381 mm in diameter) is used.
• In this SMA test stand, the shape
memory alloy wire is attached
between two wire supports. One wire
support is attached to a slider that is
free to slide through a linear bearing.
The slider is attached to a biasing
spring which pretensions the shape
memory alloy wire.
Experimental Setup
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Motion Obtained by the SMA Wire Actuator
SMA at low temperature.
L1
Stretch the wire at low temperature
by the bias spring.
L2
Remove force, new length at low
Temperature.
Apply heat, regain original length
L1
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0 0.5 1 1.5 2 2.5 3 3.5 4
0
2
4
6
8
10
12
14
Displacement v/s Voltage
Voltage (volt)
D
is
pl
ac
em
en
t
(m
m
)
• The shape memory alloy wire is excited using a
sinusoidal signal. Though input voltage is pure
sinusoidal, the displacement is not.
• The hysteresis loops observed have an average width of
2 volts. The curves are not very smooth, and this can be
attributed to the uncontrolled ambient conditions.
• The shape memory alloy wire actuator is not fully
repeatable due to the uncontrolled ambient condition. 0 50 100 150 200 250 300
0
0.5
1
1.5
2
2.5
3
3.5
4
Applied Voltage and Current - Training Signal
.....Voltage _____Current
Time (sec)
V
ol
ta
ge
(
vo
lt)
a
nd
C
ur
re
nt
(
am
p)
0 50 100 150 200 250 300
0
2
4
6
8
10
12
14
Displacement - Training Signal
Time (sec)
D
is
pl
ac
em
en
t (
m
m
)
The Applied Sinusoidal Voltage and Measured Current
Displacement of the SMA Wire Actuator Relationship between the Applied Voltage and
Displacement
Hysteresis
Loops
Hysteresis Loop:
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Stress-Strain Relationship of SMA
• The Stress-Strain relationship of shape memory alloys shows strong temperature
dependence, because of the reversible Austenite to Martensite transformation.
• This figure shows the stress-strain relationship of a shape memory alloy at or below the
Mf temperature. It is assumed that the SMA is cooled from the Austenite without
applying stress.
Stress
Strain
Detwinning
Elastic
Region
Elastic
Region
Plastic
Deformation
O
BA
CStress-strain Relationship at or below Mf
OA: The initial curve segment represents
elastic deformation and the microstructure
consists of randomly oriented Martensite
twins.
A: Detwinning starts. At this point, the stress
level is sufficient to start the twins to reorient
according to the applied stress field.
AB: Detwinning. The twins reorient until
they all lie in the same crystallographic
direction.
B: Detwinning is complete at point.
BC: The Martensite undergoes mostly elastic
deformation again in segment BC. At point
C: The stress level is sufficient to start plastic
deformation of the Martensite.
Beyond C: The shape memory effect is
destroyed or severely diminished by plastic
deformation of the Martensite.
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Stress
Strain
Stress induced Martensite
Elastic
RegionElastic Region
Plastic
Deformation
O
BA
CStress-strain Relationship above Af below Md
Md: temperature at which non-elastic deformation is due
to slip (plastic yielding) at stress induced Martensite.
O: The material is fully austenitic.
OA: Elastic deformation.
A: Martensite begins to form from
the austenite, this material is
referred to as stress induced
martensite.
AB: Stress induced Martensite..
BC: Represents elastic deformation.
C: Plastic deformation starts to occur.
AB: When the material is unloaded in this segment with stress
induced Martensite, the Martensite becomes unstable and the
material returns to austenite and its original shape. The material can
experience 8% of strain change. Superelasticity occurs.
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At temperatures above Md, non-elastic deformation is entirely due
to plastic yielding, and no stress induced Martensite is formed.
Stress
Elastic
Region
Plastic
Deformation
Strain
Stress-strain Relationship above Md
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Example: Stress-Strain Memory Effect of an SMA Wire
Stress
Strain
heating
Deformed state
w
wHigh temperature
Austenite curve
Low temperature
Martensite curve
sA
sM
eA eM
When heated
contracts to high
temperature state
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Superelasticity
• Definition: the behavior of certain alloys to return to their original shape upon unloading
after a substantial deformation has been applied.
• The superelastic mode takes place under constant temperature conditions.
• When a shape memory alloy is deformed above Af and below Md (the temperature above
which stress-induced martensite can no longer be formed). stress-induced martensite is
formed. When the material is unloaded, the martensite becomes unstable and the material
returns to austenite and its original shape. Superelasticity occurs. The stress-strain
relationship is shown in the figure.
The unloading curve occurs at
a lower stress due to
transformational hysteresis
which is closely related to the
thermal hysteresis in shape
memory behavior. The loading
plateau is the result of the
martensite accommodating the
applied stress by forming the
crystallographic twin variant
most favorably inclined to the
applied stress field.
Unloading plateau
Loading plateau
STAIN
STRESS
Sl: loading stress Su: unloading stress
et: total strain
Sl
Su
et
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Superelasticity: Effect of Temperature on
loading and Unloading Stresses
Loading and unloading stress increase with increasing
temperature within the “Superelastic window.”
Unloading
plateau
Loading
plateau
Temperature
Stress
Material
Elastic
Strain
Steel 0.8%
Cu-Zn-AI 5.0%
Ni-Ti 10.0%
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Superelastic Window
• In the left portion of the figure, the plastic strain is large and due to the
Martensitic transformation associated with the shape memory event (i.e. it can
be recovered by heating above Af,).
• To the right of the minimum point there exists a relatively flat portion which
defines the “superelastic window” since the permanent plastic strain is small.
• To the right of the “superelastic window” the permanent plastic strain increases
dramatically and is therefore not acceptable for superelastic applications.
% set
after
8% Strain
Shape memory
zone
(recover strain
by heating)
Superelastic + plastic
Deformation
(permanent set)
Temperature
Superelastic
zone
• This figure shows the
useable temperature
range for superelastic
behavior, commonly
referred to as the
"superelastic window".
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Narrow Superelastic Window Limits Application
• An approximately 40°C window, starting at the Af temperature,
can be obtained by strengthening the alloy--through a
combination of cold work, aging, and annealing.
• Still, this functional temperature range is too narrow for most
industrial and consumer applications. Automobile springs, for
example, generally require elasticity from -30° to 200°C.
Moreover, the stiffness of a superelastic device changes with
temperature according to the Claussius-Clapeyron equation, at a
rate of approximately 4-8 MPa/°C.
• The variability of superelasticity with temperature, and therefore
its narrow superelastic window, limits the general use of
superelastic materials.
Superelastic Window (con’t)
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Types of Shape Memory Alloy Materials
• There are many known alloy systems which exhibit the shape memory effect, but only
three have shown promise for commercial applications. They are Nickel-Titanium (Ni-
Ti), Copper-Zinc-Aluminum (Cu-Zn-Al), and Copper-Aluminum-Nickel (Cu-Al-Ni).
• The copper-zinc-aluminum alloys have a typical composition of 15 – 25 weight
percentage Zn / 6 – 9 weight percentage Al / balance Cu. Cu-Zn-Al alloys are lower in
cost than nickel titanium, but they possess some inferior characteristics.
Transformation temperatures can drift slightly during cycling (particularly at service
temperatures greater than 100 oC) and to a significant extent if the alloy is not processed
properly. These alloys are susceptible to stress corrosion cracking when exposed to
certain corrosive agents.
• The copper-aluminum-nickel alloys have a typical composition of 13 – 14 weight
percentage Al / 3 – 4 weight percentage Ni / balance Cu. Cu-Al-Ni alloys possess
lower ductility than either Ni-Ti or Cu-Zn-Al. Their corrosion resistance is inferior to
Ni-Ti and their cost is higher than Cu-Zn-Al. Cu-Al-Ni alloys undergo less degradation
in shape memory properties than Cu-Zn-Al, after exposure to temperatures in the 100 to
350O C range. In addition, Cu-Al-Ni alloys have the highest transformation
temperatures of the three alloys.
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Nitinol
• The nickel titanium alloys (Nitinol) they have typical compositions of
approximately 50 atomic percentage Ni / 50 atomic percentage Ti, and may have
small additions of copper, iron, cobalt, or chromium.
• Nickel-titanium is about four times the cost of Cu-Zn-Al alloys.
• It has several advantages over Cu-Zn-Al and Cu-Al-Ni:
– greater ductility
– more recoverable motion
–