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SHAPE MEMORY ALLOYS
BASICS
INTRODUCTION:
 The demand for lighter, stronger materials with tailored properties has spawned a new branch of materials called
multifunctional materials.
 A specialized subgroup of multifunctional materials exhibiting sensing and actuation capabilities is known as
active materials.
 Some examples of active materials include piezo electrics and electrostrictives (coupling of mechanical with
electric fields), piezo magnetics and magnetostrictives (coupling of mechanical with magnetic fields), and shape
memory materials(coupling of thermal with mechanical fields).
Active materials can be further subdivided into materials that exhibit direct or indirect coupling.
Piezoceramics, piezoelectric polymers, magnetostrictive ceramics, shape memory alloys and
magnetic shape memory alloys are examples of active materials that exhibit a direct coupling. In
contrast, for active materials such as electro-rheological fluids (ERF) and magneto-rheological fluids
(MRF), a change in the electric field or the magnetic field can indirectly couple with the mechanical
behavior through a change in the viscosity of the fluid.
 An active material with direct coupling for actuation applications depends on many factors:
 the actuation energy density (available work output per unit volume) : defined as the product of the actuation
strain (related to the stroke of an actuator) with the actuation Stress and
 the actuation frequency of the material.
SMAs
Aunique class of shape memory materials with the ability to recover their shape when the
temperature is increased.
Under specific conditions, SMAs can absorb and dissipate mechanical energy by undergoing a
reversible hysteretic shape change when subjected to applied mechanical cyclic loading. So, used
in impact absorption and vibration damping applications.
The application of SMAs spans a wide variety of industrial sectors such as aerospace,
automotive, biomedical, and oil exploration.
A BRIEF HISTORY
 Discovery of martensite in steels in the 1890s by Adolf Martens.
 The concept of thermoelastic martensitic transformation was introduced in 1949 by Kurdjumov and Khandros.(CuZn and
CuAl alloys.)
 By 1953, the occurrence of thermoelastic martensitic transformation was demonstrated in other alloys such as InTl and
CuZn.
 1963. The breakthrough for engineering applications occurred with the discovery of NiTi by Buehler and coworkers while
investigating materials useful for heat shielding. the term “NiTiNOL” was coined for this NiTi material in honor of its
discovery at the Naval Ordnance Laboratory (NOL). The term Shape Memory Effect (SME) was given to the associated
shape recovery behavior. The effects of heat treatment, composition and microstructure were widely investigated.
 In 1965, studies showed that the addition of a third alloying element( Co and Fe). Led to the first commercial SMA
application, known as Cryofit
 Continued research to address this issue led to the development of the NiTiNb system in 1989.
 High Temperature SMAs (HTSMAs), such as TiPd, TiPt and TiAu (with transformation temperatures greater than
100 ◦C), were also developed as early as 1970 .Meanwhile, Melton and Mercier ,while studying the fatigue
properties of NiTi in 1978.
 Later in 1999, Miyazaki showed improved fatigue life for NiTiCu alloys.
 By 1990s that NiTi stents made their commercial breakthrough.
Phenomenology of Phase Transformation in Shape
Memory Alloys
 Within the typical operating temperature range, SMAs have two phases, each with a different crystal structure and therefore
different properties. One is the high temperature phase called austenite (A) and the other is the low temperature phase called
martensite (M). Austenite (generally cubic) has a different crystal structure from martensite (tetragonal, orthorhombic or
monoclinic).
 Transformation from one structure to the other occur by shear lattice distortion. Such a transformation is known as martensite.
 Martensitic crystal formed can have a different orientation direction, called a variant.
 The phase transition from austenite to martensite is termed the forward transformation.
 When the material is heated from the martensitic phase, the crystal structure transforms
back to austenite, and this transition is called reverse transformation
 Four characteristic temperatures associated with the phase transformation.(Ms, Mf,As And Af)
SHAPE MEMORY EFFECT:
 The load applied must be sufficiently large to start the detwinning process.
 The minimum stress required for detwinning initiation is termed the detwinning start stress (σs).
 Sufficiently high load levels will result in complete detwinning of martensite where the corresponding stress level is called
the detwinning finish stress (σf ).
 The transformation temperatures strongly depend on the magnitude of the applied load,
with higher values of applied load leading to higher transformation temperatures.
 Irrespective of the nature of applied load (tension or compression), the
transformation temperatures increase with an increase in the magnitude of the load.
PSEUDOELASTIC EFFECT
Transformation can also be induced by
applying a sufficiently high mechanical load to
the material in the austenitic phase. The result
of this load is fully detwinned martensite
created from austenite. If the temperature of
the material is above Af , a complete shape
recovery is observed upon unloading to
austenite. This material behavior is called the
pseudo elastic effect.
PHASE DIAGRAM OF SMA:
A diagram, illustrating the different phases
in a stress-temperature space for a given
SMA with fixed composition, is called the
phase diagram.
SHAPE MEMORY EFFECT:
 An SMA exhibits the shape memory effect (SME) when it is deformed while in the twinned martensitic phase and
then unloaded while at a temperature below As.
 The strain recovered due to the phase
transformation from detwinned martensite to
austenite is termed as the transformation
strain (εt).
PSEUDOPLASTICITY
 The pseudo elastic behavior of SMAs is associated with stress-induced transformation , which leads to strain
generation during loading and subsequent strain recovery upon unloading at temperatures above Af.
 Generally, the term pseudo elasticity describes both super elastic behavior and so-called rubber-like behaviour
CYCLIC BEHAVIOR OF SMAS:
 We have studied the one-way SME behavior in SMAs. Sometimes an SMA can exhibit repeatable shape
changes under no applied mechanical load when subjected to a cyclic thermal load. This behavior is termed
two-way shape memory effect (TWSME).
 Training an SMA refers to a process of repeatedly loading the material following a cyclic thermomechanical
loading path until the hysteretic response of the material stabilizes and the inelastic strain saturates.
 There are limitations that reduce the usability of the two-way effect, such as
smaller strains (2 %), extremely low cooling transformation forces and
unknown long-term fatigue and stability
APPLICATIONS:
 Aircraft
 Automobiles
 Robotics
 Medicines
 Piping
 Optometry

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SHAPE MEMORY ALLOYS(ppt_1).pptx

  • 2. INTRODUCTION:  The demand for lighter, stronger materials with tailored properties has spawned a new branch of materials called multifunctional materials.  A specialized subgroup of multifunctional materials exhibiting sensing and actuation capabilities is known as active materials.  Some examples of active materials include piezo electrics and electrostrictives (coupling of mechanical with electric fields), piezo magnetics and magnetostrictives (coupling of mechanical with magnetic fields), and shape memory materials(coupling of thermal with mechanical fields).
  • 3. Active materials can be further subdivided into materials that exhibit direct or indirect coupling. Piezoceramics, piezoelectric polymers, magnetostrictive ceramics, shape memory alloys and magnetic shape memory alloys are examples of active materials that exhibit a direct coupling. In contrast, for active materials such as electro-rheological fluids (ERF) and magneto-rheological fluids (MRF), a change in the electric field or the magnetic field can indirectly couple with the mechanical behavior through a change in the viscosity of the fluid.
  • 4.  An active material with direct coupling for actuation applications depends on many factors:  the actuation energy density (available work output per unit volume) : defined as the product of the actuation strain (related to the stroke of an actuator) with the actuation Stress and  the actuation frequency of the material.
  • 5. SMAs Aunique class of shape memory materials with the ability to recover their shape when the temperature is increased. Under specific conditions, SMAs can absorb and dissipate mechanical energy by undergoing a reversible hysteretic shape change when subjected to applied mechanical cyclic loading. So, used in impact absorption and vibration damping applications. The application of SMAs spans a wide variety of industrial sectors such as aerospace, automotive, biomedical, and oil exploration.
  • 6. A BRIEF HISTORY  Discovery of martensite in steels in the 1890s by Adolf Martens.  The concept of thermoelastic martensitic transformation was introduced in 1949 by Kurdjumov and Khandros.(CuZn and CuAl alloys.)  By 1953, the occurrence of thermoelastic martensitic transformation was demonstrated in other alloys such as InTl and CuZn.  1963. The breakthrough for engineering applications occurred with the discovery of NiTi by Buehler and coworkers while investigating materials useful for heat shielding. the term “NiTiNOL” was coined for this NiTi material in honor of its discovery at the Naval Ordnance Laboratory (NOL). The term Shape Memory Effect (SME) was given to the associated shape recovery behavior. The effects of heat treatment, composition and microstructure were widely investigated.  In 1965, studies showed that the addition of a third alloying element( Co and Fe). Led to the first commercial SMA application, known as Cryofit
  • 7.  Continued research to address this issue led to the development of the NiTiNb system in 1989.  High Temperature SMAs (HTSMAs), such as TiPd, TiPt and TiAu (with transformation temperatures greater than 100 ◦C), were also developed as early as 1970 .Meanwhile, Melton and Mercier ,while studying the fatigue properties of NiTi in 1978.  Later in 1999, Miyazaki showed improved fatigue life for NiTiCu alloys.  By 1990s that NiTi stents made their commercial breakthrough.
  • 8. Phenomenology of Phase Transformation in Shape Memory Alloys  Within the typical operating temperature range, SMAs have two phases, each with a different crystal structure and therefore different properties. One is the high temperature phase called austenite (A) and the other is the low temperature phase called martensite (M). Austenite (generally cubic) has a different crystal structure from martensite (tetragonal, orthorhombic or monoclinic).  Transformation from one structure to the other occur by shear lattice distortion. Such a transformation is known as martensite.  Martensitic crystal formed can have a different orientation direction, called a variant.  The phase transition from austenite to martensite is termed the forward transformation.  When the material is heated from the martensitic phase, the crystal structure transforms back to austenite, and this transition is called reverse transformation  Four characteristic temperatures associated with the phase transformation.(Ms, Mf,As And Af)
  • 10.  The load applied must be sufficiently large to start the detwinning process.  The minimum stress required for detwinning initiation is termed the detwinning start stress (σs).  Sufficiently high load levels will result in complete detwinning of martensite where the corresponding stress level is called the detwinning finish stress (σf ).  The transformation temperatures strongly depend on the magnitude of the applied load, with higher values of applied load leading to higher transformation temperatures.  Irrespective of the nature of applied load (tension or compression), the transformation temperatures increase with an increase in the magnitude of the load.
  • 11. PSEUDOELASTIC EFFECT Transformation can also be induced by applying a sufficiently high mechanical load to the material in the austenitic phase. The result of this load is fully detwinned martensite created from austenite. If the temperature of the material is above Af , a complete shape recovery is observed upon unloading to austenite. This material behavior is called the pseudo elastic effect.
  • 12. PHASE DIAGRAM OF SMA: A diagram, illustrating the different phases in a stress-temperature space for a given SMA with fixed composition, is called the phase diagram.
  • 13. SHAPE MEMORY EFFECT:  An SMA exhibits the shape memory effect (SME) when it is deformed while in the twinned martensitic phase and then unloaded while at a temperature below As.  The strain recovered due to the phase transformation from detwinned martensite to austenite is termed as the transformation strain (εt).
  • 14. PSEUDOPLASTICITY  The pseudo elastic behavior of SMAs is associated with stress-induced transformation , which leads to strain generation during loading and subsequent strain recovery upon unloading at temperatures above Af.  Generally, the term pseudo elasticity describes both super elastic behavior and so-called rubber-like behaviour
  • 15. CYCLIC BEHAVIOR OF SMAS:  We have studied the one-way SME behavior in SMAs. Sometimes an SMA can exhibit repeatable shape changes under no applied mechanical load when subjected to a cyclic thermal load. This behavior is termed two-way shape memory effect (TWSME).  Training an SMA refers to a process of repeatedly loading the material following a cyclic thermomechanical loading path until the hysteretic response of the material stabilizes and the inelastic strain saturates.  There are limitations that reduce the usability of the two-way effect, such as smaller strains (2 %), extremely low cooling transformation forces and unknown long-term fatigue and stability
  • 16. APPLICATIONS:  Aircraft  Automobiles  Robotics  Medicines  Piping  Optometry