Pseudoelasticity

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In materials science, pseudoelasticity, sometimes called superelasticity, is an elastic (reversible) response to an applied stress, caused by a phase transformation between the austenitic and martensitic phases of a crystal. It is exhibited in shape-memory alloys.

Contents

Overview

Pseudoelasticity is from the reversible motion of domain boundaries during the phase transformation, rather than just bond stretching or the introduction of defects in the crystal lattice (thus it is not true super elasticity but rather pseudo elasticity). Even if the domain boundaries do become pinned, they may be reversed through heating. Thus, a pseudoelastic material may return to its previous shape (hence, shape memory) after the removal of even relatively high applied strains. One special case of pseudoelasticity is called the Bain Correspondence. This involves the austenite/martensite phase transformation between a face-centered crystal lattice (FCC) and a body-centered tetragonal crystal structure (BCT). [1]

This behavior differs fundamentally from ordinary elasticity and plasticity:

Superelastic alloys belong to the larger family of shape-memory alloys. When mechanically loaded, a superelastic alloy deforms reversibly to very high strains (up to 10%) by the creation of a stress-induced phase. When the load is removed, the new phase becomes unstable and the material regains its original shape. Unlike shape-memory alloys, no change in temperature is needed for the alloy to recover its initial shape.

Superelastic devices take advantage of their large, reversible deformation and include antennas, eyeglass frames, and biomedical stents.

Pseudoelasticity of nickel titanium (Nitinol)

Superelasticity is most famously exhibited by shape-memory alloys (SMAs) such as nickel-titanium (NiTi), also known as Nitinol. [2]

The key points of the mechanism for Nitinol are:

Stress–strain behavior and characteristics

The stress–strain curve of a superelastic alloy (like NiTi) has a distinctive shape, reflecting the sequence of phase transformations during loading and unloading

Loading

During loading, three regimes are observed

  1. Elastic Austenite: At small strains , the material responds with ordinary elastic behavior as austenite. Stress rises approximately linearly with strain () up to the point where the martensitic transformation begins. The end of this stage is around the Martensite-Start strain (corresponding to a stress ). For NiTi, this might be on the order of ~0.5–1% strain and a few hundred MPa of stress.
  2. Stress Plateau – Martensitic Transformation: Once the stress is high enough to trigger martensite nucleation, the stress remains roughly constant over a considerable strain interval. In this plateau region, additional strain is being accommodated not by increasing stress (much), but by the progressive conversion of austenite to martensite (phase transformation). The plateau stress level is often around 400–600 MPa in NiTi (depending on alloy/process), and the plateau strain range can span 5–8% strain
  3. Elastic Martensite & Hardening: Once the transformation to martensite is almost complete (at Martensite-Finish strain ), further strain requires deforming the martensite itself or aligning the last remaining variants. The stress begins to rise steeply again with strain. Martensite’s elastic modulus may differ from austenite’s (often somewhat lower), but the curve climbs until ultimate stress/strain or until the loading is stopped. If the material is loaded to a high strain (beyond the transformation strain), some plastic deformation of martensite can also occur, which would manifest as deviation from full strain recovery later

Mathematically, an idealized piecewise model for the superelastic loading curve can be written as:

where is the stress, is the strain, E is the Young's modulus, and are the start and finish strains for the martensitic transformation, is the stress at the start of the martensitic transformation, and is a material parameter.

In an ideal case, so the stress plateau is flat (perfectly constant stress during phase change). For simplicity, the above model assumes the transformation finish stress (flat plateau). [3]

Unloading

On unloading, the reverse sequence occurs, but importantly at a lower stress level. As soon as the load is released from the fully martensitic state, the material unloads elastically in martensite briefly, then enters a reverse transformation plateau (martensite reverts to austenite) at a stress which is below . Finally, once all martensite has turned back to austenite (at ), the last part of unloading is just elastic recovery of austenite. Thus, the unloading curve is shifted down relative to loading. The result is a hysteresis loop in the stress–strain diagram. The area inside this loop represents the energy dissipated per cycle (as heat) due to internal friction and phase transformation entropy change.

Size effects

Recently, there have been interests of discovering materials exhibiting superelasticity in nanoscale for MEMS (Microelectromechanical systems) application. The ability to control the martensitic phase transformation has already been reported. [4] But the behavior of superelasticity has been observed to have size effects in nanoscale.

Qualitatively speaking, superelasticity is the reversible deformation by phase transformation. Therefore, it competes with the irreversible plastic deformation by dislocation motion. At nanoscale, the dislocation density and possible Frank–Read source sites are greatly reduced, so the yield stress is increased with reduced size. Therefore, for materials exhibiting superelasticity behavior in nanoscale, it has been found that they can operate in long-term cycling with little detrimental evolution. [5] On the other hand, the critical stress for martensitic phase transformation to occur is also increased because of the reduced possible sites for nucleation to begin. Nucleation usually begins near dislocation or at surface defects. But for nanoscale materials, the dislocation density is greatly reduced, and the surface is usually atomically smooth. Therefore, the phase transformation of nanoscale materials exhibiting superelasticity is usually found to be homogeneous, resulting in much higher critical stress. [6] Specifically, for Zirconia, where it has three phases, the competition between phase transformation and plastic deformation has been found to be orientation dependent, [7] indicating the orientation dependence of activation energy of dislocation and nucleation. Therefore, for nanoscale materials suitable for superelasticity, one should research on the optimized crystal orientation and surface roughness for most enhanced superelasticity effect.

Applications

Biomedical stents and medical devices

One of the most celebrated uses of superelastic NiTi is in self-expanding stents for cardiovascular surgery. A NiTi stent can be crimped and inserted into a blood vessel, once released at body temperature, it springs back to a larger diameter to prop the vessel open. The superelastic effect allows the stent to apply a consistent outward force over a range of deformations and to resist kinking.

Eyeglass frames and consumer products

Eyewear frames made of NiTi (or Cu-based SMAs) can be bent dramatically (e.g. twisted or sat on) and will recover their original shape. This durability has made flexible “memory metal” glasses a popular consumer product. Similarly, some high-end sports equipment and cell phone antennas have used superelastic alloys to withstand deformation.

Aerospace and morphing structures

The aerospace industry exploits superelasticity for lightweight, adaptive components. Superelastic actuators and damping links can be used in deployable structures or morphing wings. For instance, a superelastic SMA rod or tendon can act as a passive actuator that accommodates deformation when a certain load is reached (protecting structures by “giving” and then springing back). Landing gear and aircraft engine components have been explored that utilize NiTi inserts to absorb impact or vibration and then self-center. The high energy absorption per unit volume and the ability to sustain cyclic deformation make superelastic alloys appealing for these purposes.

In satellite applications, temperature-controlled SMA elements (combining superelasticity and shape-memory effect) are used for deployable antennas and solar panels, thanks to their reliability and compactness.

See also

References

  1. Bhadeshia, H. K. D. H. "The Bain Correspondence" (PDF). Materials Science and Metallurgy. University of Cambridge.
  2. Chen, Weimei; Xi, Rui; Jiang, Hao; Li, Xiaoqiang; Dong, Guiwei; Wang, Xiebin (2023-08-26). "Superelasticity of Geometrically Graded NiTi Shape Memory Alloys". Metals. 13 (9): 1518. doi: 10.3390/met13091518 . ISSN   2075-4701.
  3. Otsuka, K.; Ren, X. (2005-07-01). "Physical metallurgy of Ti–Ni-based shape memory alloys" . Progress in Materials Science. 50 (5): 511–678. doi:10.1016/j.pmatsci.2004.10.001. ISSN   0079-6425.
  4. Thorsten Krenke; et al. (2007). "Magnetic superelasticity and inverse magnetocaloric effect in Ni-Mn-In". Physical Review B. 75 (10) 104414. arXiv: 0704.1243 . Bibcode:2007PhRvB..75j4414K. doi:10.1103/PhysRevB.75.104414. S2CID   29563170.
  5. J. San Juan; et al. (2014). "Long-term superelastic cycling at nano-scale in Cu-Al-Ni shape memory alloy micropillars". Applied Physics Letters. 104 (1). AIP: 011901. Bibcode:2014ApPhL.104a1901S. doi:10.1063/1.4860951.
  6. J. San Juan; et al. (2013). "superelasticity and shape memory at nano-scale: size effects on the martensitic transformation". Journal of Alloys and Compounds. 577. Elsevier: S25 –S29. doi:10.1016/j.jallcom.2011.10.110.
  7. Ning Zhang; et al. (2016). "Competing mechanisms between dislocation and phase transformation in plastic deformation of single crystalline yttria-stabilized tetragonal zirconia nanopillars". Acta Materialia. 120: 337–347. arXiv: 1607.03141 . Bibcode:2016AcMat.120..337Z. doi:10.1016/j.actamat.2016.08.075. S2CID   118512427.