4.6 Article

The Influence of the Soaking Temperature Rotary Forging and Solution Heat Treatment on the Structural and Mechanical Behavior in Ni-Rich NiTi Alloy

Journal

MATERIALS
Volume 15, Issue 1, Pages -

Publisher

MDPI
DOI: 10.3390/ma15010063

Keywords

shape-memory alloys; NiTi; thermomechanical process; synchrotron radiation; heat treatments

Funding

  1. FEDER funds through COMPETE2020 -Programa Operacional Competitividade e Internacionalizacao (POCI) [PTDC/CTM-CTM/29101/2017POCI-01-0145-FEDER-029101]
  2. national funds (PIDDAC) through FCT/MCTES
  3. FEDER funds through the program COMPETE-Programa Operacional Factores de Competitividade
  4. FCT-Fundacao para a Ciencia e a Tecnologia [UIDB/EMS/00285/2020]
  5. CENIMAT/I3N by national funds through the FCT-Fundacao para a Ciencia e a Tecnologia, I.P. [UIDB/50025/2020-2023]
  6. CAPES [APQ-1 2009/02 E-26/110.414/2010, APQ-1 2011-2 E-26/110.269.2012, E-26/111.435/2012-CsF/Brazil-BEX 11943-13-0]
  7. CNPq [307798/2015-1]
  8. project CALIPSOplus from the EU Framework Programme for Research and Innovation HORIZON 2020 [730872]

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The structural and thermophysical characteristics of an Ni-rich NiTi alloy rod were studied. The suitable reheating between forging process steps is crucial for the structural characteristics of the product. The solution heat treatment at 950 degrees C/120 min was found to be the most suitable condition for producing materials with a superelasticity effect.
The structural and thermophysical characteristics of an Ni-rich NiTi alloy rod produced on a laboratory scale was studied. The soak temperature of the solution heat-treatment steps above 850 degrees C taking advantage of the precipitate dissolution to provide a matrix homogenization, but it takes many hours (24 to 48) when used without thermomechanical steps. Therefore, the suitable reheating to apply between the forging process steps is very important, because the product's structural characteristics are dependent on the thermomechanical processing history, and the time required to expose the material to high temperatures during the processing is reduced. The structural characteristics were investigated after solution heat treatment at 900 degrees C and 950 degrees C for 120 min, and these heat treatments were compared with as-forged sample structural characteristics (one hot deformation step after 800 degrees C for a 30 min reheat stage). The phase-transformation temperatures were analyzed through differential scanning calorimetry (DSC), and the structural characterization was performed through synchrotron radiation-based X-ray diffraction (SR-XRD) at room temperature. It was observed that the solution heat treatment at 950 degrees C/120 min presents a lower martensitic reversion finish temperature (A(f)); the matrix was fully austenitic; and it had a hardness of about 226 HV. Thus, this condition is the most suitable for the reheating stages between the hot forging-process steps to be applied to this alloy to produce materials that can display a superelasticity effect, for applications such as crack sensors or orthodontic archwires.

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