2021
DOI: 10.1016/j.jmatprotec.2021.117060
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Understanding the deformation and fracture mechanisms in backward flow-forming process of Ti-6Al-4V alloy via a shear modified continuous damage model

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Cited by 19 publications
(11 citation statements)
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“…As a matter of fact, titanium alloys are widely used in aerospace, automotive, and biomedical and chemical industries due to their superior properties, such as their corrosion resistance and high strength-to-weight ratio [19][20][21][22][23]. In such a context, Ti-6Al-4V here examined has excellent tensile (tensile strength ≥ 895 MPa) and fatigue strength (equal to about 460MPa at a number of loading cycles of 109 under rotating bending), as well as high resistance to a wide spectrum of corrosive environments, with respect to other titanium based alloys, due to its inclination to form protective surface oxides [24][25][26][27][28][29][30][31][32][33][34][35]. As such, it is used in lifelimit components of civil aviation engines and as fractured critical components of military engines [36][37][38][39].…”
Section: Introductionmentioning
confidence: 99%
“…As a matter of fact, titanium alloys are widely used in aerospace, automotive, and biomedical and chemical industries due to their superior properties, such as their corrosion resistance and high strength-to-weight ratio [19][20][21][22][23]. In such a context, Ti-6Al-4V here examined has excellent tensile (tensile strength ≥ 895 MPa) and fatigue strength (equal to about 460MPa at a number of loading cycles of 109 under rotating bending), as well as high resistance to a wide spectrum of corrosive environments, with respect to other titanium based alloys, due to its inclination to form protective surface oxides [24][25][26][27][28][29][30][31][32][33][34][35]. As such, it is used in lifelimit components of civil aviation engines and as fractured critical components of military engines [36][37][38][39].…”
Section: Introductionmentioning
confidence: 99%
“…Zhang et al [20]investigated the mechanisms underlying deformation and fracture for Ti-6Al-4V alloys under different heat treatments and noted that excellent hardening and deforming behaviour can be achieved at the beta-transus temperature (980 °C). Further, Singh et al [21] suggested that the increase of cooling rate may increase the hardening effects. This was principally ascribed to the maintenance of constant temperature and rapid cooling rate on surface which increased the volume of ′-martensite and grain refinement within the microstructure.…”
Section: Introductionmentioning
confidence: 99%
“…The results showed that Lemaitre criterion could effectively predict the cracking location, but the prediction location of C&L criterion was inconsistent with the reality. Singh [12] IOP Publishing doi:10.1088/1757-899X/1270/1/012038 2 compared the damage behavior of backward spinning of single roller, three roller and wedge feed, and found that the stress state of the maximum damage location was different, but all fracture occurred under tensile stress state. Due to the different width of stiffeners, the spinning forming process is more complicated and uneven material flowing is more prominent.…”
Section: Introductionmentioning
confidence: 99%