Abstract
As one of the relatively new titanium (Ti) alloys in the engineering field, β-Ti alloy–Ti55531 has attracted a great deal of attention due to its excellent mechanical properties, while a few research papers on weldability and the post-weld heat treatment (PWHT) process of Ti55531 have been reported. Based on an orthogonal experiment design, the parameters of laser beam welding (LBW) of Ti55531 alloy with a thickness of 2 mm were optimized. Moreover, the influences of welding parameters and PWHT on the microstructures and performance of the laser-welded joint of Ti55531 were analyzed. The results showed that, for microstructures in different zones of as-welded joints of Ti55531: three forms of α phases (i.e., equiaxial αp phase, lamellar αS phase, and αGB phase at grain boundaries) were observed in base metal (BM); in the heat affected zone (HAZ), part of lamellar αS phase had dissolved while equiaxial αp phase had grown; the fusion zone (FZ) mainly consisted of β phase, which presented as coarse columnar crystals. After the PWHT process, the microstructures of the welded joint were changed: in the BM zone, α phase at grain boundary disappeared and lamellar α phase decreased; in the HAZ, the edge of αp phase obviously dissolved; in the FZ, plenty of compact needle-like α phases were observed. The tensile strength of the as-welded joint was about 940 MPa and then increased to 1161 MPa after PWHT, which were 78.4% and 96.8% of that of the original BM respectively. The fracture position transformed from the interface between the FZ and HAZ to the BM during tensile tests after PWHT.
Highlights
Some important structural parts, such as airframes and engines, need to achieve light weight by applying materials with high strength and low density [1,2]
The results indicated that the obtained laser beam welding (LBW) joint showed higher hardness of the fusion zone (FZ) and higher values of ultimate tensile strength than those joints previously obtained with other joining processes [20]
It can be seen from the Figure that after undergoing post-weld heat treatment (PWHT), compact lamellar α phases re-occurred in the FZ
Summary
Some important structural parts, such as airframes and engines, need to achieve light weight by applying materials with high strength and low density [1,2]. The nominal component of Ti55531 alloy is Ti-5Al-5Mo-5V-3Cr-1Zr. The nominal component of Ti55531 alloy is Ti-5Al-5Mo-5V-3Cr-1Zr This type of Ti alloy without an Fe element shows the advantages of traditional high-strength and high-toughness Ti alloys and avoids the drawbacks of the majority of traditional Ti alloys. Ti55531 alloy exhibits various advantages including less sensitivity to segregation, good hardenability, excellent strength and high fracture toughness, and it is extremely applicable for manufacturing parts bearing huge stress, such as structural parts, landing gears, wings of airplanes, and engine pylon [3].
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