Laser melting deposition of Inconel625/Ti6Al4V bimetallic structure with Cu/V interlayers

A bimetallic structure (BS) made of Inconel625 (IN625) nickel-base superalloy with excellent high temperature properties and Ti6Al4V (TC4) titanium alloy with a light weight and a high strength has broad application prospects in aerospace engineering. However, the integrated manufacturing of the IN625/TC4 BS is a difficult research topic in the industry. In this work, the laser melting deposition (LMD) technology was used to prepare an IN625/TC4 BS without cracks and other metallurgical defects by adding Cu/V interlayers. The results show that the IN625/TC4 BS structure from the IN625 side to the TC4 one can be divided into four regions: IN625 region (region A) & RARR; Interlayers/IN625 transition region (region B) & RARR; TC4/Interlayers transition region (region C) & RARR; TC4 region (region D). The phase compositions of these regions are: & gamma;-Ni + laves & RARR; (Ni, Cu)ss + (V, Cr)ss + TiNi & RARR; & alpha;-Ti + & beta;-Ti + Ti2Ni & RARR; & alpha;-Ti + & beta;-Ti. The Vickers hardness distribution is uneven in all regions, and the highest value (about 590.0 HV) is achieved in region B. The tensile strength of the IN625/TC4 BS with Cu/V interlayers reaches nearby 514.5 & PLUSMN;9.5 MPa at room temperature, and fractures are initiated in region B.

Automated summary

In this study, a bimetallic structure (BS) consisting of Inconel625 (IN625) nickel-base superalloy and Ti6Al4V (TC4) titanium alloy was successfully prepared using laser melting deposition (LMD) technology with Cu/V interlayers to prevent cracks and defects. The BS structure can be divided into four regions with different phase compositions and Vickers hardness distribution. The tensile strength of the IN625/TC4 BS with Cu/V interlayers reached around 514.5 ± 9.5 MPa at room temperature, and fractures occurred in region B.