Additive Manufacturing (AM) or rapid prototyping technologies are presented as one of the
best options to produce customized prostheses and implants with high-level requirements in …

钛合金是航空发动机关键构件的主选材料, 切削加工是其制造工艺中最基本的加工方法之一.
切削加工产生的热-机载荷会导致钛合金表层微观组织发生复杂变化, 从而在加工表面形成表面 …

Offshore and oil & gas industries have shown the interest toward the use of dissimilar
metals, so there is the problem of their joining. The aim of this research activity was to …

The influence of microstructure (bimodal and lamellar structure) on the fatigue crack growth
(FCG) rate of Ti–6Al–3Nb–2Zr–1Mo alloy was investigated using compact-tension (CT) …

The ultrasonic fatigue tests under two three‐point bending loading modes were carried out
on TC4 specimens with the equiaxed, bimodal, and lamellar microstructure in the range of …

A turbine engine blade alloy (Ti‐8Al‐1Mo‐1V) under different heat treatment conditions was
employed to conduct ultrasonic fatigue tests to investigate the influence of the colony content …

Based on the self-built three point bending ultrasonic fatigue test system, fatigue behavior of
TC4 titanium alloy after different forging processes in high cycle fatigue (HCF) and very high …

As aero engine life increases, blade fatigue has become one of the key factors restricting the
high reliability and long service life of aero engine. In this paper, TC4 bar was treated by α+ …

The influence of microstructure on the shock-induced strengthening behavior of Ti–6Al–4V
(Ti-64) alloy was systematically investigated through plate impact experiments and quasi …