Investigation of Strain Fatigue Behavior for Inconel 625 with Laser Shock Peening

Abstract

With excellent creep resistance, high-temperature thermal strength and high-temperature fatigue strength, Inconel 625 is widely applied to fabricate structural components in the aerospace field, where fatigue life is a key point. Laser shock peening (LSP) is considered to improve the fatigue strength and fatigue crack growth resistance of metal materials. The present work was conducted to investigate the influence of LSP on strain-controlled fatigue behavior of Inconel 625. The surface microstructures of specimens before and after LSP were observed by transmission electron microscope (TEM). The strain-controlled fatigue loading tests with different strain amplitudes ranging from 0.4% to 1.2% were carried out on the specimens, and the topography of fracture appearance was examined by scanning electron microscope (SEM). The investigations showed that the specimens with LSP presented fewer crack initiations, shorter fatigue striations space and smaller dimples or micropores, which account for the enhancement of the fatigue life for the LSP specimens. Furthermore, the plastic deformation, ultra-fine grains, twins and dislocations caused by LSP could prevent crack initiation, crack propagation and ultimate fracture, hence prolonging the fatigue life of the Inconel 625. In addition, it was revealed that the cyclic strain hardening as well as cyclic strain softening remains almost the same to Inconel 625 with or without LSP.

Cavitation Erosion Prevention Using Laser Shock Peening: Development of a Predictive Evaluation System

“…Laser Shock Peening (LSP), an advanced technique widely used in aerospace and other critical military fields, has gained a lot of attention in the field of cavitation erosion resistance in recent years [ 14 , 15 , 16 , 17 ]. The principle of LSP technic is using laser beams to generate plasma shock waves to act on metallic materials to improve their fatigue and corrosion resistance [ 18 , 19 , 20 , 21 , 22 ]. S. Zabeen et al used LSP to study the residual stress field around aero-engine specimens.…”