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With the development of technology in aerospace, medical devices and other fields, high-performance difficult-to-machine materials have been widely used in these fields due to their good comprehensive mechanical properties. However, when using traditional machining methods, it is difficult to ensure the machining accuracy and surface quality, and at the same time, there are problems such as serious tool wear and low machining efficiency. Laser-assisted machining (LAM) technology is an advanced manufacturing process that softens the material in the machining area through the preheating effect of the laser, thus reducing the surface hardness of the material and improving the machinability of the material, which has the advantages of high efficiency and economy in machining difficult-to-machine materials. This paper introduces the common methods of establishing thermal models and simulation modeling of removal behavior in the LAM material removal process, summarizes the research progress on the removal behavior of LAM processing of various difficult-to-machine materials, and analyzes the shortcomings and challenges of the current research. Finally, the key issues of LAM material removal mechanism are proposed, and the development direction of LAM material removal technology is envisioned in order to provide a reference for the research and development in this field.
With the development of technology in aerospace, medical devices and other fields, high-performance difficult-to-machine materials have been widely used in these fields due to their good comprehensive mechanical properties. However, when using traditional machining methods, it is difficult to ensure the machining accuracy and surface quality, and at the same time, there are problems such as serious tool wear and low machining efficiency. Laser-assisted machining (LAM) technology is an advanced manufacturing process that softens the material in the machining area through the preheating effect of the laser, thus reducing the surface hardness of the material and improving the machinability of the material, which has the advantages of high efficiency and economy in machining difficult-to-machine materials. This paper introduces the common methods of establishing thermal models and simulation modeling of removal behavior in the LAM material removal process, summarizes the research progress on the removal behavior of LAM processing of various difficult-to-machine materials, and analyzes the shortcomings and challenges of the current research. Finally, the key issues of LAM material removal mechanism are proposed, and the development direction of LAM material removal technology is envisioned in order to provide a reference for the research and development in this field.
Objective Laserdirected energy deposition (LDED) is an effective technique for processing Inconel 718. However, because of the overlap of cladding tracks and the stacking effect of the deposition layers with unmelted powders, the processing accuracy and surface quality of the asdeposited parts are poor; thus, subsequent substrate processing must be performed before use. Electrochemical machining (ECM) can effectively improve machining accuracy and surface quality and has a wide range of applications in the precision manufacturing of difficulttoprocess metals (such as nickelbased superalloys). Therefore, ECM is used for the subsequent substrate processing of LDED -Inconel 718 components. However, the processing quality of LDED components with inhomogeneous microstructures is unclear, particularly when nonwaterbased electrolytes are used. Therefore, the microstructural characteristics and dissolution behavior of the constituent phases of the LDED -Inconel 718 alloy under a pulsed current and ethylene glycol electrolyte are systematically investigated to improve the surface quality of the LDED -Inconel 718 alloy.Methods In this study, the LDED -Inconel 718 alloy is used as the research object. The parameters of the highfrequency narrowpulse current with a frequency of 30 -100 kHz, duty cycle of 30% -80%, and saturated NaCl glycol electrolyte are employed to perform electrolyte jet machining (EJM) experiments. The dendritic morphologies and constituent phases of the asdeposited Inconel 718 alloy and the micromorphologies of the machined surface after the EJM experiments are characterized using scanning electron microscope (SEM). Confocal laser microscope is performed to measure the central region of the groove along the Xaxis. The surfacemachining quality of the groove is characterized based on the surface roughness, and the machining precision is evaluated based on the depthtowidth ratio of the groove profile. Results and DiscussionsThe results show that the microstructure of the asdeposited Inconel 718 alloy is composed of the γ matrix phase, Nbsegregated γ phase, and interdendritic phase (mainly the γ/Laves eutectic phase), as shown in Fig. 2. At a current density of 10.50 A/cm 2 , the surface roughness increases with increasing pulse frequency, and the smallest surface roughness (R a = 1.562 μm) and highest machining accuracy (Fig. 5) are obtained when the pulse frequency is 30 kHz. The surface roughness first decreases and then increases with an increase in the duty cycle, whereas the machining precision is optimum when the duty cycle is 60% (Fig. 7). In the directcurrent mode, the surface roughness decreases with increasing current density. When the current density reaches 10.50 A/cm 2 , the surface quality is the best (R a =0.526 μm). This is because a high current density can easily induce the formation of surfacesupersaturated salt films and effectively inhibit selective dissolution and reduce the surface roughness. However, in terms of the machining accuracy, the processing localization in the highfrequency...
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