scholarly journals Cutting Forces Modeling in Finish Turning of Inconel 718 Alloy with Round Inserts

2011 ◽  
Vol 223 ◽  
pp. 75-84 ◽  
Author(s):  
Sebastien Campocasso ◽  
Jean Philippe Costes ◽  
Gérard Poulachon ◽  
Alexis Perez Duarte
Keyword(s):  
Cutting Forces ◽  
Inconel 718 ◽  
Orthogonal Design ◽  
Generic Model ◽  
Inconel 718 Alloy ◽  
Cutting Coefficients ◽  
Homogeneous Matrix ◽  
Applied Forces ◽  
Experimental Values ◽  
Clearance Face

In turning, the applied forces have to be known as accurately as possible, especially in the case of difficult-to-cut materials for aircraft workpieces finishing operations. Traditionally, edge discretisation methodology based on local cutting laws is used to determine the cutting forces and results are usually considered suitable. Nevertheless, only the rake face is considered in most of studies and the cutting relations are determined by direct identification with a straight edge. This study deals with finishing operations of Inconel 718 alloy with one type of round insert. The main objective is to formulate a novel cutting forces model, taking into account the clearance face. First, a generic model based on a geometrical description using homogeneous matrix transformation is presented. Then, cutting coefficients are identified by inverse identification from experimental measurements distributed with an orthogonal design experiment including tool wear. Finally, modeling and experimental values of the cutting forces are compared and the identified model is analysed.

A cutting forces model for milling Inconel 718 alloy based on a material constitutive law

2012 ◽  
Vol 227 (8) ◽  
pp. 1761-1775 ◽  
Author(s):  
HZ Li ◽  
J Wang
Keyword(s):  
Cutting Forces ◽  
Inconel 718 ◽  
Shear Plane ◽  
Material Model ◽  
Constitutive Law ◽  
Percentage Error ◽  
Force Model ◽  
Inconel 718 Alloy ◽  
Average Percentage ◽  
Constitutive Material Model

This article presents a cutting force model for the milling of Inconel 718 whose machinability is considered to be very poor. The Johnson–Cook constitutive material model is used to determine the flow stress of Inconel 718 while the shear angle is determined based on a shear plane model assuming that the total energy on the shear plane plus the energy on the rake face is minimum. The temperature in the machining region is determined by using an iterative process. Finally, the cutting forces on each tooth of the milling cutter are calculated from its chip load considering the oblique cutting effects. The model is then verified by comparing the model predictions with the experimental data under the corresponding conditions, which shows a relatively good agreement with an average percentage error of 10.5% along the feed and normal directions.

Finite Element Simulation of the Cutting Process for Inconel 718 Alloy Using a New Material Constitutive Model

2016 ◽  
Vol 693 ◽  
pp. 1046-1053
Author(s):  
Xiang Yu Wang ◽  
Chuan Zhen Huang ◽  
Jun Wang ◽  
Bin Zou ◽  
Guo Liang Liu ◽  
...  
Keyword(s):  
Finite Element ◽  
Constitutive Model ◽  
Finite Element Simulation ◽  
Cutting Forces ◽  
Inconel 718 ◽  
Cutting Process ◽  
Inconel 718 Alloy ◽  
Cutting Edge Radius ◽  
Material Constitutive Model ◽  
Element Simulation

Inconel 718 alloy is a typical difficult-to-cut material and widely used in the aerospace industry. Finite element simulation is an efficient method to investigate the cutting process, whereby a work material constitutive model plays an important role. In this paper, finite element simulation of the cutting process for Inconel 718 alloy using a new material constitutive model for high strain rates is presented. The effect of tool cutting edge radius on the cutting forces and temperature is then investigated with a view to facilitate cutting tool design. It is found that as the cutting edge radius increases, the characteristics of tool-work friction and the material removal mechanisms change, resulting in variation in cutting forces and temperature. It is shown that a smaller cutting edge radius is preferred to reduce the cutting forces and cutting temperature.

scholarly journals Cutting Forces during Inconel 718 Orthogonal Turn-Milling

Materials ◽  
2021 ◽  
Vol 14 (20) ◽  
pp. 6152
Author(s):  
Agata Felusiak-Czyryca ◽  
Marek Madajewski ◽  
Paweł Twardowski ◽  
Martyna Wiciak-Pikuła
Keyword(s):  
Tool Wear ◽  
Cutting Force ◽  
Cutting Forces ◽  
Inconel 718 ◽  
Material Removal ◽  
Harsh Environments ◽  
Ability To Work ◽  
Inconel 718 Alloy ◽  
Turn Milling

Inconel 718 is a material often used in the aerospace and marine industries due to its properties and ability to work in harsh environments. However, its machining is difficult, and therefore methods are sought to facilitate this process. One of such methods is turn-milling. This paper presents the forces during orthogonal turn-milling of the Inconel 718 alloy. In this machining, both the side and the end edge are involved in the material removal, which causes the tool to be more loaded. The forces during turn-milling can be up to 50% higher than in the case of milling, which causes damage to the tool. Tool wear during machining has a significant impact on the values of the cutting force proportional coefficients. In the case of the tested material, it is important to take it into account when creating cutting force models.

scholarly journals A Comparative Analysis of Laser Additive Manufacturing of High Layer Thickness Pure Ti and Inconel 718 Alloy Materials Using Finite Element Method

Materials ◽  
2021 ◽  
Vol 14 (4) ◽  
pp. 876 ◽  
Author(s):  
Sapam Ningthemba Singh ◽  
Sohini Chowdhury ◽  
Yadaiah Nirsanametla ◽  
Anil Kumar Deepati ◽  
Chander Prakash ◽  
...  
Keyword(s):  
Finite Element Method ◽  
Finite Element ◽  
Layer Thickness ◽  
Inconel 718 ◽  
Laser Power ◽  
Scanning Speed ◽  
Laser Additive Manufacturing ◽  
Inconel 718 Alloy ◽  
Melt Pool ◽  
High Layer

Investigation of the selective laser melting (SLM) process, using finite element method, to understand the influences of laser power and scanning speed on the heat flow and melt-pool dimensions is a challenging task. Most of the existing studies are focused on the study of thin layer thickness and comparative study of same materials under different manufacturing conditions. The present work is focused on comparative analysis of thermal cycles and complex melt-pool behavior of a high layer thickness multi-layer laser additive manufacturing (LAM) of pure Titanium (Ti) and Inconel 718. A transient 3D finite-element model is developed to perform a quantitative comparative study on two materials to examine the temperature distribution and disparities in melt-pool behaviours under similar processing conditions. It is observed that the layers are properly melted and sintered for the considered process parameters. The temperature and melt-pool increases as laser power move in the same layer and when new layers are added. The same is observed when the laser power increases, and opposite is observed for increasing scanning speed while keeping other parameters constant. It is also found that Inconel 718 alloy has a higher maximum temperature than Ti material for the same process parameter and hence higher melt-pool dimensions.

Corrosion Behavior of a Selective Laser Melted Inconel 718 Alloy in a 3.5 wt.% NaCl Solution

2021 ◽  
Author(s):  
Yanbing Tang ◽  
Xinwang Shen ◽  
Yanxin Qiao ◽  
Lanlan Yang ◽  
Jian Chen ◽  
...  
Keyword(s):  
Corrosion Behavior ◽  
Inconel 718 ◽  
Nacl Solution ◽  
Inconel 718 Alloy

scholarly journals Very-High-Cycle Fatigue Behavior of Inconel 718 Alloy Fabricated by Selective Laser Melting at Elevated Temperature

Materials ◽  
2021 ◽  
Vol 14 (4) ◽  
pp. 1001
Author(s):  
Zongxian Song ◽  
Wenbin Gao ◽  
Dongpo Wang ◽  
Zhisheng Wu ◽  
Meifang Yan ◽  
...  
Keyword(s):  
Elevated Temperature ◽  
Selective Laser Melting ◽  
Fatigue Resistance ◽  
Inconel 718 ◽  
High Cycle Fatigue ◽  
Cycle Fatigue ◽  
Laser Melting ◽  
Inconel 718 Alloy ◽  
Very High Cycle Fatigue ◽  
Very High

This study investigates the very-high-cycle fatigue (VHCF) behavior at elevated temperature (650 °C) of the Inconel 718 alloy fabricated by selective laser melting (SLM). The results are compared with those of the wrought alloy. Large columnar grain with a cellular structure in the grain interior and Laves/δ phases precipitated along the grain boundaries were exhibited in the SLM alloy, while fine equiaxed grains were present in the wrought alloy. The elevated temperature had a minor effect on the fatigue resistance in the regime below 108 cycles for the SLM alloy but significantly reduced the fatigue strength in the VHCF regime above 108 cycles. Both the SLM and wrought specimens exhibited similar fatigue resistance in the fatigue life regime of fewer than 107–108 cycles at elevated temperature, and the surface initiation mechanism was dominant in both alloys. In a VHCF regime above 107–108 cycles at elevated temperature, the wrought material exhibited slightly better fatigue resistance than the SLM alloy. All fatigue cracks are initiated from the internal defects or the microstructure discontinuities. The precipitation of Laves and δ phases is examined after fatigue tests at high temperatures, and the effect of microstructure on the formation and the propagation of the microstructural small cracks is also discussed.

Microstructure and Wear Properties of Laser-clad NiCo Alloy Coating on Inconel 718 Alloy

2021 ◽  
pp. 160412
Author(s):  
Tao Wang ◽  
Chao Wang ◽  
Juanjuan Li ◽  
Linjiang Chai ◽  
Xing Hu ◽  
...  
Keyword(s):  
Inconel 718 ◽  
Alloy Coating ◽  
Wear Properties ◽  
Inconel 718 Alloy
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