Abstract

Residual stresses affect the service life and cause the deformation of machined parts. Therefore, the study on the development of residual stresses during machining operation is very important. For this, analytical and numerical models have been developed to predict the residual stresses for single-step machining operation. However, the parts are usually machined with a serial of production processes. A numerical model for predicting residual stress in sequential side milling GH4169, considering initial stress, was proposed in this research. The initial residual stress distribution due to previous-step milling was considered in the proposed model. It was assumed that this initial residual stress value changed with the depth from the machined surface, while the residual stress on the identical horizontal plane was assumed with uniform distribution. The proposed numerical simulation model could predict the stress value of the machined surface, the stress value of the compression valley, and the residual stress distribution in the depth direction beneath the machined surface with high accuracy. Experimental investigations of sequential side milling GH4169 were conducted and the generated residual stresses were measured. The distribution trend and influence rule of residual stress between two sequential milling steps were analyzed. The residual stress distribution beneath the surface showed a spoon-shaped pattern. The thickness of the residual stress influence layer (RSIL) after the current milling step was affected by the depth of cut and the RSIL thickness of the previous milling step. The numerical model could predict the thickness of RSIL and optimize the depth of cut in sequential side milling.

Highlights

  • Superalloy GH4169 has been widely used in the aerospace field due to its excellent hightemperature strength, heat corrosion resistance, high-temperature oxidation resistance, and fatigue resistance [1,2]

  • The results showed a non-linear superposition relationship in the residual stress distribution between each process step

  • A numerical model for predicting the machined surface residual stress in sequential side milling GH4169 considering initial stress was proposed in this research

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Summary

Introduction

Superalloy GH4169 has been widely used in the aerospace field due to its excellent hightemperature strength, heat corrosion resistance, high-temperature oxidation resistance, and fatigue resistance [1,2]. Ma et al [11] conducted an experimental research to study the evolution of the residual stress field during multi-steps face milling. The surface after twostep turning could be obtained by the design of a double-edged turning tool in sole one-step cutting.The initial residual stress effect was neglected in the numerical simulation model of two-step turning. A numerical model for predicting machined surface residual stress in sequential side milling GH4169 considering initial stress will be proposed in this research. The initial residual stress distribution due to previous-step milling is considered in the proposed model. Effective conversion from three-dimensional (3D) side milling to two-dimensional (2D) orthogonal turning makes it easier to import the initial residual stress into the simulation model [13]. Where Vr 2 R RPM is the rotation speed and R is the tool radius

Modification equation of measured residual stress in depth
Geometry modeling and mesh controlling
Boundary conditions and initial conditions
Sequential milling experiments and measurements of residual stress
Residual stress distribution of experiment
Residual stress distribution of simulation
Conclusion
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