Linear friction welding joint uniaxial tension simulation calculation method

A linear friction welding and uniaxial stretching technology, applied in design optimization/simulation, CAD numerical modeling, sustainable transportation, etc., can solve problems such as superalloy joints that are not involved, and ensure predictability and continuity. Effect

Active Publication Date: 2021-06-11
NORTHWESTERN POLYTECHNICAL UNIV
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Problems solved by technology

[0005] In his master’s thesis “Research on Fracture Failure of Superalloys During Plastic Deformation” by Deng Jiao from Central South University, he studied the local necking law of superalloys during high-temperature tensile deformation, and analyzed the effects of deformation parameters and initial aging time on the characteristic parameters of the damage model. influence, established the mathematical expression of the characteristic parameters of the damage model based on parameters, and obtained the GTN damage model parameters of the superalloy tensile deformation, but did not involve the uniaxial tensile simulation analysis of the superalloy joint; Xu Kaixuan of Nanjing University of Aeronautics and Astronautics His master's thesis "Research on Modeling and Numerical Simulation of Ductility Fracture Behavior of GH4169 Nickel-based Alloy" has carried out theoretical modeling and numerical simulation research on the plastic deformation and ductile fracture behavior of the GH4169 nickel-based superalloy used in disks, using the inversion method The B-W model material parameters of the GH4169 alloy were optimized and estimated, and the finite element calculation and analysis of the tensile response of the GH4169 smooth and notched specimens was carried out based on the B-W model, but it was still only for the superalloy raw materials

Method used

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  • Linear friction welding joint uniaxial tension simulation calculation method
  • Linear friction welding joint uniaxial tension simulation calculation method
  • Linear friction welding joint uniaxial tension simulation calculation method

Examples

Experimental program
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Effect test

Embodiment 1

[0085] The specific method of this embodiment includes the following steps:

[0086] (1) Stress data collection steps at the sampling position of the post-weld stress nephogram:

[0087] The steps are based on the post-processing analysis of the superalloy linear welding stress nephogram, respectively collecting the stress data S11, S22, S33 and S12 at five positions selected in the joint, and the sampling positions of the micro-tensile specimens are shown in Figure 4, BRIEF DESCRIPTION OF THE DRAWINGS 5 is a graph of stress data at five sampling locations.

[0088] (2) Steps for establishing a micro-stretch geometric model:

[0089] The part module in ABAQUS is used to establish the micro-tensile geometric model. According to the different sampling positions, the heat-affected zone of the weld zone and the base metal area of ​​the micro-tensile geometric model are divided, and the 5 sampling points are respectively located in the center of the micro-tensile sample. . The t...

Embodiment 2

[0100] (1) Steps for establishing a micro-stretch geometric model:

[0101] The same as the geometric model modeling steps of Node 1 in Embodiment 1.

[0102] (2) Define the mechanical parameters, thermodynamic parameters and GTN damage constitutive parameters of the micro-tensile specimen of the linear welded joint. Steps:

[0103] Same as the material property setting of Node 1 in Example 1.

[0104] (3) Boundary conditions and predefined field setting steps:

[0105] It is the same as the prestress application steps of node 1 in embodiment 1. In this step, the predefined temperatures of the micro-tensile specimens are set as 293°C, 400°C and 650°C respectively, and there are three finite element models in total.

[0106] (4) Grid attributes and control steps:

[0107] Same as the grid attributes and control steps of node 1 in Embodiment 1.

[0108] (5) Calculation and post-processing analysis steps:

[0109] Post-processing analysis obtained the micro-tensile fracture...

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Abstract

The invention relates to a linear friction welding joint uniaxial tension simulation calculation method, and belongs to the technical field of welding and fracture mechanical numerical simulation. The method comprises the following steps: dividing welding model sub-regions, and distributing region serial numbers; establishing a high-temperature alloy linear friction welding finite element model; determining the size and the cutting position of a micro-tensile sample; and establishing a micro-stretching finite element model of the high-temperature alloy linear friction welding joint. Based on a high-temperature alloy linear friction welding numerical simulation result, the welding stress final states of different sub-regions serve as the stress initial state of joint micro-stretching, and the mechanical property difference of different regions of a high-temperature alloy linear welding joint micro-stretching model is fully considered. By means of calculation forming, calculation continuity is guaranteed, predictability of a stress concentration area is guaranteed, and the method has important value and significance on theoretical research of fracture mechanics of the high-temperature alloy linear welding joint.

Description

technical field [0001] The invention belongs to the technical field of numerical simulation of welding and fracture mechanics, and relates to the formation process, mechanism and physical field evolution law of linear friction welding of high-temperature-resistant materials for aerospace, and the dynamic evolution law and exploration of fracture damage of linear welded joints. Specifically, it is a uniaxial tensile simulation calculation method of a linear friction welding joint. Background technique [0002] Linear friction welding is a thermal-mechanical coupling (energy conversion) process and solid-state metallurgical process under high temperature and high pressure, which overcomes the limitations of other friction welding processes on the shape of the welded workpiece. High-temperature alloys are irreplaceable key materials for high-temperature components such as turbine blades, guide vanes, high-pressure compressor disks, and combustion chambers of aviation, aerospace...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/23G06F111/10
CPCG06F30/23G06F2111/10Y02P10/20
Inventor 杨夏炜王艳莹彭冲徐雅欣李文亚
Owner NORTHWESTERN POLYTECHNICAL UNIV
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