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A kind of processing deformation control method of aluminum alloy thick plate milling process

A technology of processing deformation and control method, which is applied in the direction of metal processing equipment, neural learning methods, genetic rules, etc., can solve the problems of influence mechanism and lack of theoretical basis, and achieve the effect of suppressing processing deformation

Active Publication Date: 2022-04-19
NANCHANG HANGKONG UNIVERSITY
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, there is still a lack of effective theoretical basis for the process parameters of grooving and the mechanism of deformation.

Method used

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  • A kind of processing deformation control method of aluminum alloy thick plate milling process
  • A kind of processing deformation control method of aluminum alloy thick plate milling process
  • A kind of processing deformation control method of aluminum alloy thick plate milling process

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Embodiment Construction

[0039] In order to facilitate the understanding of the present invention, the present invention will be described more fully below with reference to the associated drawings. Preferred embodiments of the invention are shown in the accompanying drawings. However, the present invention can be embodied in many different forms and is not limited to the embodiments described herein. On the contrary, these embodiments are provided to make the understanding of the disclosure of the present invention more thorough and comprehensive.

[0040] The invention provides a method for controlling machining deformation of an aluminum alloy thick plate during milling, comprising the following steps:

[0041] Step 1: Establish the blank finite element model, as attached figure 1 As shown, its length is l, width is w, and height is H.

[0042] Step 2: Grooving on the blank, the groove depth is H 0 , the slot width is W 0 , the groove length is L 0 ;

[0043] Step 3: In the ABAQUS software, ...

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Abstract

The invention discloses a processing deformation control method in the milling process of an aluminum alloy thick plate. The processing deformation control method of the aluminum alloy thick plate milling process comprises the following steps: Step 1: Establish a blank finite element model, its length is L, width is W, and height is H; Step 2: Groove on the blank, the groove depth is h 0 , the slot width is W 0 , the groove length is L 0 ;Step 3: In the ABAQUS software, according to the shape of the groove and the part and the initial residual stress distribution of the blank, divide the unit separation surface in the blank, and generate a mesh; Step 4: According to the material that needs to be removed during the processing of the part and its removal sequence Define the set of slot elements and the set of part elements and nodes respectively. The processing deformation control method of the aluminum alloy thick plate milling process of the present invention has a better effect of suppressing the processing deformation of the aluminum alloy member.

Description

technical field [0001] The invention relates to an aluminum alloy thick plate milling processing technology, in particular to a processing deformation control method in the aluminum alloy thick plate milling process. Background technique [0002] With the continuous development of the aviation manufacturing industry, the requirements for the performance of modern aircraft and spacecraft continue to increase, and the overall structural parts are more and more used in actual production. The overall structure is smooth in appearance and light in weight. It is better than the riveted structure in terms of stiffness, fatigue strength and various instability critical values. The application of integral structural parts is a great progress in the aviation manufacturing industry. However, due to the more complex shape of the overall structural part, the higher material removal rate, and the more stringent requirements for machining accuracy, the overall structural part is often acc...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/17G06F30/23G06F30/27G06N3/04G06N3/08G06N3/12B23C3/28G06F119/14
CPCG06F30/17G06F30/23G06F30/27G06N3/04G06N3/084G06N3/126B23C3/28G06F2119/14
Inventor 秦国华叶海潮娄维达候源君陶江
Owner NANCHANG HANGKONG UNIVERSITY
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