CN111737828A - Calculation method of panel rebound warpage and optimization method of panel rebound warpage - Google Patents
Calculation method of panel rebound warpage and optimization method of panel rebound warpage Download PDFInfo
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- CN111737828A CN111737828A CN201910220390.6A CN201910220390A CN111737828A CN 111737828 A CN111737828 A CN 111737828A CN 201910220390 A CN201910220390 A CN 201910220390A CN 111737828 A CN111737828 A CN 111737828A
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- 238000005457 optimization Methods 0.000 title abstract description 8
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- 238000012545 processing Methods 0.000 description 10
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Abstract
The invention relates to a method for calculating the rebound warpage of a panel, which provides a first panel rebound warpage formula to calculate the rebound warpage of the panel under different panel materials. The invention also provides an optimization method for the rebound and warpage of the panel, which comprises the following steps: acquiring the maximum radial diameter of a panel to be manufactured; obtaining material parameters of a panel material, wherein the material parameters comprise an elastic modulus and a yield strength of the panel material; calculating the resilience warping of the panel when the panel to be manufactured is manufactured by adopting the panel material according to a first panel resilience warping formula; and (4) determining qualified panel materials. The invention can optimize the resilience and warping of the panel and reduce the rejection rate.
Description
Technical Field
The application relates to the field of panel processing, in particular to a calculation method for panel rebound warpage and an optimization method for panel rebound warpage.
Background
Panel parts are used as members of vehicle bodies, furniture and the like, and are generally produced by processing panels by molds according to design requirements. Generally, the panel is prone to springback and warp during the process of forming, which causes the shape of the formed part to change, for example, the shape of the part is inaccurate or the part is distorted. However, such parts often bring great difficulty to subsequent processes such as assembly welding and the like, so that in the industry, when the rebound and warpage of the panel are serious, the formed parts can only be treated as waste products.
In order to reduce the rejection rate, the method is mainly started from a die at present, and the rebound warpage of the panel is optimized by adopting a rebound compensation mode. However, due to the performance differences of the panel materials, the above approach is also limited to optimize the springback warpage of the panel, and also increases the cost in the handling of the mold.
Disclosure of Invention
The embodiment of the application provides a calculation method for the rebound warpage of a panel, which can predict the rebound warpage of the panel according to panel materials, so that the selection of the panel materials is facilitated to optimize the rebound warpage of the panel, and meanwhile, the generation of other costs can be avoided.
The embodiment of the application provides the following specific technical scheme:
a method for calculating the rebound warpage of a panel adopts the following formula for calculating the rebound warpage of the panel:
wherein Warp is the rebound warpage of the panel; e is the modulus of elasticity of the panel material; sigmabIs the yield strength of the panel material; l is the maximum radial diameter of the panel.
In order to solve the same technical problem, an embodiment of the present application further provides an optimization method for springback and warpage of a panel, including the following steps:
acquiring the maximum radial diameter of a panel to be manufactured;
obtaining material parameters of a panel material, wherein the material parameters comprise an elastic modulus and a yield strength of the panel material;
calculating the resilience warping of the panel when the panel to be manufactured is manufactured by adopting the panel material according to a first panel resilience warping formula;
and (4) determining qualified panel materials.
Preferably, the step of determining a qualified panel material comprises:
calculating the difference value of the rebound warpage of the panel and the preset maximum rebound warpage;
and when the difference is smaller than the threshold value, judging the panel material to be qualified.
Preferably, the step of determining a qualified panel material comprises:
calculating the difference value of the rebound warpage of the panel and the preset maximum rebound warpage;
when the difference value is smaller than the threshold value, simulating the rebound warping of the panel corresponding to the panel material by adopting simulation software;
and when the difference value between the simulated rebound warpage of the panel and the preset maximum rebound warpage is still smaller than the threshold value, judging that the panel material is a qualified panel material.
Preferably, the following steps are further included after the determination of the qualified panel material:
obtaining the curvature radius of a panel to be manufactured, wherein the curvature radius is the curvature radius corresponding to the maximum radial length of the panel to be manufactured;
calculating the resilience warping of the panel when the panel to be manufactured is manufactured by adopting the curvature radius according to a second panel resilience warping formula, wherein the second panel resilience warping formula is as follows:
Warp＝-0·0006L2+0.000001R2-0.0002L·R-0.196L+0.125R-100
wherein Warp is the rebound warpage of the panel, L is the maximum radial length of the panel, and R is the curvature radius corresponding to the maximum radial length of the panel;
and determining the qualified radius of curvature.
Preferably, the step of determining an acceptable radius of curvature comprises:
calculating the difference value of the rebound warpage of the panel and the preset maximum rebound warpage;
and when the difference is smaller than the threshold value, judging the curvature radius as a qualified curvature radius.
Preferably, the step of determining an acceptable radius of curvature comprises:
calculating the difference value of the rebound warpage of the panel and the preset maximum rebound warpage;
when the difference is smaller than the threshold value, simulating the panel to be manufactured by adopting simulation software;
and when the difference value between the simulated rebound warpage of the panel and the preset maximum rebound warpage is still smaller than the threshold value, judging that the curvature radius is a qualified curvature radius.
Preferably, the simulation software is one of PAM-STAMP and Autoform.
Preferably, when the panel is used in a vehicle body, the threshold is 1 mm.
Preferably, when the panel is used in a household appliance, the threshold is 2 mm.
According to the first panel rebound warping formula, the rebound warping of each panel when different panel materials are adopted can be predicted before the panel is processed, so that the unqualified panel materials are eliminated, namely the rebound warping of the formed panel exceeds the range and causes panel parts to be scrapped, and therefore the panel materials are suitable to be selected before the panel is processed. Meanwhile, the first panel springback and warping formula is an empirical formula which is fitted according to experimental data of related panel materials, so that the first panel springback and warping formula has certain universality in the field of panel processing, is easy to operate and does not generate other costs.
In the method for calculating the springback warpage of the panel, provided by the embodiment, the springback warpage of each panel under different panel materials can be estimated by adopting the first panel springback warpage formula, so that the springback warpage of the panel is optimized from a material layer, and the rejection rate of the panel in a processing process is reduced.
Drawings
Fig. 1 is a flowchart of a method for optimizing springback and warpage of a panel according to a second embodiment of the present application;
fig. 2 is a flowchart of a method for optimizing springback and warpage of a panel according to a fourth embodiment of the present application.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is further described in detail below with reference to the accompanying drawings and the detailed description. It should be understood that the detailed description and specific examples, while indicating the scope of the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention.
The first embodiment is as follows:
the embodiment provides a method for calculating the rebound warpage of a panel, which adopts the following formula for calculating the rebound warpage of the panel:
wherein Warp is the rebound warpage of the panel; e is the modulus of elasticity of the panel material; sigmabIs the yield strength of the panel material; l is the maximum radial diameter of the panel. In this embodiment, the derivation of the first panel springback warping formula was performed with the maximum radial diameter as a reference, because the panel is likely to have large springback warping at the maximum radial diameter according to the actual processing data.
By adopting the first panel rebound warping formula, the rebound warping of each panel when different panel materials are adopted can be predicted before the panel is processed, so that panel materials which do not meet requirements, namely panel parts are scrapped due to the fact that the rebound warping of the formed panel exceeds the range, can be eliminated, and therefore the panel materials can be selected conveniently before the panel is processed. Meanwhile, the first panel springback and warping formula is an empirical formula which is fitted according to experimental data of related panel materials, so that the first panel springback and warping formula has certain universality in the field of panel processing and is easy to operate.
In the method for calculating the springback warpage of the panel, provided by the embodiment, the springback warpage of each panel under different panel materials can be estimated by adopting the first panel springback warpage formula, so that the springback warpage of the panel is optimized from a material layer, and the rejection rate of the panel in a processing process is reduced.
Example two:
the embodiment provides an optimization method for springback and warping of a panel, as shown in fig. 1, specifically including the following steps:
step S1: acquiring the maximum radial diameter of a panel to be manufactured;
the panel to be produced is, in the present embodiment, a part for a vehicle door, which is approximately rectangular in shape, and the maximum radial diameter of which can be considered as the diagonal length of the rectangular panel in the present embodiment. Of course, in other embodiments, the maximum radial diameter may be a non-diagonal length, taking into account the shape of the panel to be made.
Step S2: obtaining material parameters of a panel material, wherein the material parameters comprise an elastic modulus and a yield strength of the panel material;
the modulus of elasticity and yield strength of the panel material are used as variables of the first panel rebound warping formula, which is directly related to the panel material, so that the related material parameters of the panel material can be directly obtained from the existing data in the step for facilitating the subsequent steps.
Step S3: calculating the resilience warping of the panel when the panel to be manufactured is manufactured by adopting the panel material according to a first panel resilience warping formula;
in the step, the elastic modulus and the yield strength of the panel material and the maximum radial diameter of the panel to be manufactured are only required to be brought into the rebound warpage of the first panel for calculation.
Step S4: determining qualified panel materials;
in this embodiment, this step may be performed by performing a threshold comparison to determine acceptable panel material, although other methods may be used in other embodiments. Specifically, the difference between the rebound warpage of the panel and the preset maximum rebound warpage can be calculated, then the difference is compared with a threshold, and when the difference is smaller than the threshold, the panel material can be determined to be a qualified panel material.
The preset maximum rebound warpage can be the maximum rebound warpage of the panel after processing only after the rejection according to experience or related standards. The threshold value, which may be defined specifically according to industry standards as follows, is 1mm when the panel is used in a vehicle body. And when the panel is used for household appliances, the threshold value is 2 mm.
Example three:
the difference between this embodiment and the second embodiment lies in the step of determining the qualified panel material. Specifically, in the embodiment, when a qualified panel material is determined, a difference between the rebound warpage of the panel and a preset maximum rebound warpage is calculated, then the difference is compared with a threshold, and when the difference is smaller than the threshold, the panel material is preliminarily determined to meet the requirement. However, the panel material needs to be further verified, and therefore, simulation software needs to be used to simulate the springback warpage of the panel corresponding to the panel material, specifically, existing simulation software, such as PAM-STAMP or auto, is used to simulate the springback warpage of the panel material after the panel to be manufactured is manufactured, and when the difference between the simulated springback warpage of the panel and the preset maximum springback warpage is still smaller than the threshold value, the panel material can be determined to be a qualified panel material.
In the embodiment, the selected panel material can be further ensured to meet the requirement by combining a formula with two steps of simulation in the process of determining the qualified panel material, so that the rejection rate in the subsequent actual processing process is further reduced, and the aim of optimization is fulfilled.
Example four:
the difference between this embodiment and the second embodiment is that the following steps are added after the determination of qualified panel material in this embodiment, see fig. 2:
step S5: obtaining the curvature radius of a panel to be manufactured, wherein the curvature radius is the curvature radius corresponding to the maximum radial length of the panel to be manufactured;
in this embodiment, the shape of the panel to be manufactured is similar to that of the panel to be manufactured in the second embodiment, and thus the curvature radius corresponding to the maximum radial length of the panel also refers to the diagonal curvature radius of the panel.
Step S6: calculating the resilience warping of the panel when the panel to be manufactured is manufactured by adopting the curvature radius according to a second panel resilience warping formula, wherein the second panel resilience warping formula is as follows:
Warp＝-0.0006L2+0.000001R2-0.0002L·R-0.196L+0.125R-100
wherein Warp is the rebound warpage of the panel, L is the maximum radial length of the panel, and R is the curvature radius corresponding to the maximum radial length of the panel;
in order to adapt to different vehicle bodies or boxes or improve the aesthetic property, part of the panel needs to be processed into a certain radian, namely, a certain curvature radius, and the rebound warpage of the panel to be manufactured with the certain curvature radius can be estimated through a second panel rebound warpage formula in the step.
Step S7: determining a qualified radius of curvature;
in this embodiment, this step may determine the qualified radius of curvature by performing a threshold comparison, although other methods may be used in other embodiments. Specifically, the difference between the rebound warpage of the panel and the preset maximum rebound warpage may be calculated, and then the difference is compared with a threshold, and when the difference is smaller than the threshold, the curvature radius may be determined to be a qualified curvature radius.
Example five:
the difference between this embodiment and the fourth embodiment lies in the step of determining the acceptable radius of curvature. Specifically, in the embodiment, when the qualified radius of curvature is determined, the difference between the rebound warpage of the panel and the preset maximum rebound warpage is calculated, then the difference is compared with the threshold, and when the difference is smaller than the threshold, the radius of curvature is preliminarily determined to meet the requirement. However, the curvature radius needs to be further verified, so that simulation software needs to be used to simulate the springback warpage of the panel corresponding to the curvature radius, specifically, existing simulation software, such as PAM-STAMP or auto, is used to simulate the springback warpage of the panel after the panel to be manufactured is manufactured under the curvature radius, and when the difference between the simulated springback warpage of the panel and the preset maximum springback warpage is still smaller than the threshold value, the curvature radius can be determined as the qualified curvature radius.
In the embodiment, the selected qualified radius of curvature can be further ensured to meet the requirement by combining a formula with two steps of simulation in the process of determining the qualified radius of curvature, so that the rejection rate in the subsequent actual processing process is further reduced, and the aim of optimization is fulfilled.
It is understood that, in the above embodiments, when the difference is greater than or equal to the threshold value in the process of comparing the threshold values, the panel material or the curvature radius is not satisfactory, and thus, the above steps can be repeated by changing the corresponding values until the qualified panel material or the qualified curvature radius is selected.
The above-mentioned embodiments only express several embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the inventive concept, which falls within the scope of the present invention. Therefore, the protection scope of the present patent shall be subject to the appended claims.
Claims (10)
1. A method for calculating the rebound warpage of a panel is characterized by adopting the following first panel rebound warpage formula to calculate:
wherein Warp is the rebound warpage of the panel; e is the modulus of elasticity of the panel material; sigmabIs the yield strength of the panel material; l is the maximum radial diameter of the panel.
2. A method for optimizing the rebound warpage of a panel is characterized by comprising the following steps:
acquiring the maximum radial diameter of a panel to be manufactured;
obtaining material parameters of a panel material, wherein the material parameters comprise an elastic modulus and a yield strength of the panel material;
calculating the resilience warping of the panel when the panel to be manufactured is manufactured by adopting the panel material according to a first panel resilience warping formula;
and (4) determining qualified panel materials.
3. A method of optimizing the resilient warping of a panel as claimed in claim 2, wherein said step of determining acceptable panel material comprises:
calculating the difference value of the rebound warpage of the panel and the preset maximum rebound warpage;
and when the difference is smaller than the threshold value, judging the panel material to be qualified.
4. A method of optimizing the resilient warping of a panel as claimed in claim 2, wherein said step of determining acceptable panel material comprises:
calculating the difference value of the rebound warpage of the panel and the preset maximum rebound warpage;
when the difference value is smaller than the threshold value, simulating the rebound warpage of the panel corresponding to the panel material by adopting simulation software;
and when the difference value between the simulated rebound warpage of the panel and the preset maximum rebound warpage is still smaller than the threshold value, judging that the panel material is a qualified panel material.
5. A method of optimising the springback warpage of a panel as claimed in any one of claims 2 to 4, further including the steps, after the determination of acceptable panel material, of:
obtaining the curvature radius of a panel to be manufactured, wherein the curvature radius is the curvature radius corresponding to the maximum radial length of the panel to be manufactured;
calculating the resilience warping of the panel when the panel to be manufactured is manufactured by adopting the curvature radius according to a second panel resilience warping formula, wherein the second panel resilience warping formula is as follows:
Warp＝-0.0006L2+0.000001R2-0.0002L·R-0.196L+0.125R-100
wherein Warp is the rebound warpage of the panel, L is the maximum radial length of the panel, and R is the curvature radius corresponding to the maximum radial length of the panel;
and determining the qualified radius of curvature.
6. The method of optimizing panel spring back warp of claim 5, wherein said step of determining an acceptable radius of curvature comprises:
calculating the difference value of the rebound warpage of the panel and the preset maximum rebound warpage;
and when the difference is smaller than the threshold value, judging the curvature radius as a qualified curvature radius.
7. The method of optimizing panel spring back warp of claim 5, wherein said step of determining an acceptable radius of curvature comprises:
calculating the difference value of the rebound warpage of the panel and the preset maximum rebound warpage;
when the difference is smaller than the threshold value, simulating the panel to be manufactured by adopting simulation software;
and when the difference value between the simulated rebound warpage of the panel and the preset maximum rebound warpage is smaller than the threshold value, judging the curvature radius as a qualified curvature radius.
8. The method for optimizing springback warpage of a panel according to claim 4 or 7, wherein the simulation software is one of PAM-STAMP and auto.
9. A method of optimising the springback warpage of a panel as claimed in any one of claims 2 to 7, wherein the threshold value is 1mm when the panel is used in a vehicle body.
10. The method for optimizing the rebound warpage of a panel as set forth in any one of claims 2 to 7, wherein the threshold value is 2mm when the panel is used in an electric appliance.
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006339423A (en) * | 2005-06-02 | 2006-12-14 | Nec Corp | Board warping analyzing method, its system, its program, and record medium |
| CN103237418A (en) * | 2013-05-15 | 2013-08-07 | 广州兴森快捷电路科技有限公司 | Judging method for warping of PCB (Printed Circuit Board) |
| CN105488263A (en) * | 2015-11-24 | 2016-04-13 | 广州兴森快捷电路科技有限公司 | Method for predicting warpage of package substrate subjected to resistance welding |
| CN106903166A (en) * | 2017-03-21 | 2017-06-30 | 北京科技大学 | A kind of aluminum alloy plate materials asymmetrical rolling warpage forecast and the method for optimization |
-
2019
- 2019-03-22 CN CN201910220390.6A patent/CN111737828A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006339423A (en) * | 2005-06-02 | 2006-12-14 | Nec Corp | Board warping analyzing method, its system, its program, and record medium |
| CN103237418A (en) * | 2013-05-15 | 2013-08-07 | 广州兴森快捷电路科技有限公司 | Judging method for warping of PCB (Printed Circuit Board) |
| CN105488263A (en) * | 2015-11-24 | 2016-04-13 | 广州兴森快捷电路科技有限公司 | Method for predicting warpage of package substrate subjected to resistance welding |
| CN106903166A (en) * | 2017-03-21 | 2017-06-30 | 北京科技大学 | A kind of aluminum alloy plate materials asymmetrical rolling warpage forecast and the method for optimization |
Non-Patent Citations (5)
| Title |
|---|
| 刘京雷,谢仕强,阮锋: "弯曲回弹逆解公式及其在焊管预弯机组设计中的应用", 锻压技术, no. 02 * |
| 刘月云;刘碧俊;: "基于DOE、RSM及PSO的大尺寸板类塑件的翘曲优化", 中国塑料, no. 10 * |
| 尹红灵;: "基于CAE技术的汽车前面板注塑成型工艺优化", 模具技术, no. 02 * |
| 白振华;李龙华;李铭泽;高明磊;王瑞;李和;: "热轧带钢卷取后翘曲计算模型研究", 燕山大学学报, no. 03 * |
| 赵小月 等: "某冰箱门体端部翘曲的有限元分析及改进设计", 机械研究与应用, no. 05, pages 2 - 4 * |
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