Method and procedure for evaluation and compensation of springback

Patent metadata

Field	Value
Publication number	US-2023028435-A1
Application number	US-202117380464-A
Country	US
Kind code	A1
Filing date	Jul 20, 2021
Priority date	Jul 20, 2021
Publication date	Jan 26, 2023
Grant date	—

Abstract

A method for compensating springback of a part includes running a finite element analysis (FEA) simulation of forming a panel using a model of forming die such that a panel with springback is simulated, determining at least two zero springback locations on the panel where hanging apertures are simulated, running an FEA simulation of the panel hanging from the hanging apertures, and comparing a geometry of the hanging panel to a geometry of a reference panel such that a difference between the geometry of the hanging panel and the geometry of the reference panel due to the springback is determined and compensated.

First claim

What is claimed is:

1 . A method for compensating springback of a part, the method comprising:
a) running a finite element analysis (FEA) simulation of forming a panel using a model of an Alpha(i) forming die such that an Alpha(i) panel with springback is simulated, wherein i=1; b) determining at least two locations on the Alpha(i) panel where springback displacement is about 0.0 mm and simulating an aperture at each of the at least two locations, wherein the simulated apertures in the Alpha(i) panel comprise hanging apertures; c) running an FEA simulation of the Alpha(i) panel hanging from the hanging apertures in an installed orientation and in a stress-free state except for an effect of gravity; d) comparing a geometry of the hanging Alpha(i) panel to a geometry of a reference panel and determining a difference between the geometry of the hanging Alpha(i) panel and the geometry of the reference panel due to the springback; e) incrementing i to equal i+1; f) generating the Alpha(i) forming die model with at least one morphed die surface as a function of the difference between the geometry of the hanging Alpha(i−1) panel and the geometry of the reference panel due to the springback; g) running an FEA simulation of forming the panel with the hanging apertures using the Alpha(i) forming die model such that the Alpha(i) panel with springback and at least one morphed surface is simulated; and h) repeating steps c) through g) until the difference between the geometry of the hanging Alpha(i) panel and the geometry of the reference panel due to the springback is less than a predefined delta value.

2 . The method according to claim 1 , wherein the springback displacement of the least two hanging apertures in the Alpha(i) panel comprise about 0.0 mm springback in a length direction and in a width direction of the Alpha(i) panel.

3 . The method according to claim 1 , wherein the Alpha(i) panel comprises a Class A surface and a non-Class A surface.

4 . The method according to claim 3 , wherein the at least two hanging apertures extend through the Class A surface of the Alpha(i) panel.

5 . The method of according to claim 4 , wherein step c) comprises running the FEA simulation of the Alpha(i) panel hanging from the apertures hanging in the installed orientation and in the stress-free stated except for the effect of gravity, wherein the Alpha(i) panel has a morphed non-Class A surface compared to the Alpha(i−1) panel.

6 . The method according to claim 5 , wherein step d) comprises comparing the Class A surface geometry of the hanging Alpha(i) panel to a Class A surface geometry of the reference panel and determining a difference between the Class A surface geometry of the hanging Alpha(i) panel and the Class A surface geometry of the reference panel.

7 . The method according to claim 6 , wherein step f) comprises generating the Alpha(i) forming die model with springback consideration of the Class A surface as a function of the difference between the Class A surface geometry of the hanging Alpha(i) panel geometry and the Class A surface geometry of the reference panel.

8 . The method according to claim 7 , wherein step h) comprises repeating steps c) through g) with springback consideration of the Class A surface until the difference between the Class A surface geometry of the hanging Alpha(i) panel and the Class A surface geometry of the reference panel due to the springback is less than the predefined delta value.

9 . The method according to claim 8 further comprising:
j) running an FEA simulation of the Alpha(i) panel hanging in the installed orientation and in the stress-free stated except for the effect of gravity, wherein the Alpha(i) panel is simulated hanging from the hanging apertures or from at least one hanging pin attached to the non-Class A surface;
k) comparing the non-Class A surface geometry of the hanging Alpha(i) panel to a non-Class A surface geometry of the reference panel and determining a difference between the non-Class A surface geometry of the hanging Alpha(i) panel and the non-Class A surface geometry of the reference panel;
l) incrementing i to equal i+1;
m) generating the Alpha(i) forming die with springback consideration of the non-Class A surface as a function of the difference between the non-Class A surface geometry of the hanging Alpha(i) panel and the non-Class A surface geometry of the reference panel;
n) running an FEA simulation of forming an Alpha(i) panel with the hanging apertures using the Alpha(i) forming die model and with springback consideration of the non-Class A surface; and
o) repeating steps j) through n) until the difference between the non-Class A surface of the hanging Alpha(i) panel geometry and the non-Class A surface geometry of the reference panel due to the springback is less than a predefined epsilon value.

10 . The method according to claim 1 , wherein the panel is a fender panel of a vehicle, the fender panel comprising a Class A surface, a catwalk surface, a doorline surface, and a wheel opening surface.

11 . The method according to claim 10 , wherein the steps a) through h) comprise:
a) running an FEA simulation of forming the fender panel using the Alpha(i) forming die model where i=1 such that an Alpha(i) fender panel is simulated; b) determining the at least two locations on the Class A Surface of the Alpha(i) fender panel where the springback displacement is about 0.0 mm and simulating the aperture at each of the at least two locations, wherein the simulated apertures in the Alpha(i) fender panel comprise the hanging apertures; c) running an FEA simulation of the Alpha(i) fender panel hanging from the hanging apertures in the installed orientation and in the stress-free stated except for the effect of gravity; d) comparing the Class A surface geometry of the hanging Alpha(i) fender panel to a Class A surface geometry of the reference panel and determining a difference between the Class A surface geometry of the hanging Alpha(i) fender panel and the Class A surface geometry of the reference panel due to the springback; e) incrementing i to equal i+1; f) generating the Alpha(i) forming die model with springback consideration of the Class A surface as a function of the difference between the Class A surface geometry of the hanging Alpha(i−1) fender panel and the Class A surface geometry of the reference panel due to the springback; g) running an FEA simulation of forming the panel with the hanging apertures using the Alpha(i) forming die model and with springback consideration of the Class A surface; and h) repeating steps c) through g) until the difference between the Class A surface geometry of the hanging Alpha(i) fender panel and the Class A surface geometry of the reference panel due to the springback is less than the predefined delta value.

12 . The method according to claim 11 further comprising:
j) running the FEA simulation of the catwalk surface of the Alpha(i) fender panel hanging from the hanging apertures in the installed orientation and in the stress-free stated except for the effect of gravity;
k) comparing a catwalk surface geometry of the hanging Alpha(i) fender panel to a catwalk surface geometry of the reference panel and determining a difference between the catwalk surface geometry of the hanging Alpha(i) fender panel geometry and the catwalk surface geometry of the reference panel;
I) incrementing i to equal i+1;
m) generating the Alpha(i) forming die model with springback consideration of the catwalk surface as a function of the difference between the catwalk surface geometry of the hanging Alpha(i) fender panel and the catwalk surface geometry of the refere

Assignees

• Ford Motor Co

Inventors

• Liasi Evangelos
• Huang Liang
• Degenhardt Robert Vaughn
• Genereux Christian Richard
• Muirhead Ryan

Classifications

• G06F30/23 Primary

  using finite element methods [FEM] or finite difference methods [FDM] · CPC title

• G06F30/15 Primary

  Vehicle, aircraft or watercraft design · CPC title

• G06F2119/14

  Force analysis or force optimisation, e.g. static or dynamic forces · CPC title

• G06F2113/24

  Sheet material · CPC title