Method of identifying critical elements in fatigue analysis with von mises stress bounding and filtering modal displacement history using dynamic windowing

• US 6,212,486 B1
• Filed: 09/17/1998
• Issued: 04/03/2001
• Est. Priority Date: 09/17/1998
• Status: Expired due to Fees

• Current Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Original Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Inventors: Huang, Liping, Agrawal, Hari
• Primary Examiner(s): Teska, Kevin J.
• Assistant Examiner(s): THOMSON, WILLIAM D
• Application Number:
  US09/156,195
• Time in Patent Office: 929 Days
• Field of Search: 703/2, 703/6, 703/7, 703/8, 703/1
• US Class Current: 703/7
• CPC Class Codes: G06F 30/15 Vehicle, aircraft or watercraft design
• CPC Class Codes: G06F 30/23 using finite element methods [FEM] or finite difference methods [FDM]

Abstract

A method of dynamic durability analysis and fatigue area identification using modal techniques for a structure includes the steps of simulating a finite element model of the structure to determine modal stresses and modal displacements for an element of the structure and performing a modal transient analysis using the modal displacements. The method also includes the steps of determining a stress bound for the element from the modal stresses and modal transient analysis, determining if a stress bound for the element is greater than a predetermined value and identifying the element as a critical element if the stress bound for the element is greater than the predetermined value. The method further includes the steps of determining a stress time history for the critical element and using the stress time history to perform a fatigue analysis to identify an area of fatigue within the structure.

Claims

1. A computer implemented method of dynamic durability analysis and fatigue area identification for a structure comprising:

simulating a finite element model of a structure to determine modal stresses and modal displacements for an element of the structure;

performing a modal transient analysis using the modal displacements;

determining a stress bound for the element from the modal stresses and modal transient analysis, wherein the stress bound is determined by finding an upper bound and a lower bound of a normal stress and a shear stress for the element, determining a Von Mises stress from the upper bound and the lower bound of the normal stress and the shear stress for the element and selecting the upper bound of the Von Mises stress as the stress bound;

determining if the stress bound for the element is greater than a predetermined value, wherein the stress bound is the upper bound of a Von Mises stress;

identifying the element as a critical element if the stress bound for the element is greater than the predetermined value;

determining a stress time history for the critical element;

using the stress time history to perform a fatigue analysis to identify an area of fatigue within the structure; and

filtering the modal displacement time history using a dynamic window, prior to said step of determining a stress time history.

2. A computer implemented method of dynamic durability analysis and fatigue area identification for a structure comprising:

simulating a finite element model of a structure to determine modal stresses and modal displacements for an element of the structure;

performing a modal transient analysis using the modal displacements;

determining a stress bound for the element from the modal stresses and modal transient analysis;

determining if the stress bound for the element is greater than a predetermined value, wherein the stress bound is the upper bound of a Von Mises stress;

identifying the element as a critical element if the stress bound for the element is greater than the predetermined value;

determining a stress time history for the critical element;

using the stress time history to perform a fatigue analysis to identify an area of fatigue within the structure; and

filtering the modal displacement time history using a dynamic window, prior to said step of determining a stress time history.

3. A method as set forth in claim 2 wherein the dynamic window is a maximum modal displacement less a minimum modal displacement multiplied by a predetermined percentage.

4. A computer implemented method of dynamic durability analysis and fatigue area identification for a structure comprising:

simulating a finite element model of a structure;

determining a modal stress for each element of the finite element model;

determining a modal displacement time history for each element of the finite element model;

determining a minimum modal displacement value and a maximum modal displacement value for each mode from the modal displacement time history;

determining an upper bound and lower bound of a normal stress and a shear stress for each element;

determining a stress bound for each element from the upper bound and the lower bound of the normal stress and the shear stress;

determining if the stress bound for each element is less than a predetermined value, wherein the stress bound is the upper bound of a Von Mises stress;

identifying the element as a non-critical element if the stress bound is less than the predetermined value;

identifying the element as a critical element if the stress bound is greater than the predetermined value;

determining a dynamic stress time history of the critical element;

using the dynamic stress time history to perform a fatigue analysis on the critical element to identify an area of fatigue within the structure; and

filtering the modal displacement time history using a dynamic window, prior to said step of determining a dynamic stress time history.

5. A method as set forth in claim 4 wherein the dynamic window is a maximum modal displacement less a minimum modal displacement multiplied by a predetermined percentage.

6. A method as set forth in claim 5 wherein the modal displacement time history is determined by a modal transient analysis.

7. A computer implemented method of dynamic durability analysis and fatigue area identification for a structure, said method comprising the steps of:

simulating a finite element model of a structure;

determining a modal stress for each element of the finite element model;

determining a modal displacement time history for each element of the finite element model by a modal transient analysis;

determining a minimum modal displacement value and a maximum modal displacement value for each mode from the modal displacement time history;

determining an upper bound and lower bound of a normal stress and a shear stress for each element;

determining a stress bound for each element from the upper bound and the lower bound of the normal stress and the shear stress;

determining if the stress bound for each element is less than a predetermined material value;

identifying the element as a non-critical element if the stress bound is less than the predetermined value;

identifying the element as a critical element if the stress bound is greater than the predetermined value;

filtering the modal displacement time history using a dynamic window, wherein the dynamic window is a maximum modal displacement less a minimum modal displacement multiplied by a predetermined percentage;

determining a dynamic stress time history of the critical element; and

using the dynamic stress time history to perform a fatigue analysis on the critical element to identify an area of fatigue within the structure; and

wherein the stress bound is the upper bound of a Von Mises stress.

8. A method as set forth in claim 7 wherein the dynamic stress time history is determined from a normal stress and a shear stress for the critical element at a filtered modal displacement.

9. A computer implemented method of dynamic durability analysis and fatigue area identification for a vehicle comprising:

simulating a finite element model of a structure for a vehicle;

determining a modal stress for each element of the finite element model;

determining a modal displacement time history for each mode of the finite element model;

determining a minimum modal displacement value and a maximum modal displacement value for each mode from the modal displacement time history;

determining an upper bound and lower bound of a normal stress and a shear stress for each element;

determining a stress bound for each element, wherein the stress bound is a Von Mises stress determined from the upper bound and the lower bound of the normal stress and the shear stress;

determining if the stress bound for each element is less than a predetermined material yield strength;

identifying the element as a non-critical element if the stress bound is less than said predetermined yield strength;

identifying the element as a critical element if the stress bound is greater than said predetermined yield strengths;

filtering the modal displacement time history using a dynamic window;

determining a dynamic stress time history of the critical element; and

using the dynamic stress time history to perform a fatigue analysis on the critical element to identify an area of fatigue within the structure.

10. A method as set forth in claim 9 wherein the dynamic window is a maximum modal displacement less a minimum modal displacement multiplied by a predetermined percentage.

11. A method as set forth in claim 10 wherein the modal displacement time history is determined by a modal transient analysis.

12. A method as set forth in claim 11 wherein the dynamic stress time history is determined from a normal stress and a shear stress for the critical element at a filtered modal displacement.