Granted Patent B2

US 12,229,476 · App. 17/236,917 · Granted Feb 18, 2025

Inventors: Ravi Kumar Burla (Novi, MI); Jesus Rodriguez (Farmington, MI); Siavash Navadeh Meshkat (Carlsbad, CA); Jaesung Eom (Wexford, PA)

Assignee: Autodesk, Inc.

G06F30/12G06F17/16G06F30/10G06F30/20G06N3/0475

Abstract

Claims (72)

1. A method comprising:

obtaining one or more design criteria and a three dimensional model of an object for which a corresponding physical structure is to be manufactured, wherein the three dimensional model is a computer-implemented model having a design space in which the physical structure is to be designed;

selecting non-rigid body eigenmodes of a finite element stiffness matrix from a modal analysis of the three dimensional model of the object, wherein the non-rigid body eigenmodes that are selected are less than ten in number;

superposing strain energy density fields extracted from the non-rigid body eigenmodes to form a synthetic strain energy field for the three dimensional model of the object using weighted strain energies from the strain energy density fields;

iteratively modifying a shape of the three dimensional model of the object using the synthetic strain energy field to drive changes to the shape of the three dimensional model, wherein the iteratively modifying comprises

calculating a shape change velocity field for the shape of the three dimensional model of the object using the synthetic strain energy field, and

updating computer-implemented geometry of the shape within the design space using the shape change velocity field, wherein the geometry of the shape comprises computer representation of individual shape elements; and

providing the shape of the three dimensional model of the object, which is useable in manufacturing the physical structure using one or more computer-controlled manufacturing systems.

2. The method of claim 1 , wherein the selecting comprises selecting a number of the non-rigid body eigenmodes based on computer processing speed and a desired upper limit to processing time for the iteratively modifying.

3. The method of claim 2 , comprising receiving input from a user specifying the desired upper limit to processing time for the iteratively modifying.

4. The method of claim 1 , wherein the selecting comprises:

obtaining one or more frequencies of vibration for which structural performance of the physical structure is to be enhanced; and

extracting the strain energy density fields from the non-rigid body eigenmodes that correspond to the one or more frequencies of vibration.

5. The method of claim 4 , wherein obtaining one or more frequencies of vibration comprises receiving user specification of a specified frequency or a range of frequencies for which structural performance of the physical structure is to be enhanced, and the selecting comprises identifying the non-rigid body eigenmodes that correspond to the one or more frequencies of vibration as those eigenmodes with resonate frequencies that fall within the range of frequencies or that are within a tolerance band around the specified frequency.

6. The method of claim 1 , wherein the iteratively modifying comprises:

checking for completion of a percentage reduction in volume for the shape that is less than a target volume reduction of an original volume of the three dimensional model of the object; and

re-computing the synthetic strain energy field in response to the completion of the percentage reduction in volume for the shape that is less than the target volume reduction of the original volume, the re-computing comprising:

performing an updated modal analysis on a modified version of the shape of the three dimensional model of the object after the completion of the percentage reduction in volume for the shape that is less than the target volume reduction of the original volume;

selecting updated non-rigid body eigenmodes of an updated finite element stiffness matrix from the updated modal analysis; and

superposing updated strain energy density fields extracted from the updated non-rigid body eigenmodes selected from the updated modal analysis to update the synthetic strain energy field used in the iteratively modifying after the completion of the percentage reduction in volume for the shape that is less than the target volume reduction of the original volume.

7. The method of claim 1 , wherein the one or more design criteria comprise a manufacturing constraint, and the iteratively modifying comprises:

checking whether the manufacturing constraint is violated in a given iteration of the iteratively modifying; and

re-computing the synthetic strain energy field in response to the manufacturing constraint being violated in the given iteration, the re-computing comprising:

performing an updated modal analysis on a modified version of the shape of the three dimensional model of the object after the manufacturing constraint is violated in the given iteration;

selecting updated non-rigid body eigenmodes of an updated finite element stiffness matrix from the updated modal analysis; and

superposing updated strain energy density fields extracted from the updated non-rigid body eigenmodes selected from the updated modal analysis to update the synthetic strain energy field used in the iteratively modifying after the given iteration.

8. The method of claim 1 , wherein the calculating, in at least one iteration of the iteratively modifying, comprises:

performing numerical simulation based on a boundary condition specification for the three dimensional model of the object to form a strain energy field for the three dimensional model of the object; and

modifying the strain energy field formed by the numerical simulation using the synthetic strain energy field or modifying the synthetic strain energy field using the strain energy field formed by the numerical simulation.

9. The method of claim 1 , wherein the iteratively modifying is performed without any input regarding boundary conditions for the three dimensional model of the object, and the method comprises providing a user interface that provides user control over weighting of the strain energies from the strain energy density fields to favor some eigenmodes over other eigenmodes.

10. The method of claim 1 , wherein the providing comprises:

generating toolpath specifications for a manufacturing machine using the shape of the three dimensional model of the object; and

manufacturing at least a portion of the physical structure, or a mold for the physical structure, with the manufacturing machine using the toolpath specifications.

11. A system comprising:

a non-transitory storage medium having instructions of a computer aided design program stored thereon; and

one or more data processing apparatus configured to run the instructions of the computer aided design program to cause the one or more data processing apparatus to

obtain one or more design criteria and a three dimensional model of an object for which a corresponding physical structure is to be manufactured, wherein the three dimensional model is a computer-implemented model having a design space in which the physical structure is to be designed;

select non-rigid body eigenmodes of a finite element stiffness matrix from a modal analysis of the three dimensional model of the object, wherein the non-rigid body eigenmodes that are selected are less than ten in number;

superpose strain energy density fields extracted from the non-rigid body eigenmodes to form a synthetic strain energy field for the three dimensional model of the object using weighted strain energies from the strain energy density fields;

iteratively modify a shape of the three dimensional model of the object using the synthetic strain energy field to drive changes to the shape of the three dimensional model, wherein the iterative modification comprises

calculating a shape change velocity field for the shape of the three dimensional model of the object using the synthetic strain energy field, and

updating computer-implemented geometry of the shape within the design space using the shape change velocity field, wherein the geometry of the shape comprises computer representation of individual shape elements; and

provide the shape of the three dimensional model of the object, which is useable in manufacturing the physical structure using one or more computer-controlled manufacturing systems.

12. The system of claim 11 , wherein the one or more data processing apparatus are configured to run the instructions of the computer aided design program to cause the one or more data processing apparatus to select a number of the non-rigid body eigenmodes based on computer processing speed and a desired upper limit to processing time for the iterative modification.

13. The system of claim 12 , wherein the one or more data processing apparatus are configured to run the instructions of the computer aided design program to cause the one or more data processing apparatus to receive input from a user specifying the desired upper limit to processing time for the iterative modification.

14. The system of claim 11 , wherein the one or more data processing apparatus are configured to run the instructions of the computer aided design program to cause the one or more data processing apparatus to:

obtain one or more frequencies of vibration for which structural performance of the physical structure is to be enhanced; and

extract the strain energy density fields from the non-rigid body eigenmodes that correspond to the one or more frequencies of vibration.

15. The system of claim 14 , wherein the one or more data processing apparatus are configured to run the instructions of the computer aided design program to cause the one or more data processing apparatus to iteratively modify the shape of the three dimensional model of the object by being configured to:

receive user specification of a specified frequency or a range of frequencies for which structural performance of the physical structure is to be enhanced; and

identify the non-rigid body eigenmodes that correspond to the one or more frequencies of vibration as those eigenmodes with resonate frequencies that fall within the range of frequencies or that are within a tolerance band around the specified frequency.

16. The system of claim 11 , wherein the one or more data processing apparatus are configured to run the instructions of the computer aided design program to cause the one or more data processing apparatus to iteratively modify the shape of the three dimensional model of the object by being configured to:

check for completion of a percentage reduction in volume for the shape that is less than a target volume reduction of an original volume of the three dimensional model of the object; and

re-compute the synthetic strain energy field in response to the completion of the percentage reduction in volume for the shape that is less than the target volume reduction of the original volume by being configured to:

perform an updated modal analysis on a modified version of the shape of the three dimensional model of the object after the completion of the percentage reduction in volume for the shape that is less than the target volume reduction of the original volume;

select updated non-rigid body eigenmodes of an updated finite element stiffness matrix from the updated modal analysis; and

superpose updated strain energy density fields extracted from the updated non-rigid body eigenmodes selected from the updated modal analysis to update the synthetic strain energy field used in the iterative modification after the completion of the percentage reduction in volume for the shape that is less than the target volume reduction of the original volume.

17. The system of claim 11 , wherein the one or more design criteria comprise a manufacturing constraint, and the one or more data processing apparatus are configured to run the instructions of the computer aided design program to cause the one or more data processing apparatus to:

check whether the manufacturing constraint is violated in a given iteration of the iterative modification; and

re-compute the synthetic strain energy field in response to the manufacturing constraint being violated in the given iteration by performing operations comprising:

performing an updated modal analysis on a modified version of the shape of the three dimensional model of the object after the manufacturing constraint is violated in the given iteration;

selecting updated non-rigid body eigenmodes of an updated finite element stiffness matrix from the updated modal analysis; and

superposing updated strain energy density fields extracted from the updated non-rigid body eigenmodes selected from the updated modal analysis to update the synthetic strain energy field used in the iterative modification after the given iteration.

18. The system of claim 11 , wherein the one or more data processing apparatus are configured to run the instructions of the computer aided design program to:

perform numerical simulation based on a boundary condition specification for the three dimensional model of the object to form a strain energy field for the three dimensional model of the object; and

modify the strain energy field formed by the numerical simulation using the synthetic strain energy field or modify the synthetic strain energy field using the strain energy field formed by the numerical simulation.

19. The system of claim 11 , wherein the one or more data processing apparatus are configured to run the instructions of the computer aided design program to cause the one or more data processing apparatus to:

iteratively modify the shape of the three dimensional model of the object without any input regarding boundary conditions for the three dimensional model of the object; and

provide a user interface that provides user control over weighting of the strain energies from the strain energy density fields to favor some eigenmodes over other eigenmodes.

20. The system of claim 11 , wherein the one or more data processing apparatus are configured to run the instructions of the computer aided design program to cause the one or more data processing apparatus to:

generate toolpath specifications for a manufacturing machine using the shape of the three dimensional model of the object; and

manufacture at least a portion of the physical structure, or a mold for the physical structure, with the manufacturing machine using the toolpath specifications.

Assignments (2)

Continuity (1)

References Cited (68)