METHOD AND SYSTEM FOR AUTOMATED DESIGN GENERATION WITH INERTIAL CONSTRAINTS
A modification of a topology optimization formulation for part-level generation is provided such that it includes additional constraints that ensure that the inertial quantities (e.g., COM, Mol, and mass) of an automatically generated part are equivalent to specified targets. These targets are the inertial values used in an initial assembly-level simulation. The reaction and external forces acting on the part of interest resulting from assembly-level simulation provide the boundary conditions used for part-level generation. By constraining the inertial properties in this way, there is no need to evaluate the assembly-level dynamics each time a part is generated.
1 . A method for automated design generation, the method comprising:
receiving design domain and boundary conditions for at least one part of an assembly to be generated;
evaluating an objective and constraints;
computing decision variables based on the objective and the constraints;
augmenting or filtering the decision variables based on at least a plurality of inertial considerations;
determining or updating design variables based on decision variables;
generating a design for the at least one part; and
outputting information configured to realize or manufacture the at least one part.
2 . The method as set forth in claim 1 , wherein the evaluating comprises performing a finite element analysis.
3 . The method as set forth in claim 1 , wherein the decision variables comprise gradients and sensitivity fields.
4 . The method as set forth in claim 1 , wherein the plurality of inertial considerations comprises mass, moment of inertia, and center of mass.
5 . The method as set forth in claim 1 , wherein the augmenting or filtering is also based on design or manufacturing considerations.
6 . The method as set forth in claim 1 , wherein the outputting information configured to realize or manufacture comprises outputting information configured for at least one of: three-dimensional printing, additive manufacturing, subtractive manufacturing, or hybrid manufacturing.
7 . The method as set forth in claim 1 , further comprising outputting information for further simulation or analysis before realization or manufacturing.
8 . A system for automated design generation, the system comprising:
at least one processor and at least one memory having instructions stored thereon wherein execution of the instructions by the processor causes the system to:
receive design domain and boundary conditions for at least one part of an assembly to be generated;
evaluate an objective and constraints;
compute decision variables based on the objective and the constraints;
augment or filter the decision variables based on at least a plurality of inertial considerations;
determine or update design variables based on decision variables;
generate a design for the at least one part; and
output information configured to realize or manufacture the at least one part.
9 . The system as set forth in claim 8 , wherein the evaluating comprises performing a finite element analysis.
10 . The system as set forth in claim 8 , wherein the decision variables comprise gradients and sensitivity fields.
11 . The system as set forth in claim 8 , wherein the plurality of inertial considerations comprises mass, moment of inertia, and center of mass.
12 . The system as set forth in claim 8 , wherein the augmenting or filtering is also based on design or manufacturing considerations.
13 . The system as set forth in claim 8 , wherein the information output to realize or manufacture comprises at least one of information configured for: three-dimensional printing, additive manufacturing, subtractive manufacturing, or hybrid manufacturing.
14 . The system as set forth in claim 8 , further comprising a realization or manufacturing system.
15 . The system as set forth in claim 14 , wherein the realization or manufacturing system comprises at least one of: a three-dimensional printing system, an additive manufacturing system, a subtractive manufacturing system, or a hybrid manufacturing system.
16 . The system as set forth in claim 8 , wherein the system is further caused to perform further analysis or simulation before information is output to realize or manufacture the part.