Numerical simulation of progressive lancing operation in sheet metal forming

A system for conducting a time-marching simulation of manufacturing a sheet metal part that requires progressive lancing operation, the system comprises:

• an input/output (I/O) interface;
• a memory for storing computer readable code for an application module;
• at least one processor coupled to the memory, said at least one processor executing the computer readable code in the memory to cause the application module to perform operations of:
• receiving a finite element analysis (FEA) model representing a blank sheet metal and a die face definition that includes a lancing route of a progressive lancing operation (PLO) that starts at a start time and ends at an end time, wherein the FEA model and the die face definition are used in a time-marching simulation of manufacturing a sheet metal part, the FEA model contains a plurality of nodes connected by a plurality of finite elements, and the lancing route is defined by a series of coordinates that includes start and end locations of the lancing route;
• conducting the time-marching simulation until the simulation time reaches the start time of the PLO, wherein the nodes and the finite elements of the FEA model have deformed due to contacts with the die face;
• identifying those of the finite elements crossed by the lancing route as a group of lacing route elements by comparing the coordinates of the lancing route with the deformed FEA model;
• creating a set of respective surrogate lancing route nodes by duplicating existed nodes along the lancing route of the deformed FEA model;
• creating respective nodal constraints to initially link together each of the existed nodes along the lancing route with a corresponding one of the surrogate lancing route nodes;
• splitting each of the lancing route elements into first and second new finite elements with the first new finite element being defined using the surrogate lancing route nodes, while the second new finite element being defined using the existed nodes, as a result, the first new finite element and the second new finite element are connected through the corresponding nodal constraints
• associating a separation time schedule for progressively removing said nodal constraints between the start time and the end time of the PLO;
• and
• conducting remaining of the time-marching simulation, in which each of the nodal constraints is removed in accordance with the separation time schedule to achieve numerical simulation of the PLO.

A non-transitory computer readable storage medium containing computer executable instructions for conducting a time-marching simulation of manufacturing a sheet metal part that requires progressive lancing operation by a method comprising:

• receiving, in a computer system, a finite element analysis (FEA) model representing a blank sheet metal and a die face definition that includes a lancing route of a progressive lancing operation (PLO) that starts at a start time and ends at an end time, wherein the FEA model and the die face definition are used in a time-marching simulation of manufacturing a sheet metal part, the FEA model contains a plurality of nodes connected by a plurality of finite elements, and the lancing route is defined by a series of coordinates that includes start and end locations of the lancing route;
• conducting the time-marching simulation until the simulation time reaches the start time of the PLO, wherein the nodes and the finite elements of the FEA model have deformed due to contacts with the die face;
• identifying those of the finite elements crossed by the lancing route as a group of lacing route elements by comparing the coordinates of the lancing route with the deformed FEA model;
• creating a set of respective surrogate lancing route nodes by duplicating existed nodes along the lancing route of the deformed FEA model;
• creating respective nodal constraints to initially link together each of the existed nodes along the lancing route with a corresponding one of the surrogate lancing route nodes;
• splitting each of the lancing route elements into first and second new finite elements with the first new finite element being defined using the surrogate lancing route nodes, while the second new finite element being defined using the existed nodes, as a result, the first new finite element and the second new finite element are connected through the corresponding nodal constraints;
• creating respective nodal constraints to initially link together said each of the existed nodes along the lancing route with the corresponding one of the surrogate lancing route nodes;
• associating a separation time schedule for progressively removing said nodal constraints between the start time and the end time of the PLO;
• and
• conducting remaining of the time-marching simulation, in which each of the nodal constraints is removed in accordance with the separation time schedule to achieve numerical simulation of the PLO.