9 results about "Integration point" patented technology

The invention provides a sealing assembly completion state solving method and device, and relates to the technical field of sealing element design. Comprising the following steps: acquiring geometric models of an elastic component and a matched component thereof, constructing an assembly initial configuration, performing finite element discretization on a sealing assembly system, and setting an integral point in the elastic component; in the assembly iteration process, corresponding projection points are determined based on the integration points and the component combination where the integration points are located, and the contact force at the integration points is calculated in combination with material parameters, the positions of the projection points and the surface geometric information of the matched components; and uniformly assembling the contact force and the internal elastic force generated by the elastic component under the current configuration into an overall force balance relationship for nonlinear iterative solution until a preset convergence condition is met, thereby obtaining a sealing assembly completion state. According to the method, the sealing assembly completion state can be stably solved under the condition that initial geometric interference exists, and the convergence and calculation stability of assembly simulation are improved by uniformly processing the contact force and the internal elastic force.

The invention discloses a diesel engine cylinder cover mechanical property mapping method, and belongs to the technical field of internal combustion engine structural strength analysis. The method comprises the following steps: acquiring microstructure node data based on casting simulation, and converting the microstructure node data into a node mechanical property field through a material model; after a mixed mapping strategy is adopted, target grid integration point coordinates are determined, source units are traversed in a source grid, whether the target grid integration points are located in the spatial range of the target grid integration points or not is judged, and confirmation is carried out according to the volume coordinate relation; performing high-fidelity interpolation on the integral points in the source units by adopting a shape function; for integral points which cannot be positioned, a k-d tree-based nearest neighbor node averaging method is adopted; and finally, writing the heterogeneous mechanical property field on the integral point into a structure analysis result. The method breaks through the precision and robustness bottlenecks of cross-scale and cross-grid data transmission, solves the problem that the material is difficult to couple with a stress field due to non-uniform material performance distribution, and provides a reliable data basis for high-precision fatigue life prediction of the cylinder cover.

The invention provides a plate spinning solid shell unit modeling and simulation visualization method based on ABAQUS, and belongs to the field of spinning forming numerical simulation. The method comprises the following steps of: constructing a calculation module by using a Fortran language and packaging the calculation module into a VUEL subprogram which can be called by ABAQUS; a subprogram VUSDFLD used for redefining variables on the integration points is written in the Fortran language; a three-dimensional finite element model of plate spinning is established in the ABAQUS; and calling an ABAQUS / Explicit solver and a subprogram to perform plate spinning simulation to obtain an ODB result file, constructing a result file reconstruction tool based on a Python secondary development technology of the ABAQUS, extracting node data of a calculation component and unit integral point data of a storage component, and creating a new ODB file for visualization. The method solves the problem that the simulation result of the user-defined entity shell unit (such as VUEL) in the ABAQUS cannot be directly written into the ODB file, so that post-processing visualization is difficult.

This invention discloses a method and system for calculating finite element data based on a material constitutive model, relating to the field of finite element simulation technology for metal stamping forming. The method includes: calculating the trial stress at the i-th increment step based on the strain increment at the element mesh integration point and the stress at the (i-1)-th increment step; calculating the yield function value based on the Von Mises yield criterion, using the trial stress, the strain at the (i-1)-th increment step, and the equivalent plastic strain rate; if the yield function value does not meet the preset yield condition, marking the trial stress as the actual simulated stress at the i-th increment step and obtaining the corresponding actual simulated strain; if the yield function value meets the preset yield condition, calculating the actual simulated stress at the element mesh integration point and the corresponding actual simulated strain at the i-th increment step based on the plastic flow law. This invention, when applied to finite element software, can accurately and effectively calculate finite element simulation data.

An analogue simulation method for the oxidation behavior of a C / SiC composite material component comprises the following steps that A1, Abaqus software is used for modeling the component, space coordinates of all integration points of the component are obtained, and an oxidation starting surface is designated; a2, writing a Python program, dividing grids based on a Delaunay algorithm, calculating the shortest distance from any integral point to all oxidation starting surfaces, and outputting the shortest distance; a3, compiling a C / SiC composite material oxidation analysis Umat subprogram based on Abaqus software by adopting a Fortran language, and reading shortest distance information; and A4, based on an existing C / SiC composite material oxidation diffusion mathematical model, a C / SiC finite element analysis model is established, and the oxidation expansion process of the component under different loads and temperatures is obtained.

This invention relates to the field of geophysical exploration technology, specifically to a well-to-surface electromagnetic forward modeling method, apparatus, and storage medium. The method includes: S1, modeling based on an octree mesh; S2, constructing vector Nédélec basis functions on the elements based on Gauss integration points and Gauss-Legendre-Lobatto (GLL) integration points set in the elements; S3, deriving the governing equations of the well-to-surface electromagnetic finite element method starting from Maxwell's equations; S4, constructing block diagonal preconditions and solving using an iterative method; S5, after exiting the iteration, calculating the electromagnetic response using the iterative model. This invention significantly reduces the number of elements in the mesh while maintaining model accuracy, thereby reducing computational costs. Higher-order shape functions are constructed and used in the forward modeling calculation to improve the accuracy of the numerical solution.

This invention provides an AI-adaptive finite element mesh and integral optimization method, system, medium, and device, belonging to the field of finite element simulation technology. The method includes: dividing the target region into an initial mesh and setting integration points; performing a preliminary simulation to obtain the physical field distribution; extracting physical field gradient data; constructing an input feature set by combining geotechnical medium parameters, mesh, and integration point information; training an AI optimization model using a physical information neural network to generate a dynamically adjusted scheme; and after performing a secondary simulation, re-inputting the updated gradient data into the AI ​​model, iteratively optimizing based on the topology change rate and physical field error until convergence. This invention aligns with geotechnical mechanics and seepage laws, avoids purely data-driven biases, significantly reduces redundant calculations while ensuring computational accuracy, and significantly improves the simulation efficiency and accuracy of physical fields such as stress, strain, and seepage. It is suitable for complex geological and nonlinear working conditions and has a high level of automation and intelligence.

The application discloses an extrusion deformation state detection method and system, electronic equipment and a storage medium, and relates to the technical field of extrusion deformation detection. The method comprises the following steps: determining the deformation calculation method corresponding to each node / integration point according to the initial data of each time step in a time step iteration manner, and then determining the extrusion deformation data of the target measured object at the time step according to the corresponding deformation calculation method of each node / integration point, and obtaining the extrusion deformation state of the object at all time points through time step iteration. The application selects the corresponding deformation calculation method for deformation operation according to different nodes / integration points, retains the operation advantages of the time-space stable node integration algorithm and the node smooth finite element algorithm, and can realize high-precision and high-efficiency extrusion deformation state detection.

This application provides a method and apparatus for solving the completed state of a sealed assembly, relating to the field of sealing component design technology. It includes: acquiring the geometric model of an elastic component and its mating components and constructing an initial assembly configuration; discretizing the sealed assembly system using finite element methods and setting integration points in the elastic component; during the assembly iteration process, determining the corresponding projection point based on the integration point and the component combination it contains, and calculating the contact force at the integration point by combining material parameters, the projection point position, and the surface geometry information of the mating components; and unifying the contact force and the internal elastic force generated by the elastic component under the current configuration into a unified force balance relationship for nonlinear iterative solution until a preset convergence condition is met, thereby obtaining the completed state of the sealed assembly. This application can stably solve the completed state of a sealed assembly even with initial geometric interference, and improves the convergence and computational stability of the assembly simulation by uniformly handling the contact force and internal elastic force.