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A topology optimization method with multi-load fatigue life constraints

A topology optimization and fatigue life technology, applied in the field of topology optimization with multi-load fatigue life constraints, can solve problems such as the impact of lightweight results, differences in safety factor values, and failure to meet fatigue strength requirements, achieving important academic significance and engineering applications value, improve efficiency, and realize the effect of lightweight design

Active Publication Date: 2022-04-19
YANSHAN UNIV
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Problems solved by technology

When the allowable stress is selected as the stress constraint in topology optimization, the value of the safety factor will vary due to different designers, which will affect the lightweight results; under the action of actual cyclic loads, the work that causes fatigue failure of the mechanical structure Stresses are often lower than the calculated allowable stress values
As a result, the optimization results often do not meet the fatigue strength requirements

Method used

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  • A topology optimization method with multi-load fatigue life constraints
  • A topology optimization method with multi-load fatigue life constraints
  • A topology optimization method with multi-load fatigue life constraints

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Embodiment Construction

[0041] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0042] The invention discloses a topology optimization method with multi-load fatigue life constraints, comprising the following steps:

[0043] Step 1. Establish as figure 1 The L-shaped plate, the top end of the L-shaped plate is fixed, such as figure 2 The random load shown is applied vertically on the figure 1 In the position shown, the material is aluminum alloy 7075-T6, its elastic modulus E=7.17E10Pa, Poisson’s ratio υ=0.33, density ρ=2.81e-3g / mm3 Carry out dynamic analysis on the L-shaped plate to find the fatigue dangerous parts , and extract the stress time history of the dangerous part, and then use the Von Mises equivalent stress criterion to convert the multiaxial stress to the uniaxial stress, such as image 3 shown;

[0044] Step 2. Statistical fatigue load spectrum by rainflow counting method to obtain stress amplitude, stre...

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Abstract

The invention relates to a topology optimization method for multi-load fatigue life constraints. Aiming at the random vibration loads suffered by components, the positions of structural dangerous points are obtained through the finite element method and the stress time history is extracted; the stress time history is calculated by the rainflow counting method. Counting processing, sorting according to the amplitude and changing the interval into segments; then according to the equivalent principle of fatigue damage, using the Miner linear cumulative damage method to convert the damage equivalent, and combining the load cycles in the interval into one load cycle; then, based on Based on the principle of linear damage accumulation and multi-axial fatigue analysis, the design life of the component is required to calculate the maximum stress level that causes fatigue damage to the component, and use this stress level as the constraint condition of topology optimization to obtain the optimal structure of the component. The invention can efficiently transform the fatigue life constraints under complex random loads into stress constraints, thereby realizing the lightweight design of the structure while satisfying the fatigue strength, which is beneficial to engineering applications.

Description

technical field [0001] The invention relates to a topology optimization method with multi-load fatigue life constraints, belonging to the technical field of structural lightweight design. Background technique [0002] The purpose of structural optimization is to improve the performance of the structure. Under the premise of meeting the design requirements, the material can be optimally distributed by changing the topological form and size of the structure. Topology optimization is widely used in aviation, aerospace, automobiles and other fields, making the structure lighter and lighter, and its performance continuously improved. At present, a large number of studies have been carried out on topology optimization under the constraints of displacement, stiffness, strength, frequency, volume, and mass in engineering practice. When the allowable stress is selected as the stress constraint in topology optimization, the value of the safety factor will vary due to different design...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/17G06F30/23G06F119/02G06F119/14G06F111/04
CPCG06F30/17G06F30/23G06F2119/02G06F2119/14G06F2111/04
Inventor 李永欣常涛周国云李凯伦
Owner YANSHAN UNIV
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