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Topological optimization method for multi-load fatigue life constraints

A topology optimization and fatigue life technology, applied in constraint-based CAD, design optimization/simulation, special data processing applications, etc., can solve problems such as differences in safety factor values, failure to meet fatigue strength requirements, and impact on lightweight results. Achieve the effect of ensuring accuracy and effectiveness and improving efficiency

Active Publication Date: 2020-11-17
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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  • Topological optimization method for multi-load fatigue life constraints
  • Topological optimization method for multi-load fatigue life constraints
  • Topological optimization method for 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 topological optimization method for multi-load fatigue life constraint, which comprises the following steps of: obtaining a structure dangerous point position and extractinga stress time history by a finite element method aiming at a random vibration load borne by a component; counting the stress time history through a rain flow counting method, sorting the stress timehistory according to amplitudes, and segmenting the stress time history in a variable interval manner; according to a fatigue damage equivalence principle, adopting a Miner linear cumulative damage method to perform damage equivalent conversion, and the load cycles in the interval are combined into one load cycle; then, based on the linear damage accumulation criterion and the multi-axis fatigue analysis principle, reversely calculating the maximum stress level enabling the component to be subjected to fatigue failure according to the design life requirement of the component, and obtaining theoptimal structure of the component by taking the stress level as the constraint condition of topological optimization. According to the method, the fatigue life constraint under the complex random load can be efficiently converted into the stress constraint, so that the lightweight design of the structure is achieved while the fatigue strength is met, and engineering application is facilitated.

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 Applications(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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