CN105574306A - Method for obtaining theoretical strain in strength finite element analysis - Google Patents

Method for obtaining theoretical strain in strength finite element analysis Download PDF

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Publication number
CN105574306A
CN105574306A CN201410535565.XA CN201410535565A CN105574306A CN 105574306 A CN105574306 A CN 105574306A CN 201410535565 A CN201410535565 A CN 201410535565A CN 105574306 A CN105574306 A CN 105574306A
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strain
finite element
strength
analysis
element analysis
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鬲钰焯
范瑞娟
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Xian Aircraft Design and Research Institute of AVIC
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Xian Aircraft Design and Research Institute of AVIC
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Abstract

The invention provides a method for obtaining theoretical strain in strength finite element analysis. The method is characterized by comprising the following steps: (1) according to a finite element principle and a strain sensor measurement principle, establishing an additional bar element according to any given position and direction in the finite element model of a test specimen; (2) in order to prevent the additional bar element from affecting local structural stress and strain distribution characteristics, requiring to define that bar element stiffness characteristics are infinitesimal relative to the local structural stiffness characteristics; and (3) after analysis and solution are carried out, directly reading bar element strain in a result, wherein the strain is theoretical strain under any given position and direction.

Description

一种在强度有限元分析中获取理论应变的方法A Method of Obtaining Theoretical Strain in Strength Finite Element Analysis

技术领域technical field

本发明属于强度有限元分析与试验验证领域,涉及一种在强度有限元分析中获取理论应变的方法。The invention belongs to the field of strength finite element analysis and test verification, and relates to a method for obtaining theoretical strain in strength finite element analysis.

背景技术Background technique

强度分析中有限元方法使用越来越广泛和深入,而强度试验与有限元分析相互验证日益普遍,强度试验中通常需要通过应变传感器对试验件中给定位置和方向的应变进行测量;通过对比试验件应变与有限元分析中对应位置和方向的应变的差异来判断有限元分析或试验的正确性,因此有限元分析中对应位置和方向的应变的获取就显得尤为重要。The use of finite element method in strength analysis is becoming more and more extensive and in-depth, and the mutual verification of strength test and finite element analysis is becoming more and more common. In strength test, it is usually necessary to measure the strain at a given position and direction in the test piece through a strain sensor; by comparing The correctness of the finite element analysis or test is judged by the difference between the strain of the test piece and the strain corresponding to the position and direction in the finite element analysis, so the acquisition of the strain corresponding to the position and direction in the finite element analysis is particularly important.

以往在有限元分析中获取给定位置和方向应变时需要以下几步:首先根据分析结果对试验中应变传感器位置和方向进行确定,再根据试验中应变传感器位置和方向对有限元模型进行分割,然后对分割出的区域根据应变传感器方向建立局部坐标系,并将分割出的区域在已建立的述坐标系下赋予方向,接着按正常步骤求解,最后在各个分割出区域对应的坐标系下读取应变,此应变为试验件中应变传感器处的理论应变。In the past, the following steps were required to obtain the strain at a given position and direction in finite element analysis: first, determine the position and direction of the strain sensor in the test according to the analysis results, and then divide the finite element model according to the position and direction of the strain sensor in the test, Then establish a local coordinate system for the segmented area according to the direction of the strain sensor, and give the segmented area a direction in the established coordinate system, then follow the normal steps to solve it, and finally read it in the coordinate system corresponding to each segmented area Take the strain, which is the theoretical strain at the strain sensor in the test piece.

上述方法的繁琐性在于:对复杂形势试验件需要进行多次分割,多次定义坐标系,多次对分割出区域赋予方向,某位置应变还要在其对应坐标系下读取。The cumbersomeness of the above method lies in that it is necessary to divide the test piece in a complex situation multiple times, define the coordinate system multiple times, and assign directions to the segmented area multiple times, and the strain at a certain position must be read in its corresponding coordinate system.

发明内容Contents of the invention

本发明的目的是:提供一种强度有限元分析中获取理论应变的方法The purpose of the invention is to provide a method for obtaining theoretical strain in strength finite element analysis

本发明的技术方案是:一种强度有限元分析中获取理论应变的方法,包括以下步骤:The technical solution of the present invention is: a method for obtaining theoretical strain in strength finite element analysis, comprising the following steps:

步骤一:根据有限元原理和应变传感器测量原理,在试验件的有限元模型中根据给定的任意位置和方向建立附加杆元;Step 1: According to the finite element principle and the measurement principle of the strain sensor, an additional rod element is established according to the given arbitrary position and direction in the finite element model of the test piece;

步骤二:为使附加杆元不影响当地结构应力及应变分布特性,需定义杆元刚度特性相对结构当地刚度特性无穷小;Step 2: In order to ensure that the additional rod elements do not affect the local structural stress and strain distribution characteristics, it is necessary to define that the stiffness characteristics of the rod elements are infinitely small relative to the local stiffness characteristics of the structure;

步骤三:分析求解后直接在结果中读取杆元应变,此应变为给定的任意位置和方向下的理论应变。Step 3: After analyzing and solving, directly read the rod element strain in the result, which is the theoretical strain at any given position and direction.

本发明的优点是:本发明方法使用附加杆元模拟应变传感器,相较以往步骤:建立有限元模型——分割划分区域——建立局部坐标系——赋予材料方向——分析求解——在局部坐标系下读取理论应变,大大简化了理论应变的获取步骤,原理简单明了,易于操作。The advantage of the present invention is: the method of the present invention uses the additional rod element to simulate the strain sensor, compared with the previous steps: establishing the finite element model——dividing and dividing the area—establishing the local coordinate system—giving the material direction—analyzing and solving—in the local Reading the theoretical strain in the coordinate system greatly simplifies the steps of obtaining the theoretical strain, the principle is simple and clear, and it is easy to operate.

附图说明Description of drawings

图1是试验件有限元模型局部网格图;Figure 1 is a local grid diagram of the finite element model of the test piece;

图2是试验件添加了杆元后的有限元模型局部网格图;Fig. 2 is the local grid diagram of the finite element model after the rod element is added to the test piece;

具体实施方式detailed description

下面结合附图对本发明做进一步详细说明,请参阅图1至图2.The present invention will be described in further detail below in conjunction with accompanying drawing, please refer to Fig. 1 to Fig. 2.

如图1所示,为试验件有限元模型局部网格图;As shown in Figure 1, it is the local mesh diagram of the finite element model of the test piece;

如图2所示,在试验件的有限元模型中根据给定的任意位置和方向建立附加杆元,编号为1号~15号;As shown in Figure 2, in the finite element model of the test piece, the additional rod elements are established according to the given arbitrary position and direction, numbered from No. 1 to No. 15;

一种强度有限元分析中获取理论应变的方法,包括以下步骤:A method for obtaining theoretical strain in strength finite element analysis, comprising the following steps:

步骤一:根据有限元原理和应变传感器测量原理,在试验件的有限元模型中根据给定的任意位置和方向建立附加杆元;Step 1: According to the finite element principle and the measurement principle of the strain sensor, an additional rod element is established according to the given arbitrary position and direction in the finite element model of the test piece;

步骤二:定义杆元刚度特性相对结构当地刚度特性无穷小;Step 2: Define the stiffness characteristics of the rod element to be infinitely small relative to the local stiffness characteristics of the structure;

步骤三:分析求解后直接在结果中读取杆元应变,此应变为给定的任意位置和方向下的理论应变。Step 3: After analyzing and solving, directly read the rod element strain in the result, which is the theoretical strain at any given position and direction.

本发明的优点是:本发明方法使用附加杆元模拟应变传感器,相较以往步骤:建立有限元模型——分割划分区域——建立局部坐标系——赋予材料方向——分析求解——在局部坐标系下读取理论应变,大大简化了理论应变的获取步骤,原理简单明了,易于操作。The advantage of the present invention is: the method of the present invention uses the additional rod element to simulate the strain sensor, compared with the previous steps: establishing the finite element model——dividing and dividing the area—establishing the local coordinate system—giving the material direction—analyzing and solving—in the local Reading the theoretical strain in the coordinate system greatly simplifies the steps of obtaining the theoretical strain, the principle is simple and clear, and it is easy to operate.

Claims (2)

1.一种在强度有限元分析中获取理论应变的方法,其特征在于,包括以下步骤:1. A method for obtaining theoretical strain in strength finite element analysis, is characterized in that, comprises the following steps: (1)根据有限元原理和应变传感器测量原理,在试验件的有限元模型中根据给定的任意位置和方向建立附加杆元;(1) According to the finite element principle and the measurement principle of the strain sensor, an additional rod element is established according to a given arbitrary position and direction in the finite element model of the test piece; (2)为使附加杆元不影响当地结构应力及应变分布特性,需定义杆元刚度特性相对结构当地刚度特性无穷小;(2) In order to prevent the additional rod elements from affecting the local structural stress and strain distribution characteristics, it is necessary to define that the stiffness characteristics of the rod elements are infinitesimally small relative to the local stiffness characteristics of the structure; (3)分析求解后直接在结果中读取杆元应变,此应变为给定的任意位置和方向下的理论应变。(3) After analyzing and solving, directly read the rod element strain in the result, which is the theoretical strain at any given position and direction. 2.根据权利要求1所述的在强度有限元分析中获取理论应变的方法,其特征在于,步骤1中建立附加杆元具体为:在试验件的有限元模型中给定的任意位置和方向选取应变传感器轴向的两个节点,利用这两个节点建立杆元。2. the method for obtaining theoretical strain in strength finite element analysis according to claim 1, is characterized in that, in step 1, establishes additional rod element specifically: given arbitrary position and direction in the finite element model of test piece Select two nodes in the axial direction of the strain sensor, and use these two nodes to establish the rod element.
CN201410535565.XA 2014-10-11 2014-10-11 Method for obtaining theoretical strain in strength finite element analysis Pending CN105574306A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105930616A (en) * 2016-05-16 2016-09-07 中国航空工业集团公司西安飞机设计研究所 Load distribution method for statically indeterminate structure of dynamic wing surface of aircraft
CN108052740A (en) * 2017-12-13 2018-05-18 中国飞机强度研究所 A kind of corresponding finite element unit screening technique of foil gauge
CN111177848A (en) * 2019-12-26 2020-05-19 中国航空工业集团公司西安飞机设计研究所 A method and device for obtaining theoretical strain value based on finite element model

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101582095A (en) * 2009-06-19 2009-11-18 东南大学 Non-linear dynamic finite element method for determining cable-strut system static balancing state
CN103279611A (en) * 2013-05-29 2013-09-04 东南大学 Method for optimized arrangement of strain sensor

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101582095A (en) * 2009-06-19 2009-11-18 东南大学 Non-linear dynamic finite element method for determining cable-strut system static balancing state
CN103279611A (en) * 2013-05-29 2013-09-04 东南大学 Method for optimized arrangement of strain sensor

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
刘旺玉等: "基于特征的实用性有限元模型化知识系统", 《机械强度》 *
叶尚辉: "建立有限元模型的一般方法", 《电子机械工程》 *
徐元铭等: "航空薄壁结构有限元建模的智能化求解模型研究", 《南京航空航天大学学报》 *
赵滇生等: "有限元模型对输电塔架结构动力特性分析的影响", 《特种结构》 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105930616A (en) * 2016-05-16 2016-09-07 中国航空工业集团公司西安飞机设计研究所 Load distribution method for statically indeterminate structure of dynamic wing surface of aircraft
CN105930616B (en) * 2016-05-16 2019-09-06 中国航空工业集团公司西安飞机设计研究所 A Load Distribution Method for Hyperstatically Indeterminate Structure of Aircraft Moving Wing Surface
CN108052740A (en) * 2017-12-13 2018-05-18 中国飞机强度研究所 A kind of corresponding finite element unit screening technique of foil gauge
CN111177848A (en) * 2019-12-26 2020-05-19 中国航空工业集团公司西安飞机设计研究所 A method and device for obtaining theoretical strain value based on finite element model
CN111177848B (en) * 2019-12-26 2023-05-23 中国航空工业集团公司西安飞机设计研究所 A method and device for obtaining theoretical strain values based on a finite element model

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Application publication date: 20160511