Method for processing stress-fringe-order numerical values of photoelastic model

An elastic model and processing method technology, applied in the field of photoelasticity testing, can solve problems such as the inability to control the test accuracy effectively, the processing method accuracy is low, the stress fringe level is small, etc., achieving low processing cost, increased fringe level, The effect of precise and effective control

Active Publication Date: 2014-08-06
CHINA AVIATION POWER MACHINE INST
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Problems solved by technology

[0005] The purpose of the present invention is to provide a method for processing the stress stripe level value of a photoelastic model, so as to solve the problem of the low accuracy of the processing method for obtaining the stress stripe level value of the rotating part in the existing photoelasticity test; The stress fringes are sparse, the stress fringe level value is small, and the initial stress fringe seriously interferes with the accurate interpretation of the model stress fringe level value, resulting in a technical problem that the accuracy of the test cannot be effectively controlled

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  • Method for processing stress-fringe-order numerical values of photoelastic model

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Embodiment Construction

[0027] The embodiments of the present invention will be described in detail below with reference to the accompanying drawings, but the present invention can be implemented in various ways defined and covered.

[0028] figure 1 It is a schematic flow chart of the processing method of the stress fringe series of the photoelastic model of the preferred embodiment of the present invention, as figure 1 As shown, the processing method of the stress fringe level value of the photoelastic model of the present embodiment includes the following steps: a, select a part of the rotating photoelastic model test piece and adopt the same manufacturing method as the photoelastic model to make an auxiliary photoelastic model; b . Convert the rotational centrifugal force acting on the auxiliary photoelastic model into a tensile force, and perform stepwise incremental freeze loading on the auxiliary photoelastic model; c. Experiments to obtain the stress stripe level values ​​of the auxiliary pho...

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Abstract

The invention discloses a method for processing stress-fringe-order numerical values of a photoelastic model. The method comprises the following steps that (1) part of a rotating photoelastic model test piece is selected, and a manufacturing method same as the method for manufacturing the photoelastic model is used for manufacturing an auxiliary photoelastic model; (2) rotating centrifugal force acting on the auxiliary photoelastic model is converted into tension, and the auxiliary photoelastic model is subjected to classified increment freezing loading; (3) test data of stress-fringe-order numerical values of the auxiliary photoelastic model subjected to classified increment freezing loading are acquired, and are subjected to curve fitting; (4) the stress-fringe-order numerical values of the photoelastic model are corrected by using fitting data variables. The stress-fringe-order numerical values of the photoelastic model obtained through the method are more close to the real stress level.

Description

technical field [0001] The invention relates to the field of photoelasticity tests, in particular to a method for processing stress stripe level values ​​of a photoelastic model. Background technique [0002] At present, the stress distribution of the test piece obtained by the photoelastic test is the main technical means used to evaluate the working stress in the product prototype design, and plays an important role in the strength analysis of product design. [0003] The photoelastic test object is the photoelastic model. With the development of aviation technology, more and more test pieces are prototyped as high-speed rotating parts, but the photoelastic model is not suitable for high-speed rotation, and the test equipment has certain limitations on the applied load. However, sometimes the stress stripes in the model are sparse after the test, and the highest stress stripe level value is too small. In this case, the error of the model stress stripe level value read out ...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01L1/24
Inventor 郭天才廖学军刘飞春
Owner CHINA AVIATION POWER MACHINE INST
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