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Prediction method for stress-strain response and strength of braided ceramic matrix composite

A composite material and prediction method technology, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve the problems of low process efficiency, large dispersion of measurement results, and difficulty in ensuring the accuracy of prediction results, so as to avoid prediction. Error, the effect of improving efficiency

Active Publication Date: 2019-06-07
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

However, when using this method, mesoscopic material parameters such as fiber volume fraction, fiber elastic modulus, fiber strength distribution, matrix volume fraction, matrix elastic modulus, matrix strength and interfacial shear strength are required, and the measurement of these parameters requires a large number of There are many tests, and the measurement results are highly dispersed, which makes the process of predicting the stress-strain response and strength of braided CMCs very inefficient, and the accuracy of the prediction results is difficult to guarantee

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  • Prediction method for stress-strain response and strength of braided ceramic matrix composite
  • Prediction method for stress-strain response and strength of braided ceramic matrix composite
  • Prediction method for stress-strain response and strength of braided ceramic matrix composite

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Embodiment Construction

[0029] The present invention will be described in detail below in conjunction with the accompanying drawings. Such as figure 1 As shown, the present invention provides a method for predicting the stress-strain response and strength of braided ceramic matrix composites, the method comprising the following steps:

[0030] Step 1: Straighten a section of fiber bundle, the fiber is of the same brand as the fiber in the woven ceramic matrix composite material, put the fiber bundle and the woven ceramic matrix composite material prefabricated body into a furnace to deposit the interface layer and the matrix. After deposition, the woven ceramic matrix composite material preform becomes the woven ceramic matrix composite material, and the fiber bundles become fiber bundles with a matrix. Such as figure 2 As shown, the fiber bundle with matrix is ​​composed of fiber 1, matrix 2 and interfacial layer 3 between fibers / matrix. Since it is made in the same furnace as the braided cerami...

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Abstract

The invention discloses a prediction method for stress-strain response and strength of braided ceramic matrix composite. The method is characterized by comprising the following steps: preparing a beltmatrix fiber bundle with the same in-situ performance as woven CMCs, establishing a unit cell finite element model for the belt matrix fiber bundle, and performing finite element calculation on the unit cell finite element model to obtain the stress-strain response with matrix fiber bundles, and the maximum value of stress on stress-strain curve is strength of woven CMCs.. According to the prediction method for stress-strain response and strength of braided ceramic matrix composite, mechanical properties of fibers, a matrix and a fiber / matrix interface do not need to be used as input quantities; only the mechanical property of the yarn needs to be measured, a large number of component material performance test experiments can be omitted, prediction errors caused by component material performance test dispersity can be avoided, and therefore the efficiency of the prediction process and the accuracy of the prediction result can be greatly improved.

Description

technical field [0001] The invention relates to a method for predicting the mechanical properties of a composite material, in particular to a method for predicting the stress-strain response and strength of a braided ceramic matrix composite material. Background technique [0002] Braided ceramic matrix composites (Ceramic Matrix Composite: hereinafter referred to as CMCs) have the advantages of high temperature resistance, high specific strength, high specific modulus, insensitivity to notches, and strong designability of material properties. They are ideal for high-temperature components of next-generation aeroengines Material. Stress-strain response and strength are the two most important mechanical properties of braided CMCs, because stress-strain response affects the deformation of braided CMCs structural members, while strength involves the failure of braided CMCs structural members. [0003] Braided CMCs are the skeleton of braided CMCs because the yarns are cross-co...

Claims

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Application Information

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IPC IPC(8): G06F17/50
Inventor 张盛高希光宋迎东
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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