Calculations of tool hardness in the aviation industry

Goncharenko, V. I.; Oleshko, V. S.

doi:10.3103/s1068798x17060119

Cited by 2 publications

(2 citation statements)

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“…The highest requirements for finished product non-destructive level are applied to structures created through purpose-oriented manufacturing procedures which influence a material structure. Such procedures include casting, welding, composite product production and so on [1][2][3][4].…”

Section: Introductionmentioning

confidence: 99%

X-Ray Computed Tomography-Based Analysis of Impact Damage Propagation in Composite Materials

Yurov¹

2019

Eurasian phys. tech. j.

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A composite structure impact damage propagation evaluation procedure using linear detectorequipped X-ray computed tomography scanner has been put forward. An impact damaged carbon-fiber samples research has been carried out to evaluate testing capabilities of internal delamination through X-ray computed tomography using linear detector. A special emphasis of the research has been laid on advanced composites. It is linked to the use of the composites for high-load structural elements and necessity of adjusting manufacturing procedures. The procedure helps simplify linear detector tomography analysis of delamination and verify mobile inspection methods data. Besides, the procedure may be used for developing composite structure repair methods. The article includes an example of tomographic image of impact-damaged samples linear attenuation coefficient distribution.

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Section: Introductionmentioning

confidence: 99%

X-Ray Computed Tomography-Based Analysis of Impact Damage Propagation in Composite Materials

Yurov¹

2019

Eurasian phys. tech. j.

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“…Feature of CM is that they are not monolithic material, such as metals. KM is a structure which created in the process of manufacturing a product [1][2][3]. There is a problem of an objective assessment of quality of KM, possibility of application of various physical methods for control of their quality.…”

Section: Introductionmentioning

confidence: 99%

Experimental Study of Changes in the Structure of Polymer Composite Material by Computational X-Ray Tomography

V.M.¹

2019

Eurasian phys. tech. j.

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In article on the basis of the method of computing x-ray tomography the technique of assessing changes in the state structure of polymeric composite material under the dead load. The results of the analysis of structure changes for carbon fiber samples at the setting stage of loading are presented. Offered exploratory procedure allows to fracture propagation under the force action and to analyze the material changes depending on the presence and load levels. In addition, quantitative parameters are introduced to compare the tendency of the material to accumulate damage in various technological processes. The results of the test research show that the proposed method allows for high accuracy to analyze the behavior of the material under load and identify typical trends for the type of material and laying.

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Calculations of tool hardness in the aviation industry

Cited by 2 publications

References 0 publications

X-Ray Computed Tomography-Based Analysis of Impact Damage Propagation in Composite Materials

X-Ray Computed Tomography-Based Analysis of Impact Damage Propagation in Composite Materials

Experimental Study of Changes in the Structure of Polymer Composite Material by Computational X-Ray Tomography

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