Eurasian Physical Technical Journal. 2019; 16: 31-35
X-RAY COMPUTED TOMOGRAPHY-BASED ANALYSIS OF IMPACT DAMAGE PROPAGATION IN COMPOSITE MATERIALS
https://doi.org/10.31489/2019No2/31-35Аннотация
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.
Список литературы
1. Kluiev V.V., Sosin F.R., Kovalev A.V., Weinberg E.I. et al. Nerazrushaiuschii control I diagnostika, 2-nd edition. Мoscow, Mashinostroenie, 2003, 656 p. [in Russian]
2. Weinberg E.I., Weinberg I.A. Computed Tomography Scanners for Non-Destructive Testing and Quantity-related Diagnostics of Aerospace Products. Dvigatel. 2008, No. 2, pp. 19 – 23. [in Russian]
3. Goncharenko V.I., Oleshko V.S. Calculations of Tool Hardness in the Aviation Industry. Russian Engineering Research. 2017, Vol.37, No.6, pp. 554–556. DOI: 10.3103/S1068798X17060119.
4. Goncharenko V.I., Oleshko V.S. Determining the surface energy of tools in the aviation industry. Engineering Research. 2017, Vol.37, No.7, pp. 628–630. DOI: 10.3103/S1068798X17070127.
5. Boitsov B.V., Vasiliev S.L., Gromashev A.G., Yurgenson S.A. Metody nerazrushaiuschego kontrolya, primeniaemie dlya konstruktsiy iz perspektivnikh kompozitsionnikh materialov. MAI, Electronic Journal. 27.12.2011. Release No 49. Available at: http://www.mai.ru/science/trudy/. [in Russian]
6. Vasiliev S.L., Artemiev A.V., Yurgenson S.A. Analiz metodom vichislitelnoi rentgenovskoi tomografii vozdeistviaa staticheskoi nagruzki na strukturu polimernogo kompozitsionnogo materiala. Proceedings of 10th International Conference on Non-Equilibrium Processes in Nozzles and Streams (NPNJ 2014), May 25-31, 2014, Alushta. М.: MAI, 2014. pp. 543-545. [in Russian]
7. Vasiliev S.L., Artemiev A.V., Bakulin V.N., Yurgenson S.A. Kontrol obraztov metodom vichislitelnoi rentgenovskoi tomografii pod nagruzkoi. Russian Journal of Nondestructive Testing, 2016, No.5. pp. 63-73.
8. Advisory Circular № 20-107B Composite aircraft structure, USA, FAA, 2009. Available at: www.faa.gov/documentLibrary/media/Advisory_Circular/AC20-107B.pdf.
9. Mikulik Z., Kelly D.W., Prusty B.G., Thomson R.S. Prediction of flange debonding in composite stiffened panels using an analytical crack tip element-based methodology. Composite Structures. 2008, Vol.85, No. 3, pp. 233 – 244. DOI:10.1016/j.compstruct. 2007.10.027.
10. Nishino T., Hirokane D., Nakamae K. X-ray diffraction studies of the environmental deterioration of a transversely loaded carbon-fiber-reinforced composite. Composites Science and Technology. 2001, Vol.61, No.16, pp. 2455 – 2459. DOI:10.1016/S0266-3538(01)00174-9.
11. DeKalbermatten T., Jäggi R., FLüeler P., Kausch H.H., Davies P. Microfocus radiography studies during model interlaminar fracture tests on composites. Journal of Materials Science Letters. 1992, Vol.11, No.9, pp. 543 – 546.
12. Yurov V.M., Oleshko V.S. The impact of the environment on the contact potential difference of metal machine parts. Eurasian Physical Technical Journal. 2019, Vol.16, No.1 (31), pp. 99 – 108.
13. Oleshko V.S. Optimal Number of Duralumin Samples in Determining the Surface Energy. Russian Engineering Research, 2019, Vol. 39, No. 3, pp. 272–275. https://doi.org/10.3103/ S1068798X19030183.
Eurasian Physical Technical Journal. 2019; 16: 31-35
X-RAY COMPUTED TOMOGRAPHY-BASED ANALYSIS OF IMPACT DAMAGE PROPAGATION IN COMPOSITE MATERIALS
https://doi.org/10.31489/2019No2/31-35Abstract
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.
References
1. Kluiev V.V., Sosin F.R., Kovalev A.V., Weinberg E.I. et al. Nerazrushaiuschii control I diagnostika, 2-nd edition. Moscow, Mashinostroenie, 2003, 656 p. [in Russian]
2. Weinberg E.I., Weinberg I.A. Computed Tomography Scanners for Non-Destructive Testing and Quantity-related Diagnostics of Aerospace Products. Dvigatel. 2008, No. 2, pp. 19 – 23. [in Russian]
3. Goncharenko V.I., Oleshko V.S. Calculations of Tool Hardness in the Aviation Industry. Russian Engineering Research. 2017, Vol.37, No.6, pp. 554–556. DOI: 10.3103/S1068798X17060119.
4. Goncharenko V.I., Oleshko V.S. Determining the surface energy of tools in the aviation industry. Engineering Research. 2017, Vol.37, No.7, pp. 628–630. DOI: 10.3103/S1068798X17070127.
5. Boitsov B.V., Vasiliev S.L., Gromashev A.G., Yurgenson S.A. Metody nerazrushaiuschego kontrolya, primeniaemie dlya konstruktsiy iz perspektivnikh kompozitsionnikh materialov. MAI, Electronic Journal. 27.12.2011. Release No 49. Available at: http://www.mai.ru/science/trudy/. [in Russian]
6. Vasiliev S.L., Artemiev A.V., Yurgenson S.A. Analiz metodom vichislitelnoi rentgenovskoi tomografii vozdeistviaa staticheskoi nagruzki na strukturu polimernogo kompozitsionnogo materiala. Proceedings of 10th International Conference on Non-Equilibrium Processes in Nozzles and Streams (NPNJ 2014), May 25-31, 2014, Alushta. M.: MAI, 2014. pp. 543-545. [in Russian]
7. Vasiliev S.L., Artemiev A.V., Bakulin V.N., Yurgenson S.A. Kontrol obraztov metodom vichislitelnoi rentgenovskoi tomografii pod nagruzkoi. Russian Journal of Nondestructive Testing, 2016, No.5. pp. 63-73.
8. Advisory Circular № 20-107B Composite aircraft structure, USA, FAA, 2009. Available at: www.faa.gov/documentLibrary/media/Advisory_Circular/AC20-107B.pdf.
9. Mikulik Z., Kelly D.W., Prusty B.G., Thomson R.S. Prediction of flange debonding in composite stiffened panels using an analytical crack tip element-based methodology. Composite Structures. 2008, Vol.85, No. 3, pp. 233 – 244. DOI:10.1016/j.compstruct. 2007.10.027.
10. Nishino T., Hirokane D., Nakamae K. X-ray diffraction studies of the environmental deterioration of a transversely loaded carbon-fiber-reinforced composite. Composites Science and Technology. 2001, Vol.61, No.16, pp. 2455 – 2459. DOI:10.1016/S0266-3538(01)00174-9.
11. DeKalbermatten T., Jäggi R., FLüeler P., Kausch H.H., Davies P. Microfocus radiography studies during model interlaminar fracture tests on composites. Journal of Materials Science Letters. 1992, Vol.11, No.9, pp. 543 – 546.
12. Yurov V.M., Oleshko V.S. The impact of the environment on the contact potential difference of metal machine parts. Eurasian Physical Technical Journal. 2019, Vol.16, No.1 (31), pp. 99 – 108.
13. Oleshko V.S. Optimal Number of Duralumin Samples in Determining the Surface Energy. Russian Engineering Research, 2019, Vol. 39, No. 3, pp. 272–275. https://doi.org/10.3103/ S1068798X19030183.
