The effect of the addition of nanotubes upon the thermo-protective properties of the aramid-reinforced composite

• Autorzy: Przybylek P. , Korbela M. , Szczepaniak R. , Komorek A. , Krzyzak A , Babel R.

Identyfikatory

DOI

10.5604/01.3001.0012.2844

• Języki publikacji: EN

Abstrakty

EN

The aim of this article is to present findings concerning the thermo-protective research into ablative materials. The authors analysed the impact of the addition of carbon nanotubes upon the selected ablation properties, i.e. the ablation mass waste, average linear rate of ablation and the backside temperature of the specimens. The performed tests as well as the obtained findings allowed formulating a number of conclusions, which are useful in creating future composites. Composition of individual test samples; ablation testing; average relative ablation mass loss, depending on the volume share of carbon nanotubes; average ablation rate, depending on the volume share of carbon nanotubes; temperature of the rear surface of the insulating sample, depending on the volume share of carbon nanotubes; temperature inside the composite, depending on the volume share of carbon nanotubes; comparison of the temperature of ablation surface, temperature inside the composite and temperature on the rear surface of the wall of carbon nanotubes after the exposition to a heat flux are presented in the article.

Słowa kluczowe

EN

ablative materials; composites; thermal resistance; ablation properties

• Wydawca: Łukasiewicz Research Network - Institute of Aviation ; European Science Society of Powertrain and Transport KONES Poland ; Wydawnictwo Instytutu Technicznego Wojsk Lotniczych
• Czasopismo: Journal of KONES
• Rocznik: 2018
• Tom: Vol. 25, No. 2
• Strony: 295--301
• Opis fizyczny: Bibliogr. 13 poz., rys.

Twórcy

autor

Przybylek P.

• Polish Air Force Academy, Aeronautics Faculty Dywizjonu 303 Street 25, 08-521 Deblin, Poland tel.: + 48 261 517 427

autor

Korbela M.

• Polish Air Force Academy, Aeronautics Faculty Dywizjonu 303 Street 25, 08-521 Deblin, Poland tel.: + 48 261 517 427

autor

Szczepaniak R.

• Polish Air Force Academy, Aeronautics Faculty Dywizjonu 303 Street 25, 08-521 Deblin, Poland tel.: + 48 261 517 427

autor

Komorek A.

• Polish Air Force Academy, Aeronautics Faculty Dywizjonu 303 Street 25, 08-521 Deblin, Poland tel.: + 48 261 517 427

autor

Krzyzak A

• Polish Air Force Academy, Aeronautics Faculty Dywizjonu 303 Street 25, 08-521 Deblin, Poland tel.: + 48 261 517 427

autor

Babel R.

• Polish Air Force Academy, Aeronautics Faculty Dywizjonu 303 Street 25, 08-521 Deblin, Poland tel.: + 48 261 517 427

Bibliografia

• [1] Badhe, Y., Balasubramanian, K., Novel hybrid ablative composites of resorcinol formaldehyde as thermal protection systems for re-entry vehicles, RSC Adv. 2014.
• [2] Basavarajappa, S., Ellangovan, S., Dry sliding wear characteristics of glass–epoxy composite filled with silicon carbide and graphite particles, Wear, Vol. 296, pp. 491-496, 2012.
• [3] Bian, L. P., Xiao, J. Y., Zeng, J. C., Xing, S. L., Yin, C. P., Microstructural interpretation of the ablative properties of phenolic–quartz hybrid fabric reinforced phenolic resin composites, Materials and Design, Vol. 62, pp. 424-429, 2014.
• [4] Biswas, S., Kindo, S., Patnaik, A., Effect of Fiber Length on Mechanical Behavior of Coir Fiber Reinforced Epoxy composites, Fibers and Polymers, Vol. 12, pp. 73-78, 2011.
• [5] Garoushi, S., Vallittu, P. K., Watts, D. C., Lassila, L. V. J., Effect of nanofiller fractions and temperature on polymerization shrinkage on glass fibre reinforced filling material, Dental Materials, Vol. 24, pp. 606-610, 2008.
• [6] Kim, S. Y., Baek, S. J., Youn, J. R., New hybrid method for simultaneous improvement of tensile and impact properties of carbon fibre reinforced composites, Carbon, Vol. 49, pp. 5329-5338, 2011.
• [7] Kucharczyk, W., Kształtowanie ablacyjnych właściwości termoochronnych polimerowych kompozytów proszkowych, Kompozyty, Vol. 8-3, pp. 274-279, 2008.
• [8] Kucharczyk, W., Mazurkiewicz, A., Żurowski, W., Nowoczesne materiały konstrukcyjne wybrane zagadnienia, wydanie II, Politechnika Radomska, Radom 2010.
• [9] Przybyłek, P., Opara, T., Kucharczyk, W., Możliwości zwiększenia odporności cieplnej rejestratorów lotniczych poprzez zastosowanie osłon z polimerowych kompozytów ablacyjnych, Journal of Aeronautica Integra, Vol. 2, (9), pp. 50-56, 2011.
• [10] Sanoj, P., Kandasubramanian, B., Hybrid Carbon-Carbon Ablative Composites for Thermal Protection in Aerospace, Journal of Composites, 2014.
• [11] Suresha, B., Ramesh, B. N., Subbaya, K. M., Kumar, B. N. R., Chandramohan, G., Influence of graphite filler on two-body abrasive wear behaviour of carbon fabric reinforced epoxy composites, Materials and Design, Vol. 31, pp. 1833-1841, 2010.
• [12] Zhang, J., Chaisombat, K., He, S., Wang, C. H., Hybrid composite laminates reinforced with glass/carbon woven fabrics for lightweight load bearing structures, Materials and Design, Vol. 36, pp. 75-80, 2012.
• [13] Zhou, S., Zhang, Q., Wua, C., Huang, J., Effect of carbon fibre reinforcement on the mechanical and tribological properties of polyamide6/polyphenylene sulfide composites, Materials and Design, Vol. 44, pp 493-499, 2013.

Uwagi

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2018).