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In the modern aerospace industry, a steady increase in the share of composite materials is recorded every single year. Polymer layer composites seem to be the ones that are used most commonly in aviation. There are multiple methods of producing this type of materials, of which the most commonly used methods are as follows: the infusion method, the negative pressure bag method and the hydraulic press method. The infusion process makes it possible to obtain composites with the best mechanical properties. In the infusion process, the mould is pre-prepared (together with the reinforcement made of the material from which the composite is made, e.g. carbon fibre), which is tightly closed in a negative pressure bag, and the equipment supplying the previously mixed resin with hardener is connected to the injection points. The negative pressure generated by the negative pressure pump in the mould prepared in this way (negative pressure bag) makes the previously prepared resin seep through the reinforcement material. Various negative pressure levels can be used. This work describes the effect of the applied negative pressure level on the obtained mechanical properties of a composite reinforced with carbon fibres. It appears that the best visual properties of the composite material are obtained with the use of indirect (optimal) negative pressure but the best strength properties with the use of maximal negative pressure.
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Tom
Strony
217--227
Opis fizyczny
Bibliogr. 21 poz., fig.
Twórcy
autor
- Polish Air Force University, ul. Dywizjonu 303 no. 35, 08-521 Dęblin, Poland
autor
- Polish Air Force University, ul. Dywizjonu 303 no. 35, 08-521 Dęblin, Poland
autor
- Polish Air Force University, ul. Dywizjonu 303 no. 35, 08-521 Dęblin, Poland
autor
- Polish Air Force University, ul. Dywizjonu 303 no. 35, 08-521 Dęblin, Poland
autor
- Polish Air Force University, ul. Dywizjonu 303 no. 35, 08-521 Dęblin, Poland
Bibliografia
- 1. Boczkowska A., Krzesiński G.: Kompozyty i techniki ich wytwarzania, Oficyna Wydawnicza Politechniki Warszawskiej, Warszawa 2016.
- 2. Krzyżak, A., Mazur, M., Gajewski, M., Drozd, K., Komorek, A., & Przybyłek, P. (2016). Sandwich structured composites for aeronautics: methods of manufacturing affecting some mechanical properties. International Journal of Aerospace Engineering, 2016
- 3. Godzimirski J., Materiały lotnicze, WAT, Warszawa 2008.
- 4. Staszewski W., Boller Ch., Tomlinson G.: Health Monitoring of Aerospace Structures. John Willey & Sons, Ltd, 2004.
- 5. Boczkowska A, Kapuściński J., Puciłkowski K., Wojciechowski S: Kompozyty, Oficyna Wydawnicza Politechniki Warszawskiej, Warszawa 2000.
- 6. Ochelski S., Metody doświadczalne mechaniki kompozytów konstrukcyjnych, Wydawnictwa Naukowo-Techniczne, Warszawa 2004.
- 7. Konsztowicz K., Kompozyty wzmacniane włóknami. Podstawy technologii, Wydawnictwo AGH, Kraków 1986.
- 8. Heng H., Belouettar S., Potier-Ferry M.. Review and assessment of various theories for modeling sandwich composites. Composite Structures 84.3 (2008).
- 9. Goraj Z. Struktury kompozytowe w lotnictwie. Prace Naukowe Politechniki Warszawskiej. Mechanika 219 (2007).
- 10. Seneńko K.. Badanie właściwości lotniczych struktur kompozytowych. Diss. Instytut Techniki Lotniczej i Mechaniki Stosowanej, 2010.
- 11. Karpowicz A.S. Metody wytwarzania kompozytowych struktur płatowca. Diss. Instytut Techniki Lotniczej i Mechaniki Stosowanej, 2016.
- 12. Popham, N. Resin infusion for the manufacture of large composite structures. In Marine Composites: Design and Performance; Pemberton, R., Summerscales, J., Graham-Jones, J., Eds.; Woodhead Publishing: Amsterdam, The Netherlands, 2019.
- 13. Lunn, P. Cost-effective resin infusion. Reinf. Plast. 2009.
- 14. Mehdikhani, M.; Gorbatikh, L.; Verpoest, I.; Lomov, S.V. Voids in fiber-reinforced polymer composites: A review on their formation, characteristics, and effects on mechanical performance. J. Compos. Mater. 2019.
- 15. Correia, N.; Robitaille, F.; Long, A.; Rudd, C.; Šimáček, P.; Advani, S. Analysis of the negative pressure infusion moulding process: I. Analytical formulation. Compos. Part A Appl. Sci. Manuf. 2005.
- 16. Hashim, N., Majid, D.L.A., Baitab, D.M., Yidris, N., Zahari, R. Tensile Properties of Woven Intra-Ply Carbon/Kevlar Reinforced Epoxy Hybrid Composite at Sub-Ambient Temperature, in: Encyclopedia of Materials: Composites, ed. Dermot Brabazon, Elsevier. 2019.
- 17. Markuszewski D, Wądołowski M, Gorzym M, Bielak M. Concept of a Composite Frame of a Martian Vehicle. Advances in Science and Technology Research Journal. 2021;15(4):222-230. doi:10.12913/22998624/141213.
- 18. Juan, J.; Silva, A.; Tornero, J.A.; Gámez, J.; Salán, N. Void Content Minimization in Vacuum Infusion (VI) via Effective Degassing. Polymers 2021, 13, 2876. https://doi.org/10.3390/polym13172876
- 19. Mohd Khairul Anuar Bin Zainal Abidin, Mohd Khairul Anuar (2010) The Effect of Resin Viscosity in Vacuum Infusion Process. Universiti Teknologi PETRONAS.
- 20. Święch, Ł.; Kołodziejczyk, R.; Stącel, N. Experimental Analysis of Perimeter Shear Strength of Composite Sandwich Structures. Materials 2021, 14, 12. https://doi.org/10.3390/ma14010012
- 21. Shevtsov S., Zhilyaev I., Chang SH, Wu JK, Huang JP, Snezhina N., Experimental and Numerical Study of Vacuum Resin Infusion for Thin-Walled Comosite Parts. Applied. Sciences. 2020, 10(4), 1485; https://doi.org/10.3390/app10041485
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2024).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-16ad6310-8152-48ee-b664-e246c785929b