Pengaruh Aditif Oksida Grafit Terhadap Kekuatan Tarik dan Panjang Terbakar Komposit Gelas/Epoksi

  • Adi Purwoko Departemen Aeronautika, Akademi Angkatan Udara, Yogyakarta
  • Hermawan Judawisastra Fakultas Teknik Mesin dan Dirgantara, Institut Teknologi Bandung
Keywords: Komposit, Oksida Grafit, Sifat Tarik, Sifat Mampu Bakar

Abstract

Komponen interior pesawat udara pada umumnya berupa komposit fenolik berpenguat serat gelas. Matriks fenolik digunakan karena sifat ketahanan api yang baik. Permasalahan resin fenolik adalah sifat bonding yang rendah. Epoksi memiliki sifat bonding tinggi dengan kemiripan sifat mekanik dengan fenolik. Namun epoksi sangat mudah terbakar. Oksida grafit telah diketahui efektif menurunkan sifat mampu bakar epoksi. Serat gelas merupakan serat penguat komposit yang paling banyak digunakan. Pada penelitian ini dilakukan pembuatan komposit serat gelas dengan matriks epoksi ditambah aditif oksida grafit. Selanjutnya dilakukan pengkajian pengaruh penambahan oksida grafit terhadap kekuatan tarik dan panjang terbakar komposit. Selain itu, dilakukan pula perbandingan kekuatan tarik dan panjang terbakar komposit dengan standar kelaikan terbang BMS 8-226 dan FAR chapter 25. Pada penelitian ini, dilakukan pengujian untuk mengetahui kekuatan tarik dan panjang terbakar komposit. Karakterisasi X-Ray Diffraction dilakukan untuk grafit dan oksida grafit. Pengujian tarik sesuai ASTM D638 dan pengujian bakar vertikal sesuai BSS 7230 dilakukan pada komposit dan material penyusunnya. Pengamatan patahan komposit dilakukan menggunakan Scanning Electron Microscopy. Hasil penelitian menunjukkan bahwa penambahan aditif oksida grafit sampai dengan 20% berat pada matriks secara umum menurunkan kekuatan tarik dan panjang terbakar komposit.

References

Ashby, M. et al. Materials Science, Processing and Design. Department of Engineering, Cambridge University, England. (2000) 37-38.

Kurnia, A.. Analisa Tegangan pada Sambungan Model Piano pada Sayap Pesawat Struktur Komposit. Tesis S2 Teknik Penerbangan ITB, Bandung. (2007) 1-2.

Astrom, B. T. Manufacturing of Polymer Composites. Edisi I. London: Chapman & Hall. (1997) 24-26.

Federal Aviation Regulations Part 25. Airworthiness Standards, Transport Category Airplane. Federal Aviation Administration. (1988) 147-148.

Boeing Materials Specification. BMS 8-226 Phenolic Resin Preimpregnated Glass Fabric For Interior Sandwich Panel Bonding Materials And Laminates. (1993) 7-20.

Joseph, P. and Ebdon J. Recent Developments in Flame Retarding Thermoplastics and Thermosets. Department of Chemistry, University of Sheffield, United Kingdom. (2001) 245-247.

Kandola, B.K. Composites. Faculty of Technology, Bolton Institute, Bolton, United Kingdom. (2001) 190-191.

Lee, Y. R. Graphite Oxides as Effective Fire Retardants of Epoxy Resin. Department of Chemistry, University of Ulsan, Ulsan 680-749, Korea. (2010) 66-69.

Perez, R. M. Effect of DOP-based compounds on fire retardancy,thermal stability, and mechanical properties of DGEBA cured with 4,4_-DD. Polymer Engineering, University of Bayreuth, Bayreuth, Germany. (2006) 162-163.

Wu, Kun. Thermal degradation and intumescent flame retardation of cellulose whisker/epoxy resin composite. Akade´miai Kiado´, Budapest, Hungary. (2011) 1-2.

Pearce, et al. Fire and Smoke-Resistant Interior Materials for Commercial Transport Aircraft. Committee on Fire and Smoke Resistant Materials for Commercial Aircraft Interiors, Commission on Engineering and Technical Systems, National Research Council. (1995) 12-16.

Matthews. Composite Materials: Science And Engineering. Imperial College of Science,Technology And Medicine, London, Chapman And Hall, United Kingdom. (1993) 12-18, 29-31, 61-63.

Holleman, A. Inorganic Chemistry . Academic Press: San Diego. (2001).

Dreyer, et al.. Chemistry of Graphene Oxide. Chemical Society Review. (2009) 2-4.

Hummer, W. et al.. Preparation of Graphitic Oxide. Baroid Division, National Lead Company USA. (1958)

Kandola, B. et al. Composites. Faculty of Technology, Bolton Institute, United Kingdom. (2001) 182-200.

Price, D. et al. Introduction: polymer combustion, condensed phase pyrolysis and smoke formation. Fire Chemistry Research Group, School of Sciences, University of Salford, Salford, UK. (1998) 6-10.

Callister. W. Materials Science And Engineering: an Introduction. Department of Metallurgical Engineering, The University of Utah, United States. (2007) A8-A14

Smith, D.K, Introduction to Diffraction Methods. ASM Metals Handbook Volume 10 ASM International. (1992) pp 662-674.

Darwent, B. Bond, Dissociation Energies in Simple Molecules. Department of Chemistry, The Catholic University of America, Washington D.C., United States. (1970) 18-23.

Fabiano, I, Analisis Kekuatan Komposit Epoksi-Serat Gelas Dengan Variasi Preform dan Metode Manufaktur. Tugas Akhir Sarjana Program Studi Teknik Material, FTMD ITB. 6-10, 15-17, 20-22.
Published
2021-03-09
How to Cite
Purwoko, A., & Judawisastra, H. (2021). Pengaruh Aditif Oksida Grafit Terhadap Kekuatan Tarik dan Panjang Terbakar Komposit Gelas/Epoksi. Akademi Angkatan Udara Journal of Defense Science and Technology : AAU-JDST, 7(1), 9-22. Retrieved from https://aau.e-journal.id/jdst/article/view/66
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