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Comparison finite element analysis on duralium strength against multistage artificial aging process

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Języki publikacji
EN
Abstrakty
EN
Purpose: To analyze and estimate the strength of duralium rivets which had been treated by using multistage artificial aging compared with duralium that had not been treated. This processwas necessary to be conducted in riveting process effectively. Duralium has been widely used in aerospace industry, one of duralium usage in aerospace industry is aircraft fittings such as rivet. Riveting is one of method that used for joining airframe structural components. During riveting process, the load transfer causing stress that led to the fatigue. Riveting process also causes deformation on the rivet and sheet metal. Deformation that occurs on the rivet will affect the performance of rivet structure. Thus, duralium rivet was analyzed its total deformation, shear stress, and its equivalent stress Von Misses. Design/methodology/approach: that used in this study was finite element analysis. Geometry of rivet that used in this study was drawn by using Autodesk Inventor Professional 2018. While total deformation, shear stress and equivalent stress Von Mises on duralium rivets were found out by using ANSYS Workbench 18.1. Findings: Comparison result was obtained between duralium rivet with and without treatment of multistage artificial aging. The result shown that total deformation, shear stress and equivalent stress Von Mises which obtained by duralium rivet with multistage artificial aging had the lower value than duralium rivet without multistage artificial aging. Duralium rivet with multistage artificial aging could be used as aircraft fitting which had the higher strength. Research limitations/implications: Direct experiment on duralium rivet had not been done yet, this study only did simulation based on data that obtained form previous research that had been conducted by the researcher. Practical implications: Duralium rivet with multistage artificial aging had lower value on total deformation, shear stress, and equivalent stress Von Misses, thus duralium rivet with multistage aritificial aging had a higher strength. Originality/value: Application of duralium as a rivet with treatment of multistage artificial aging.
Rocznik
Strony
29--34
Opis fizyczny
Bibliogr. 20 poz.
Twórcy
autor
  • Department of Mechanical Engineering, Faculty of Engineering, University of Merdeka Malang, Jalan Terusan Raya Dieng 62-64, Malang, East Java, 64146, Indonesia
Bibliografia
  • [1] P.D. Merica, R.G. Waltenberg, H. Scott, Heat treatment of Duralumin, Scientific Papers of the Bureau of Standards 15 (1919) 271-315.
  • [2] S. Coriell, Precipitation Hardening of Metal Alloys, in: A Century of Excellence in Measurements, Standards, and Technology, D.R. Lide (ed.), National Institute of Standards and Technology, 2002, 14-15.
  • [3] I. Polmear, Aluminium Alloys ‒ A Century of Age Hardening, Materials Forum 28 (2004) 1-14.
  • [4] H. Tsukamoto, Impact compressive behavior of deep-drawn cups consisting of aluminum/duralumin multi-layered graded structures, Materials Science and Engineering B 198 (2015) 25-34. DOI: https://doi.org/10.1016/j.mseb.2015.04.002
  • [5] N. Eswara Prasad, R.J.H. Wanhill (eds.), Aerospace Materials and Material Technologies, Springer, Singapore, 2017. DOI: https://doi.org/10.1007/978- 981-10-2143-5
  • [6] E. Ghassemieh, Materials in Automotive Application, State of the Art and Prospects, in: M. Chiaberge (ed.), New Trends and Developments in Automotive Industry, IntechOpen, Rjeka, 2011, 365-394. DOI: https://doi.org/10.5772/13286
  • [7] D.I. Tsamroh, P. Puspitasari, Andoko, M.I.N. Sasongko, C. Yazirin, Comparison study on mechanical properties single step and three step artificial aging on duralium, AIP Conference Proceedings 1887/1 (2017) 020070. DOI: https://doi.org/10.1063/1.5003553
  • [8] P. Puspitasari, D. Izza, Duralium Behavior in Multistage, Nanoscience and Technology: An International Journal 8/3 (2017) 223-230. DOI: https://doi.org/10.1615/NanoSciTechnolIntJ.v8.i3.50
  • [9] A. Zulfia, R. Juwita, A. Uliana, I. Nyoman Jujur, J. Raharjo, Proses Penuaan (Aging) pada Paduan Aluminium AA 333 Hasil Proses Sand Casting, Jurnal Teknik Mesin 12/1 (2010) 13-20. DOI: https://doi.org/10.9744/jtm.12.1.13-20
  • [10] M. Stoicănescu, M. Smeadă, V. Geamăn, I. Radomir, The Influence of Work Parameters about the Heat Treatment Applied to AlCu4Mg1,5Mn - Aluminum Alloy, Procedia ‒ Social and Behavioral Sciences 62 (2012) 886-890. DOI: https://doi.org/10.1016/j.sbspro.2012.09.149
  • [11] R. Ranganatha, V. Anil Kumar, V.S. Nandi, R.R. Bhat, B.K. Muralidhara, Multi-stage heat treatment of aluminum alloy AA7049, Transactions of Nonferrous Metals Society of China 23/6 (2013) 1570-1575. DOI: https://doi.org/10.1016/S1003-6326(13)62632-1
  • [12] D.I. Tsamroh, P. Puspitasari, A.A. Permanasari, P.E. Setyawan, Optimization of multistage artificial aging parameters on Al-Cu alloy mechanical properties, Journal of Achievements in Materials and Manufacturing Engineering 87/2 (2018) 62-67. DOI: https://doi.org/10.5604/01.3001.0012.2828
  • [13] ASM, Aluminum 2024-T6, 2000.
  • [14] C. Lei, Y. Bi, J. Li, Y. Ke, Effect of riveting parameters on the quality of riveted aircraft structures with slug rivet, Advances in Mechanical Engineering 9/11 (2017) (published online). DOI: https://doi.org/10.1177/1687814017734710
  • [15] C. Rans, P.V. Straznicky, R. Alderliesten, Riveting Process Induced Residual Stresses Around Solid Rivets in Mechanical Joints, Journal of Aircraft 44/1 (2007) 323-329. DOI: https://doi.org/10.2514/1.23684
  • [16] K. Zhang, H. Cheng, Y. Li, Riveting process modeling and simulating for deformation analysis of aircraft’s thin-walled sheet-metal parts, Chinese Journal of Aeronautics 24/3 (2011) 369-377. DOI: https://doi.org/10.1016/S1000-9361(11)60044-7
  • [17] H. Junkers, Duralumin and the Origins of Rivets, 2014.
  • [18] Y. Zhang, Q. Bi, L. Yu, Y. Wang, Online compensation of force-induced deformation for high-precision riveting machine based on force–displacement data analysis, The International Journal of Advanced Manufacturing Technology 94/1-4 (2018) 941-956. DOI: https://doi.org/10.1007/s00170-017-0945-2
  • [19] M. Ramachandran, N. Agarwal, Identification of Most Affected Parameter for Design for Remanufacturing of Scrap Piston by Taguchi Desirability Function Analysis, in: A. Gruca, T. Czachórski, K. Harezlak, S. Kozielski, A. Piotrowska (eds.), Man-Machine Interac-tions 5. ICMMI 2017. Advances in Intelligent Systems and Computing, vol 659. Springer, Cham, 2017. DOI: https://doi.org/10.1007/978-3-319-67792-7_32
  • [20] H. Syaifuddin, Analisis Tegangan Von Mises Pegas Daun Mobil Listrik Angkutan Massal Menggunakan Metode Elemen Hingga, MSc Thesis, Universitas Negeri Semarang, 2015.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-38b8ea15-3aea-4f2e-accf-4b082a7cc304
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