The Numerical Simulation of Aviation Structure Joined by FSW

• Autorzy: Lacki P. , Adamus K. , Winowiecka J.

Identyfikatory

DOI

10.24425/amm.2019.126264

• Języki publikacji: EN

Abstrakty

EN

This work presents a numerical simulation of aviation structure joined by friction stir welding, FSW, process. The numerical simulation of aviation structure joined by FSW was created. The simulation uses thermomechanical coupled formulation. The model required creation of finite elements representing sheets, stiffeners and welds, definition of material models and boundary conditions. The thermal model took into account heat conduction and convection assigned to appropriate elements of the structure. Time functions were applied to the description of a heat source movement. The numerical model included the stage of welding and the stage of releasing clamps. The output of the simulation are residual stresses and deformations occurring in the panel. Parameters of the global model (the panel model) were selected based on the local model (the single joint model), the experimental verification of the local model using the single joint and the geometry of the panel joints.

Słowa kluczowe

EN

aviation structure; friction stir welding; FSW; thermo-mechanical simulation; FEM

• Wydawca: Institute of Metallurgy and Materials Science of Polish Academy of Sciences ; Committee of Materials Engineering and Metallurgy of Polish Academy of Sciences
• Czasopismo: Archives of Metallurgy and Materials
• Rocznik: 2019
• Tom: Vol. 64, iss. 1
• Strony: 387--392
• Opis fizyczny: Bibliogr. 24 poz., fot., rys., tab.

Twórcy

autor

Lacki P.

• Czestochowa University of Technology, 69 Dabrowskiego Str., 42-201 Częstochowa, Poland

autor

Adamus K.

• Czestochowa University of Technology, 69 Dabrowskiego Str., 42-201 Częstochowa, Poland

autor

Winowiecka J.

• Czestochowa University of Technology, 69 Dabrowskiego Str., 42-201 Częstochowa, Poland

Bibliografia

• [1] K. Hemmesi, M. Farajian, M. Boin, Mater Design 126, 339-350 (2017).
• [2] D. F. Almeida, R. F. Martins, J. B. Cardoso, Procedia Struct. Integrity 5, 633-639 (2017).
• [3] M. Dal, R. Fabbro, Opt. Laser Technol. 78, 2-14 (2016).
• [4] H. Huang, S. Tsutsumi, J. Wang, L. Li, H. Murakawa, Finite Elem. Anal. Des. 135, 1-10 (2017).
• [5] A. Kouadri-Henni, C. Seang, B. Malard, V. Klosek, Materials & Design 123, 89-102 (2017), DOI: 10.1016/j.matdes.2017.03.022.
• [6] L. Xiu, J. Wu, Z. Liu, J. Ma, X. Fan, H. Ji, X. Xia, Y. Li, Fusion Eng. Des. 121, 43-49 (2017), DOI: 10.1016/j.fusengdes.2017.03.175.
• [7] N. Ma, J. Wang, Y. Okumoto, Int. J. Adv. Manuf. Technol. 41, 4, 20 (2015), DOI: 10.1007/s00170-015-7810-y.
• [8] S. Shroff, E. Acar, C. Kassapoglou, Thin Wall Struct. 119, 235-246 (2017), DOI: 10.1016/j.tws.2017.06.006.
• [9] M. C. Simmons, G. K. Schleyer, Thin Wall Struct. 44, 5, 496-506 (2006), DOI: 10.1016/j.tws.2006.05.002.
• [10] A. Singh, F. Yang, R. Sedaghati, Engineering Structures 159, 99-109 (2018), DOI: 10.1016/j.engstruct.2017.12.040.
• [11] B. Keshtegar, P. Hao, Y. Wang, Q. Hu, Appl. Soft Comput 66, 196-207 (2018).
• [12] J. F. Caseiro, R.A.F. Valente, A. Andrade-Campos, J. W. Yoon, International Journal of Mechanical Sciences 76, 49-59 (2013), DOI: 10.1016/j.ijmecsci.2013.09.002.
• [13] J. W. Yoon, G. H. Bray, R.A.F. Valente, T.E.R. Childs, Thin Wall Struct. 47, 12, 1608-1622 (2009), DOI: 10.1016/j.tws.2009.05.003.
• [14] A. Derlatka, P. Kasza, Advanced Materials Research 1020, 151-157 (2014), DOI: 10.4028/www.scientific.net/AMR.1020.151.
• [15] A. Derlatka, K. Kudła, K. Makles, Numerical analysis of RFSSW joints. in: E. Oñate, X. Oliver, A. Huerta (Eds.), 11th World Congress on Computational Mechanics (WCCM XI), Barcelona (2014).
• [16] P. Lacki, A. Derlatka, Composite Structures 159, 491-497 (2017), DOI: 10.1016/j.compstruct.2016.10.003.
• [17] A. Derlatka, P. Kasza, Advanced Materials Research 1020, 158-164 (2014), DOI: 10.4028/www.scientific.net/AMR.1020.158.
• [18] P. Lacki, A. Derlatka, Composite Structures 202, 201-209 (2018), DOI: 10.1016/j.compstruct.2018.01.050.
• [19] Q. Shao, Y. He, T. Zhang, L. Wu, Chin. J. Mech. Eng. 27, 4, 761-767 (2014), DOI: 10.3901/CJME.2014.0507.087.
• [20] D. Deng, H. Murakawa, Computational Materials Science 43, 4, 591-607 (2008), DOI: 10.1016/j.commatsci.2008.01.003.
• [21] A. Murphy, W. McCune, D. Quinn, M. Price, Thin Wall Struct. 45, 3, 339-351 (2007), DOI: 10.1016/j.tws.2007.02.007.
• [22] D.-Y. Yan, A.-P. Wu, J. Silvanus, Q.-Y. Shi, Materials & Design 32, 4, 2284-2291 (2011), DOI: 10.1016/j.matdes.2010.11.032.
• [23] R.M.F. Paulo, P. Carlone, V. Paradiso, R.A.F. Valente, F. Teixeira-Dias, Thin-Walled Structures 120, 297-306 (2017), DOI: 10.1016/j.tws.2017.09.009.
• [24] Q.-Y. Shi, J. Silvanus, Y. Liu, D.-Y. Yan, H.-K. Li, Science and Technology of Welding and Joining 13, 5, 472-478 (2013), DOI: 10.1179/174329308X341924.

Uwagi

EN

1. Financial support of The National Centre for Research and Development, European Union, PZL Mielec / a Sikorsky Company, in the framework of European Regional Development Fund Project „Advanced techniques for the fabrication of airframe structures using innovative friction stir welding (FSW) technology”, no. INNOLOT/I/4/NCBR/2013 is gratefully acknowledged.

PL

2. Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2019).