PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Evaluation of Force-Time Changes During Impact of Hybrid Laminates Made of Titanium and Fibrous Composite

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Fibre metal laminates (FML) are the modern hybrid materials with potential wide range of applications in aerospace technology due to their excellent mechanical properties (particularly fatigue strength, resistance to impacts) and also excellent corrosion resistance. The study describes the resistance to low velocity impacts in Ti/CFRP laminates. Tested laminates were produced in autoclave process. The laminates were characterized in terms of their response to impacts in specified energy range (5J, 10J, 20J). The tests were performed in accordance with ASTM D7137 standard. The laminates were subjected to impacts by means of hemispherical impactor with diameter of 12,7 mm. The following values have been determined: impact force vs. time, maximum force and the force at which the material destruction process commences (Pi). It has been found that fibre titanium laminates are characterized by high resistance to impacts. This feature is associated with elasto-plastic properties of metal and high rigidity of epoxy - fibre composite. It has been observed that Ti/CFRP laminates are characterized by more instable force during impact in stage of stabilization of impactor-laminate system and stage of force growth that glass fibre laminates. It has been observed more stable force decrease in stage of stress relaxation and withdrawal of the impactor. In energy range under test, the laminates based on titanium with glass and carbon fibres reinforcement demonstrate similar and high resistance to low-velocity impact, measured by means of failure initiation force and impact maximum force.
Słowa kluczowe
Twórcy
autor
  • Department of Materials Engineering, Faculty of Mechanical Engineering, Lublin University of Technology, Nadbystrzycka 36, 20-618 Lublin, Poland
autor
  • Department of Materials Engineering, Faculty of Mechanical Engineering, Lublin University of Technology, Nadbystrzycka 36, 20-618 Lublin, Poland
autor
  • Department of Materials Engineering, Faculty of Mechanical Engineering, Lublin University of Technology, Nadbystrzycka 36, 20-618 Lublin, Poland
Bibliografia
  • [1] A. Vlot, J.W. Gunnink, Fiber Metal Laminates, Kluwer Academic Publishers, Dordrecht 2001.
  • [2] L. B. Vogelesang, A. Vlot, J Mater Process Tech. 103(1), 1-5 (2000).
  • [3] J. Bienias, Compos Theory and Practice 11 (1), 39-43 (2011).
  • [4] E. C. Botelho, R. A. Silva, L. C. Pardini, M. C. Rezende, Mater Res. 9 (3), 247-256 (2006).
  • [5] W. X. Wang, Y. Takao, T. Matsubara, 8 - 13 July 2007, Kyoto 2007.
  • [6] J. Bienias, B. Surowska, P. Jakubczak, Polym Compos, 1-8 (2014), DOI: 10.1002/pc.23266 (in press).
  • [7] P. Jakubczak, J., J. Bienias, K., Majerski, M., Ostapiuk, B. Surowska, Aircr Eng Aerosp Tec. 4(86), 287-294 (2014).
  • [8] B. Surowska, Inżynieria Materiałowa 5, 404-407 (2009).
  • [9] P. Molitor, V. Barron, T. Young, Int J Adhes Adhes. 21 (2), 129-136 (2001).
  • [10] J. Bienias, P. Jakubczak, Inżynieria Materiałowa 4, 307-310 (2012).
  • [11] ASTM D7136. Standard test method for Measuring the Damage Resistance of a Fiber-Reinforced-Polymer matrix Composites to a Drop-Weight Impact event, Book of Standards 15, 03, 2006.
  • [12] G. Caprino, G. Spatarob, S. Del Luongo, Compos Part A. 35, 605-616 (2004).
  • [13] http://www.iccm-central.org/Proceedings/ICCM12proceedings/site/papers/pap421.pdf.
  • [14] Z. Guan, C. Yang, J Compos Mater. 36, 851-871 (2002).
  • [15] G.B. Chai, P. Manikandan, Compos Struct. 107, 363-381 (2014).
  • [16] H. Nakatani, T. Kosaka, K. Osaka, Y. Sawada, Compos Part A. 42, 772-781 (2011).
  • [17] S. Bernhardt, M. Ramulu, A.S. Kobayashi, J Eng Mat and Tech. 129, 220-226 (2007).
  • [18] J. Bienias, Compos Theory and Practice. 11 (1). 39-43 (2011).
  • [19] J. Bienias, A. Gliszczynski, P. Jakubczak, T. Kubiak, K. Majerski, Thin Wall Struct. 85, 262-270 (2014).
  • [20] Y. X. Liu, B. M. Liaw, Costa Mesa 2004.
  • [21] M. A. Ardakani, A. A. Khatibi, H. Parsaiyan, ICCM17 Proceedings, Edinburgh 2009.
  • [22] B. M. Liaw, Y.X. Liu, E.A. Villars, Portland (2001).
  • [23] M. O. W. Richardson, M. J. Wisheart, Compos Part A. 27, 1123-1131 (1996).
  • [24] G. D. Lawcock, L. Ye, Y. W. Mai, C.T. Sun, Compos Sci Technol. 57, 1621-1628 (1997).
  • [25] J. Bienias, P. Jakubczak, B. Surowska, K. Dragan, Arch Civ Mech Eng. 15 (4), 925-932 (2015).
  • [26] K. Majerski, B. Surowska, J. Bienias, P. Jakubczak, M. Ostapiuk, Aircr Eng Aerosp Tec. 4(86), 307-311 (2014).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-f898363f-aa89-4e96-a18f-4be3a24330d5
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.