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The article presents impact tests carried out for the elements of a tailplane. The author describes the experiments in which a head-on and an off-centre collision of a bird-imitating object with the leading edge of the tailplane were recreated. The tests were performed with the use of an impact system with a projectile thrower in form of a 250 mm pneumatic gun. Objects made of gelatine and imitating birds were used in the tests. The collision was recorded by two high-speed cameras positioned at different angles to the axis of movement of a thrown projectile. The article presents the test system, test procedures and the results of the experiments available in form of a recorded image of the collision. Additionally, the effects the head-on and off-centre collisions have on the tested aircraft structures are shown.
Słowa kluczowe
Czasopismo
Rocznik
Tom
Strony
53--60
Opis fizyczny
Bibliogr. 50 poz., rys.
Twórcy
autor
- Institute for Sustainable Technologies – National Research Institute, ul. Pułaskiego 6/10, 26-600 Radom, Poland
Bibliografia
- [1] R. Dolbeeretal., Wildlife strikes to civil air craft in the United States 1990–2009. Report of the associate administrator for airports, office of airport safety and standards airport safety & certification. Federal Aviation Administration, No. 16, Washington, DC May 2011.
- [2] J. Thorpe, Update on fatalities and destroyed civil air craft due to bird strike swith appendix for 2006–2008, in: Proceedings of the Bird Strike Committee, Brasilia, Brazil, November 2008.
- [3] Transport Canada: Sharing the skies, An Aviation Industry Guide to the Management of Wildlife Hazard, 2004, isbn: 0-662-36555-0.
- [4] T. De Vault, J. Kubel, D. Glista, O. Rhodes, Mammalian hazards at small airport sin Indiana: impact of perimeter fencing, Human-Wildlife Conflicts 2 (2) (2008) 240–247.
- [5] W. Richardson, T. West: Serious birdstrike accidents to U.K. military aircraft, 1923–2004: Number sand circumstances, in: Proceedings of the Bird Strike Committee, Athens, May 2005.
- [6] J. Thorpe, Fatalities and destroyed civilair craft duet o bird strikes 1912–2002, in: Proceedings of the Bird Strike Committee, Warsaw, Poland, May 2003.
- [7] H. Kim, D. Welch, K. Kedward, Experimental investigation of high velocity ice impact son woven carbon/epoxycomposite panels, Composites Part A Applied Science and Manufacturing 34 (1) (2003) 25–41.
- [8] R. Olsson, R. Juntikka, L.E. Asp, High velocity hailimpact on composite laminates – modelling and testing. In: Solid Mechanics and Its Applications. Dynamic Failure of Composite and Sandwich Structures, S. Abrate, B. Castanie, Y. Rayapakse (Eds.), Springer, Dordrecht, Heidelberg, New York, London, pp. 393-425. http://dx.doi.org/10.1007/978-94-007-5329-7. ISBN 978-94-007-5328-8.
- [9] H. Park, H. Kim, Damage resistance of single lap adhesive composite joints by transverse ice impact, International Journal of Impact Engineering 37 (2010) 177–184.
- [10] L. Asp, R. Juntikka, High velocity impact on NC Frein forced composites, Composites Science and Technology 69 (9) (2009) 1478–1482.
- [11] G. Davies, R. Olsson, Impast on composite structures, The Aeronautical Journal of the Royal Aeronautical Society (2004) 541–563.
- [12] S. Heimbs, T. Bergmann, High-velocity impact behaviour of prestressed composite plates under bird strike loading, International Journal of Aerospace Engineering (2012) 1–11.
- [13] A. Komorek, P. Przybyłek, Examination of the influence of cross-impact load on bend strength properties of composite materials, used in aviation, Eksploatacja i Niezawodnosc – Maintenance and Reliability (2012/4) 265–269.
- [14] Bird Strikemage & Windshield Bird Strike Final Report. European Aviation Safety Agency 2009.
- [15] E. Klich, Bezpieczeństwo lotów. Wydawnictwo Naukowe Instytutu Technologii Eksploatacji – PIB, Radom, 2011, isbn: 978-83-7789-024-0.
- [16] A. Zbrowski, Bezpieczeństwo samolotów w aspekcie zagrożenia kolizją z ptakami, Problemy Eksploatacji 2 (2012) 215–228.
- [17] A. Airoldi, B. Cacchione, Modelling of impact forces and pressures in Lagrangian bird strike analyses, International Journal of Impact Engineering 32 (10) (2006) 1651–1677.
- [18] S. Georgiadis, A. Gunnion, R. Thomson, B. Cartwright, Bird-strike simulation for certification of the Boeing 787 composite moveable trailingedge, Composite Structures 86 (1–3) (2008) 258–268.
- [19] S. Heimbs, Bird Strike Simulations on Composite Aircraft Structures, in: Proceedings of the SIMULIA Customer Conference, Barcelona, Spain, May 17–19, 2011, pp.73–86.
- [20] A. Bełzowski, Z. Rechul, J. Stasieńko, Uszkodzenia udarowe w laminacie wzmocnionym tkaniną szklaną, Kompozyty (Composites) 2 (2002) 394–399 (5).
- [21] M. Lavoie, A. Gakwaya, M. Nejad Ensan, D. Zimcik, D. Nandlallc, Bird's substitute tests results and evaluation of available numerical methods, International Journal of Impact Engineering 36 (2009) 1276–1287.
- [22] M. Pinnell, P. Sjoblom, Low-velocity impact testing of thermoplastic and thermo set matrix composite materials. Technical report AD-A236092. Materiale Labradory Wright Research and Development Center, November 1990.
- [23] C. Akin, M. Şenel, An experiment al study of low velocity impact response for composite laminated plates, Journal of the Institute of Science & Technology of Dumlupinar (21) (2010) 77–90.
- [24] J. Duell, Impact Testing of Advanced Composites, in: M. Kessler (Eds.), Advanced Topic sin the Characterization of Composites, pp. 97–112.
- [25] J. Tarpani, O. Maluf, M. Gatti, Charpy impact toughness of conventional and advanced composite laminates for air craft construction, Materials Research 12 (4) (2009) 395–403.
- [26] W. Jóźwik, A. Zbrowski, Determination of the shotenergy characteristics of the pneumatic gun by means of high speed imaging method, Solid State Phenomena. Mechatronic Systems and Materials V (2013) 291–296.
- [27] A. Zbrowski, T. Samborski, S. Zacharski, Badania odporności zderzeniowej szybkich środków transportu z małymi obiektami, Pomiary Automatyka Robotyka PAR 11 (2012) 59–67.
- [28] J. Barber, H. Taylor, J. Wilbeck Bird impact forces and pressures on rigid and compliant targets, Technical report AFFDL-TR-77-60, Air Force Flight Dynamics Lab, May 1978.
- [29] J. Barber, H. Taylor, J. Wilbeck, Characterization of bird impacts on rigid plate, Technical report AFFDL-TR-75-5, Air Force Flight Dynamics Lab, January 1975.
- [30] S. James J. Wilbeck Impact Behavior of Low Strength Projectile, Technical report AFML-TR-77-134, Air Force Flight Dynamics Lab, July 1978.
- [31] A. Grimaldi, A. Sollo, M. Guida, F. Marulo, Parametric study of a SPH high velocity impact analysis – a birdstrike windshield application, Composite Structures 96 (2013) 616–630.
- [32] A. Grimaldi, SPH High velocity impact analysis. Abirdstrike windshield application (Ph. D. Thesis), Aerospace Engineering, Department of Aerospace Engineering University of Naples Federico II, Naples, Italy, 13th January 2011.
- [33] F.S. Wang, Z.F. Yue, Numerical simulation of damage and failure in air craft windshield structure against bird strike, Materials & Design 31 (2) (2010) 687–695.
- [34] C.Y. Park, B.-W. Jang, J.H. Kim, C.-G. Kim, S.-M. Jun, Bird strike event monitoring in a composite UAV wing using high speed optical fiber sensing system, Composites Science and Technology 72 (4) (2012) 498–505.
- [35] M. Guida, F. Marulo, M. Meo, A. Grimaldi, G. Olivares, SPH– Lagrangian study of bird impact on leading edge wing, Composite Structures 93 (2011) 1060–1071.
- [36] M. Guida, F. Marulo, M. Meo, M. Riccio, Analysis of bird impact on a composite tailplane leadding edge, Applied Composite Materials 15 (4–6) (2008) 241–257.
- [37] A. Johnson, M. Holzapfel, Modelling soft body impact on composite structures, Composite Structures 61 (1–2) (2003) 103–113.
- [38] T. Kermanidis, G. Labeas, M. Sunaric, L. Ubels, Development and validation of a novel bird strike resistant composite leading edge structure, Applied Composite Materials 12 (6) (2005) 327–353.
- [39] M. Mc Carthy, J. Xiao, C. Mc Carthy, A. Kamoulakos, J. Ramos, J. Gallard, V. Melito, Modelling of bird strike on an air craft wing leadingedge made from fibre metal aminates – Part 2: modelling of impact with SPH bird model, Applied Composite Materials 11 (5) (2004) 317–340.
- [40] I. Smojver, D. Ivancevic, Numerical simulation of bird strike damage prediction in air plane flap structure, Composite Structures 92 (9) (2010) 2016–2026.
- [41] D. Ivancevic, I. Smojver, Hybryd approach In bird strike damage prediction on aeronautical composite structures, Composite Structures 94 (1) (2011) 15–23.
- [42] I. Smojver, D. Ivancevic, Birdstrike damage analysis in aircraft structures using Abaqus/explicit and coupled Eulerian Lagrangian approach, Composites Science and Technology 71 (4) (2011) 489–498.
- [43] J. Reglero, M. Rodríguez-Pérez, E. Solórzano, Jde Saja, Aluminium foams as a filler for leading edges: improvements in the mechanical behaviour under bird strike impact tests, Materials & Design 32 (2) (2011) 907–910.
- [44] A. Shulev, W. Van Paepegem, J. Harizanova, A. Moentjens, J. Degrieck, V. Sainov, Projection Moire measurement of the deflection of composite plates subject to bird strike impact, Optical Measurement Systems for Industrial Inspection V, PTS1 AND 2 Proceedings of SPIE, vol. 6616, 2007, pp. 2 Z1–9.
- [45] W. Van Paepegema, A. Shulev, A. Moentjens, J. Harizanova, J. Degrieck, V. Sainov, Use of projection moire for measuring the instantaneous out-of-plane deflections of composite plates subject to bird strike, Optics and Lasersin Engineering 46 (7) (2008) 527–534.
- [46] A. Zbrowski, Badania prototypu działa pneumatycznego, Problemy Eksploatacji 3 (2011) 217–234.
- [47] A. Zbrowski, A. Majcher, Mechatronic system for impact tests for aerostructures. Solid State Phenomena, Mechatronic Systems and Materials IV 198 (2013) 366–371.
- [48] A. Zbrowski, T. Samborski, S. Zacharski, The method for high-energy throwing of the object sin impact testing, TTS Technika Transportu Szynowego 9 (2012) 619–627.
- [49] A. Zbrowski, Działo pneumatyczne do testów zderzeniowych, Problemy Eksploatacji 3 (2012) 133–144.
- [50] A. Zbrowski, S. Zacharski, Urządzenie wylotowe w armacie pneumatycznej do testów konstrukcji lotniczych, TTS Technika Transportu Szynowego 9 (2012) 629–638.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-169cba10-d843-4a9d-ae20-755b2d9e0a03
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