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Analysis of the Quasi-Static Riveting Process for 90° Countersunk Rivet

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Riveting is the most commonly used method of joining sheet metal components of the aircraft structure. The riveted joints are critical areas of the aircraft structure due to severe stress concentrations and effects such as fretting and secondary bending. The most spectacular and wellknown evident of this was the accident of Boeing B737 of Aloha Airline in 1988, when during the flight at altitude of 7300 m a large part of fuselage skin was removed due to explosive decompression. The investigation showed that the reason for this accident was widespread fatigue damage of riveted joints. This accident was an impulse for establishing many research programs around the world focused on fatigue of riveted joints.
Słowa kluczowe
Rocznik
Tom
Strony
141--156
Opis fizyczny
Bibliogr. 18 poz., rys., tab., wykr.
Twórcy
autor
  • Institute of Aviation, Warsaw, Poland
autor
  • Institute of Aviation, Warsaw, Poland
Bibliografia
  • [1] Muller R.( 1995). An Experimental and Analytical Investigation on the Fatigue Behaviour of Fuselage Riveted Lap Joint. Ph.D. thesis, TU Delft, Netherlands.
  • [2] Müller R. P.G., Hart-Smith L.J.: Making fuselage riveting lap splices with 200-year crackfree fatigue life. ICAF 97` Fatigue in new and ageing aircraft. Proceedings of the 19th Symposium of the International Committee of Aeronautical Fatigue1997, Edinburgh, EMAS Publishing, pp. 499-522.
  • [3] Simenz R. F., Steinberg M. Alloy Needs and Design: the Airframe, In Fundamental Aspects of Structural Alloy Design. Proceeding of the 10th Battelle Colloquium in the Materials Science, Jaffee R. I., Wilcox B. (Ed), A, PLENUM PRESS, New York and London 1977.
  • [4] Dębski M. (1995). Metoda oceny trwałości zmęczeniowej struktur nośnych samolotów (Methods of Fatigue Life estimation of Airframes). PhD thesis, PW Warszawa, Poland.
  • [5] Kaniowski J. (1998). Badania wpływu geometrycznych cech konstrukcyjnych na trwałość zmęczeniową na przykładzie skrzydła samolotu PZL I-22 Iryda (The Study of the Influence of Geometric Features on the Fatigue Durability on the Example of the PZL I-22 IRYDA Plane Wing). PhD thesis, ATR Bydgoszcz, Poland.
  • [6] Skorupa M, Skorupa A, Michniewicz T, Korbel A. Effect of production variables on the fatigue behaviour of riveted lap joint. International Journal of Fatigue, 32 (2010), pp. 996-1003
  • [7] Wronicz W., Kaniowski J., Experimental and Numerical Study of Strain Progress During and After Riveting Process for Brazier Rivet and Rivet with Compensator - squeezing force and rivet type effect. In A. Niepokólczycki (Ed.), Fatigue of Aircraft Structures, ISSUE 2011 (pp. 165-189). Warsaw: Institute of Aviation Scientific Publication.
  • [8] Gadalińska E., Wronicz w., Kaniowski J., Korzeniewski B.: Calculation and Experimental Verification of Residual Stresses in Riveted Joints Used in an Airframe. In A. Niepokólczycki (Ed.), Fatigue of Aircraft Structures, ISSUE 2010 (pp. 23-36). Warsaw: Institute of Aviation Scientific Publication.
  • [9] Skorupa M., Skorupa A., Machniewicz T., Korbel A.: An Experimental Investigation on the Fatigue Performance of Riveted Lap Joints. ICAF2009, Bridging the Gap between Theory and Operational Practice. Proceedings of the 25th Symposium of the Int. Committee on Aeronautical Fatigue, Rotterdam, The Nederlands, 27-29 May 2009. Editor M.J. Bos, Springer, 2009, pp. 449-474.
  • [10] Szala J.(Ed.), Boroński D., Lipski A, Mroziński S. Metody doświadczalne w badaniach materiałów stosowanych na poszycia samolotów i połączeń nitowych. Wybrane zagadnienia (Experimental Methods in Test of Materials for Aircraft Skin and Riveted Joint. Selected Problems). Wydawnictwa Naukowe Instytutu Technologii i Eksploatacji - PIB w Radomiu, Radom, 2010, ISBN 978-83-7204-950-6.
  • [11] Szymczyk E., Jachimowicz J., Sławiński G., Derewońko A., Influence of technological imperfections on residual stress fields in riveted joint. Dissipation and Damage across Multiple Scales in Physical and Mechanical Systems, Oxford, United Kingdom, 2009, 1, 118, pp. 1-4.
  • [12] Papuga J. (2010). Fatigue Prediction Based on Finite Element Analysis of Riveted Joints. Czech Aerospace Proceedings, Journal For Czech Aerospace Research, No. 3,Vol. 2010, pp. 27-31.
  • [13] Fárek J. (2010). FE-Modelling Methodology of Riveted Joints. Czech Aerospace Proceedings. Journal For Czech Aerospace Research, No 2/2010, pp. 12-16.
  • [14] Langrand B., Patronelli L., Deletombe E., Markiewicz E., Drazétic P., An alternative numerical approach for full scale characterisation for riveted joint design. Aerospace Science and Technology, Vol 6, 2002, pp. 343-354.
  • [15] Li G., Shi G., Berlinger N.C., Studies of Residual Stress in Single-Row Countersunk Riveted Lap Joints. 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference 18 - 21 Apr 2005, Hyatt Regency Austin, Austin, Texas
  • [16] ASM Handbook, Volume 18, Friction, Lubrication, and Wear Technology,1995.
  • [17] Stojman I.M.: Cholodnaja svarka metallov. Mašinostrojenie,1985, pp.38 and 51.
  • [18] Sachackij G.P.: Technologia svarki metellov w cholodnom sostojanii, Naukowa Dumka 1979, p.111.
Uwagi
EN
Experimental research was carried out as part of the Eureka project E!3496 IMPERJA.
PL
Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-0f396647-eb14-46cd-a3c2-b55ea0fad687
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