The Analysis of the Influence of Riveting Parameters Specified in Selected Riveting Instructions on Residual Stresses

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The riveting parameters strongly affect residual stresses induced during riveting, which in turn have an impact on the fatigue life of riveted joints. Since rivets are established as critical from the fatigue point of view, the fatigue life of riveted joints often determines the life of the whole structure.

The authors were able to become acquainted with three riveting instructions (process specifications) used by the aerospace companies from western Europe. This work presents the analysis of the riveting parameters' influence on residual stresses around the rivets. The impact of the clearance between a rivet shank and a hole as well as driven head dimensions and a rivet length were investigated based on the numerical simulations. The aim of the analysis was to determine the range of stresses variation when the requirements of the riveting instructions are fulfilled. For the purposes of comparison, the calculations were performed also with the parameters as specified in the Polish industry standards. For all calculations, the geometry of the universal rivet MS20470 was used.

The results show that residual stresses can vary strongly depending on the parameters in the instructions and standard requirements.

1. Muller R.P.G., Hart-Smith L.J., Making fuselage riveted lap splices with 200-year crack-free fatigue lives, ICAF 97: Fatigue in New and Ageing Aircraft, Vols I and Ii: Vol I: Lecture Papers, Vol Ii: Poster Papers, (1997) 499-522.

2. Skorupa M., Skorupa A., Machniewicz T., Korbel A., Effect of production variables on the fatigue behaviour of riveted lap joints, International Journal of Fatigue, 32 (2010) 996-1003.

3. Muller R., „An Experimental and Analytical Investigation on the Fatigue Behaviour of Fuselage Riveted Lap Joint”, Ph.D. thesis, TU Delft, Netherlands, 1995.

4. Rans C. D. The Role of Rivet Installation on the Fatigue Performance of Riveted Lap Joints. PhD thesis, Carleton University Ottawa, Ontario, Canada, 2007.

5. Szymczyk E., Numeryczna analiza lokalnych zjawisk fizycznych w połączeniach nitowych konstrukcji lotniczych (in Polish, Numerical analysis of local physical phenomena in riveted joints used in aerospace structures). Wyd. WAT, 2013, ISBN 978-83-62954-70-4

6. Kaniowski J. Comparision of Selected Rivets and Riveting Instructions. Fatigue of Aircraft Structures Monographic Series A. Niepokólczycki (Ed.), Institute of Aviation Scientific Publication, ISSUE 2014.

7. Li G., Shi G.Q., Bellinger N.C., Stress in Triple-Row Riveted Lap Joints Under the Influence of Specific Factors, Journal of Aircraft, 48 (2011) 527-539.

8. Wronicz W., Kaniowski J. (2011). 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. A. Niepokólczycki (Ed.). Fatigue of Aircraft Structures, Monographic Series, ISSUE 2011, pp. 166–190, ISSN (Online) 2300-7591, DOI: 10.2478/v10164-010-0047-1, August 2011.

9. ASM Handbook, Volume 18, „Friction, Lubrication, and Wear Technology”, 1995

10. Fárek J.: FE-Modelling Methodology of Riveted Joints. Czech Aerospace Proceedings. Journal for Czech Aerospace Research, No 2/2010, pp. 12-16

Fatigue of Aircraft Structures

The Journal of Institute of Aviation

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SCImago Journal Rank (SJR) 2017: 0.102


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