Analysis of the Local Phenomena during Riveting Process

Author:

Kaniowski Jerzy1,Wronicz Wojciech1,Pietrzak Krystyna2

Affiliation:

1. Institute of Aviation

2. Instytut Transportu Samochodowego

Abstract

The riveting still remains the most popular and basic method of joining metal parts in airframes. At the same time, the rivets are critical from the fatigue point of view. The paper presents the selected investigations of local phenomena during the riveting process. At the beginning, some results from the literature, concerned on the riveting process influence on fatigue of the three-row lap joint were shown. The analysis of these results leads to the conclusion that the increase in fatigue life caused by higher riveting force is so high that the more beneficial residual stress cannot be the only explanation, but the new phenomena in riveting process occurs and it is a reason of huge increase in fatigue life. The working hypothesis has been assumed that during the riveting process adhesive joint (called cold welding) were formed between the rivet shank and the sheets. Several microstructure tests were conducted in order to verify this hypothesis. The tests include riveting the specimens for various configurations and analyses of the microsection of selected specimens with the use of optical and scanning electron microscope. In the case of several specimens the punctual and linear welding between rivet shank and sheets were observed. The paper presents the investigation and selected results. The authors are going to continue presented researches.

Publisher

Trans Tech Publications, Ltd.

Subject

Condensed Matter Physics,General Materials Science,Atomic and Molecular Physics, and Optics

Reference7 articles.

1. J. Kaniowski. The Synthetic Description of the Results, Scientific Achievements and Practical Application of the Eureka-IMPERJA Project, in: A. Niepokólczycki (Ed. ), Fatigue of Aircraft Structures, Monographic Series, Institute of Aviation Scientific Publication, Warsaw, 2012, pp.38-57.

2. R.P. G Müller., An Experimental and Analytical Investigation on the Fatigue Behaviour of Fuselage Riveted Lap Joint, Ph.D. thesis, Delft University of Technology, Delft, (1995).

3. R.P.G. Müller, L.J. Hart-Smith, Making fuselage riveting lap splices with 200-year crack-free fatigue life, in: P. Pool (Ed. ), ICAF 19, Fatigue in new and ageing aircraft, EMAS Publishing, Edinburgh, 1997 pp.499-522.

4. A. Skorupa, M. Skorupa, Riveted Lap Joints in Aircraft Fuselage, Design, Analysis and Properties, in series Solid Mechanics and Application, vol. 189, Springer, Dordrecht, Heidelberg, New York, London, (2012).

5. J. Kaniowski et al., Improving the Fatigue Performance of Riveted Joints in Airframes, The Final Report of The Research Project No. EUREKA/59/2006, Institute of Aviation internal report, Warsaw, 2011 (in Polish).

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