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Abstrakty
This paper presents diffraction measurements of residual stresses around the rivet, formed during the riveting process. The measurements were made with the XSTRESS-3000 diffractometer, manufactured by Stresstech Oy. The measurements were carried out on specimens made of bare sheet 2024-T3 alloy, (standard AMS-QQ-250 / 4). The measurement results were compared with the FEM simulation results. The work was performed under the EUREKA IMPERIA project E! 3496.
Słowa kluczowe
Czasopismo
Rocznik
Tom
Strony
23--36
Opis fizyczny
Bibliogr. 4 poz., fot., rys., tab., wykr.
Twórcy
autor
- Institute of Aviation, Warsaw, Poland
autor
- Institute of Aviation, Warsaw, Poland
autor
- Institute of Aviation, Warsaw, Poland
autor
- Institute of Aviation, Warsaw, Poland
Bibliografia
- [1] Müller, R., P., G. (1995). An Experimental Investigation on the Fatigue Behavior of Fuselage Riveted Lap Joints; The Significance of the Rivet Squeeze Force, and a Comparison of 2924-T3 and Glare 3. Praca doktorska, Delft University of Technology, Universitatdrukkerij, Delft.
- [2] Mruk, Z. (2008). Riveting process for specimen used in durability tests of riveted joint made with rivets closed with force control and axial strain measure. INSTRUCTION. (in polish). PZL Mielec. (Internal Report 1/DRG-6/42/2008)
- [3] Skorupa, M., Skorupa, A., Machniewicz, T., Korbel, A. (2009). An Experimental Investigation on the Fatigue Performance of Riveted Lap Joints. In: M. J. Bos (Eds.), ICAF 2009, Bridging the Gap between Theory and Operational Practice. Proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue, Rotterdam, The Nederlands, 27-29 May 2009.
- [4] MSC Marc Documentation, Volume A: Theory and User Information. MSC Corp. 2008.
Uwagi
EN
The financial support from Ministry of Science and Higher Education under the contract No. 59/EUR/2006/02 is gratefully acknowledged.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-658bb95c-f7ff-4aef-925c-892fc8fe4125