Back to Search Start Over

Pre-tensioning effect on fatigue life of bolted shear joints

Authors :
Taha Benhaddou
Pierre Stéphan
Alain Daidié
Jean-Baptiste Tuery
Jean Guillot
Clement Chirol
Département Matériaux et Procédés, Airbus Operations SAS
Airbus [France]
Institut Clément Ader (ICA)
Institut National des Sciences Appliquées - Toulouse (INSA Toulouse)
Institut National des Sciences Appliquées (INSA)-Institut National des Sciences Appliquées (INSA)-Centre National de la Recherche Scientifique (CNRS)-Université Toulouse III - Paul Sabatier (UT3)
Université Fédérale Toulouse Midi-Pyrénées-Université Fédérale Toulouse Midi-Pyrénées-IMT École nationale supérieure des Mines d'Albi-Carmaux (IMT Mines Albi)
Institut Mines-Télécom [Paris] (IMT)-Institut Mines-Télécom [Paris] (IMT)-Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO)
Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO)-Institut National des Sciences Appliquées - Toulouse (INSA Toulouse)
Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Université Toulouse III - Paul Sabatier (UT3)
Université de Toulouse (UT)-Centre National de la Recherche Scientifique (CNRS)-IMT École nationale supérieure des Mines d'Albi-Carmaux (IMT Mines Albi)
Institut Mines-Télécom [Paris] (IMT)-Institut Mines-Télécom [Paris] (IMT)
Source :
Aerospace Science and Technology, Aerospace Science and Technology, 2014, 36, pp.36-43. ⟨10.1016/j.ast.2014.03.003⟩
Publication Year :
2014
Publisher :
HAL CCSD, 2014.

Abstract

International audience; A number of experimental studies have demonstrated that pre-tensioning fasteners significantly increases the fatigue life of shear joints. Fatigue life prediction for clamped joints is still a complex and unresolved issue because of the mixed nature of load transfer, which partly occurs by frictional forces. This article presents a calculation method based on a multiaxial-type critical-plane criterion, which determines the fatigue life and fatigue crack initiation site. For this purpose, the values of hydrostatic pressure and amplitude of maximum alternating shear stress on a critical octahedral plane are determined at each point of the structure and for each loading increment, and are used to predict the fatigue life of the joint. A dedicated experimental study was conducted within materials & processes airbus laboratory to validate the numerical results. In addition, a dimensionless parameter Rs is introduced to quantify the proportion of load transferred by friction and by bearing of the bolt, and allows the optimal preload to be approximated, above which value more clamping should not give further improvement. This value characterizes the shift of the crack location from the net section to the outside of the compressed area.

Details

Language :
English
Database :
OpenAIRE
Journal :
Aerospace Science and Technology, Aerospace Science and Technology, 2014, 36, pp.36-43. ⟨10.1016/j.ast.2014.03.003⟩
Accession number :
edsair.doi.dedup.....66af8771434f18364266aa348964b8fe
Full Text :
https://doi.org/10.1016/j.ast.2014.03.003⟩