کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1718231 1013835 2013 9 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Flexibility of hybrid load transfer assemblies: Influence of tightening pre-stress
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Flexibility of hybrid load transfer assemblies: Influence of tightening pre-stress
چکیده انگلیسی

The flexibility of bolted assemblies of thin parts is a significant parameter, especially in calculating the load distribution between the various fasteners in an assembly. This characteristic is poorly understood in the case of assemblies that are working both in plastic deformation-shearing and friction. The present study firstly focuses on flexibility of an assembly working only by friction. It highlights the influence of pre-stressing and the coefficient of friction on flexibility as also on hysteresis and assesses the influence of the assembled partsʼ geometrical characteristics. The study then goes on to consider a hybrid load transfer assembly. Simulations performed using ABAQUS software provided insight as to how the joint behaves in relation to the pre-stress applied. The results are compared to the case of an assembly working without pre-stress. Using these simulations, a model for determination is proposed. This allows the apparent flexibility of the fastener to be calculated, dissociating the case of apparent flexibility on the first loading cycle needed to calculate the load transfer from the apparent flexibility of the following loading cycles. The formulations proposed thus allow the behaviour of a hybrid load transfer fastener to be characterised in relation to the transferred load FTFT and a dimensionless parameter characterising the latterʼs global behaviour (adhesion or slipping).

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Aerospace Science and Technology - Volume 25, Issue 1, March 2013, Pages 84–92
نویسندگان
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