Comparison of Riveted, Bonded & Hybrid Joints using FEA
نویسندگان
چکیده
منابع مشابه
Finite Element Modeling for Thermal Stresses Developed in Riveted and Rivet - Bonded Joints
A three-dimensional finite element modeling is developed using ABAQUS software. This includes riveted and rivet-bonded joints models. Both models undergo thermal heat caused by hot-driven rivet process and then are subjected to a constant velocity at one of its strip edges to simulate the shear tensile test up to the failure point. The developed FE models were based on elastic-plastic propertie...
متن کاملDesigning for Manufacturability in Riveted Joints
The study of human experts in the areas of design and manufacturing has lead to two hypotheses concerning the problem solving methods which these engineers utilize to attack difficult problems. The basis of both hypotheses is a modular approach to problem solving. One hypothesis addresses the nature of the modules utilized while the other hypothesis deals with the organization of the modules. A...
متن کاملModelling and Analysis of Hybrid Composite Joint Using Fem in Ansys
Composite materials are widely used in the various Fields. Due to the high strength they are widely used in the low weight constructions and also used as a suitable alternative to metals. In various applications and also for joining various composite parts together, they are fastened together using adhesives or Mechanical fasteners. Modeling and static analysis of 3-D Models of joints such as b...
متن کاملOptimal Riveted Joints Design of Frame Strcture by IGA
Department of Systems and Information Engineering, Ashikaga Institute of Technology, Ashikaga 326-8558, Japan † Fuzzy Logic Systems Institute, Iizuka 820-0067, Japan Abstract In this paper, we formulate an optimal riveted joints design (ORD) problem of a through gusset plate on a frame structure for a constrained allowable stress as a rigid structural calculation problem and solve it directly b...
متن کاملResidual Strength Analyses of Riveted Lap-Splice Joints
Aging aircraft may develop multiple-site damage (MSD) that can reduce the structural integrity of fuselage structures. The existence of small cracks emanating from adjacent rivet holes in a fuselage lap-splice joint is of major concern. Small collinear cracks greatly reduce the residual strength of a panel with a lead crack. Recent studies predicting the residual strength of flat and curvilinea...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: IARJSET
سال: 2017
ISSN: 2393-8021
DOI: 10.17148/iarjset.2017.4106