Parametric study of combined adhesive-riveted lap joints

Riveted lap joints are widely used to assemble complex structures, e.g. aircraft fuselages. A thin layer of adhesive (sealant), is normally applied to lap joints in order to restrict the entry of moisture and retard corrosion. In this work, combined adhesive-riveted lap joints were studied to unders...

Full description

Saved in:
Bibliographic Details
Main Authors: Fongsamootr T., Dechwayukul C., Kamnerdtong N., Rubin C.A., Hahn G.T.
Other Authors: Kishimoto K.Kikuchi M.Shoji T.Saka M.
Format: Conference or Workshop Item
Language:English
Published: 2014
Online Access:http://www.scopus.com/inward/record.url?eid=2-s2.0-3142743237&partnerID=40&md5=00fb39129001256c5b4377cacda7e1d6
http://cmuir.cmu.ac.th/handle/6653943832/1612
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Chiang Mai University
Language: English
id th-cmuir.6653943832-1612
record_format dspace
spelling th-cmuir.6653943832-16122014-08-29T09:29:31Z Parametric study of combined adhesive-riveted lap joints Fongsamootr T. Dechwayukul C. Kamnerdtong N. Rubin C.A. Hahn G.T. Kishimoto K.Kikuchi M.Shoji T.Saka M. Riveted lap joints are widely used to assemble complex structures, e.g. aircraft fuselages. A thin layer of adhesive (sealant), is normally applied to lap joints in order to restrict the entry of moisture and retard corrosion. In this work, combined adhesive-riveted lap joints were studied to understand the effect of three parameters: panel thickness, adhesive stiffness and adhesive layer thickness, on single row non-countersunk riveted lap joints. Finite element analysis (FEA), along with Thin Adhesive Layer Analysis (TALA - developed for simulating the adhesive layer in lap joint models), were used to analyze the joint behavior. In previous studies, the stress concentration factor for single row riveted lap joints was found to be approximately 6.1, and the stress concentration factor for sealed riveted lap joints was approximately 5.2 for a 180 micron thick sealant layer. In this study, panel thickness, adhesive stiffness and adhesive layer thickness were varied parametrically in FEA analyses to determine their affects on the joints. The FEA/TALA results were used to predict the fatigue life of the joints as functions of the three parameters. The results show that the maximum tensile stress is smaller with a smaller panel thickness. The results also showed that the stress concentration factor in the joints was reduced when the stiffness of the adhesive layer was increased or when the thickness of the adhesive layer was decreased. Finally, fatigue tests showed that the fatigue life of the combined adhesive-riveted lap joints was greater than for riveted lap joints without adhesive. 2014-08-29T09:29:31Z 2014-08-29T09:29:31Z 2004 Conference Paper 10139826 63333 KEMAE http://www.scopus.com/inward/record.url?eid=2-s2.0-3142743237&partnerID=40&md5=00fb39129001256c5b4377cacda7e1d6 http://cmuir.cmu.ac.th/handle/6653943832/1612 English
institution Chiang Mai University
building Chiang Mai University Library
country Thailand
collection CMU Intellectual Repository
language English
description Riveted lap joints are widely used to assemble complex structures, e.g. aircraft fuselages. A thin layer of adhesive (sealant), is normally applied to lap joints in order to restrict the entry of moisture and retard corrosion. In this work, combined adhesive-riveted lap joints were studied to understand the effect of three parameters: panel thickness, adhesive stiffness and adhesive layer thickness, on single row non-countersunk riveted lap joints. Finite element analysis (FEA), along with Thin Adhesive Layer Analysis (TALA - developed for simulating the adhesive layer in lap joint models), were used to analyze the joint behavior. In previous studies, the stress concentration factor for single row riveted lap joints was found to be approximately 6.1, and the stress concentration factor for sealed riveted lap joints was approximately 5.2 for a 180 micron thick sealant layer. In this study, panel thickness, adhesive stiffness and adhesive layer thickness were varied parametrically in FEA analyses to determine their affects on the joints. The FEA/TALA results were used to predict the fatigue life of the joints as functions of the three parameters. The results show that the maximum tensile stress is smaller with a smaller panel thickness. The results also showed that the stress concentration factor in the joints was reduced when the stiffness of the adhesive layer was increased or when the thickness of the adhesive layer was decreased. Finally, fatigue tests showed that the fatigue life of the combined adhesive-riveted lap joints was greater than for riveted lap joints without adhesive.
author2 Kishimoto K.Kikuchi M.Shoji T.Saka M.
author_facet Kishimoto K.Kikuchi M.Shoji T.Saka M.
Fongsamootr T.
Dechwayukul C.
Kamnerdtong N.
Rubin C.A.
Hahn G.T.
format Conference or Workshop Item
author Fongsamootr T.
Dechwayukul C.
Kamnerdtong N.
Rubin C.A.
Hahn G.T.
spellingShingle Fongsamootr T.
Dechwayukul C.
Kamnerdtong N.
Rubin C.A.
Hahn G.T.
Parametric study of combined adhesive-riveted lap joints
author_sort Fongsamootr T.
title Parametric study of combined adhesive-riveted lap joints
title_short Parametric study of combined adhesive-riveted lap joints
title_full Parametric study of combined adhesive-riveted lap joints
title_fullStr Parametric study of combined adhesive-riveted lap joints
title_full_unstemmed Parametric study of combined adhesive-riveted lap joints
title_sort parametric study of combined adhesive-riveted lap joints
publishDate 2014
url http://www.scopus.com/inward/record.url?eid=2-s2.0-3142743237&partnerID=40&md5=00fb39129001256c5b4377cacda7e1d6
http://cmuir.cmu.ac.th/handle/6653943832/1612
_version_ 1681419702960652288