Failure of Blind Riveted Joint of Carbon Laminates

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F49777513%3A23520%2F20%3A43957627" target="_blank" >RIV/49777513:23520/20:43957627 - isvavai.cz</a>

Výsledek na webu

<a href="https://arc.aiaa.org/doi/10.2514/6.2020-1931" target="_blank" >https://arc.aiaa.org/doi/10.2514/6.2020-1931</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.2514/6.2020-1931" target="_blank" >10.2514/6.2020-1931</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Failure of Blind Riveted Joint of Carbon Laminates

Popis výsledku v původním jazyce

Thispaperdealswiththeexperimentalandnumericalinvestigationsofmechanicalbehavior of the single-lap joint of laminates consisting of TENAX-J IMS60 E13 24K carbon fibers and MSG L285 epoxy resin. TIBULB high-strength blind rivets having a diameter of 4.8 mm and 6.4 mm were used for the joint. Tension tests were performed to investigate the material parameters of the laminate and the clearance effect. The rivet clamping force was evaluated based on a torsion test. The finite element method model of the joint using non-linear shear stress-strain relations of a lamina and using Puck’s failure criterion for the 3D stress state was created. The model was used to analyze the failure of the joint under quasi-static loading. The maximum number of loading cycles leading to joint failure and the decrease in the joint load capacity and stiffness due to the cyclic loading were investigated.

Název v anglickém jazyce

Failure of Blind Riveted Joint of Carbon Laminates

Popis výsledku anglicky

Thispaperdealswiththeexperimentalandnumericalinvestigationsofmechanicalbehavior of the single-lap joint of laminates consisting of TENAX-J IMS60 E13 24K carbon fibers and MSG L285 epoxy resin. TIBULB high-strength blind rivets having a diameter of 4.8 mm and 6.4 mm were used for the joint. Tension tests were performed to investigate the material parameters of the laminate and the clearance effect. The rivet clamping force was evaluated based on a torsion test. The finite element method model of the joint using non-linear shear stress-strain relations of a lamina and using Puck’s failure criterion for the 3D stress state was created. The model was used to analyze the failure of the joint under quasi-static loading. The maximum number of loading cycles leading to joint failure and the decrease in the joint load capacity and stiffness due to the cyclic loading were investigated.

Druh

D - Stať ve sborníku

CEP obor

—

OECD FORD obor

20302 - Applied mechanics

Projekt

Výsledek vznikl pri realizaci vícero projektů. Více informací v záložce Projekty.

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2020

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

AIAA Scitech 2020 Forum

ISBN

978-1-62410-595-1

ISSN

—

e-ISSN

—

Počet stran výsledku

18

Strana od-do

1-18

Název nakladatele

American Institute of Aeronautics and Astronautics Inc, AIAA

Místo vydání

Neuveden

Místo konání akce

Orlando, FL

Datum konání akce

6. 1. 2020

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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