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Adhesively bonded single lap joint of composites

Uniones adhesivas de traslape simple de compuestos

dc.creatorAlvarado Prieto, Peter
dc.date2013-09-01
dc.date.accessioned2021-06-17T12:57:07Z
dc.date.available2021-06-17T12:57:07Z
dc.identifierhttps://publicacionesfac.com/index.php/cienciaypoderaereo/article/view/5
dc.identifier10.18667/cienciaypoderaereo.5
dc.identifier.urihttps://hdl.handle.net/20.500.12963/70
dc.descriptionA study of single lap joints of composite materials with and without attachments is presented. Failure of this type of joint is caused by the high peel stress in a perpendicular direction presented in the geometric singularity. It is shown that the joint strength is affected by factors such as surface preparation, the adhesive curing process and cleaning. The two configurations, with and without attachments, are compared. It is shown that the single lap joint with attachment has a higher strength than the joint without attachments when no fillet is left on the geometrical singularity. However, because of the low increase in joint strength and the complexity of manufacturing, the choice of type of joint is left to the manufacturer's judgment.eng
dc.description El siguiente artículo muestra un estudio de uniones de traslape simple de materiales compuestos, con y sin modificación. La falla de este tipo de uniones es causada por el alto esfuerzo de despegue en dirección perpendicular a la aplicación de la fuerza presentado en la singularidad geométrica. Se muestra que la resistencia de la unión es afectada por factores como la preparación de la superficie, el proceso de curado del adhesivo, y la limpieza. Ambas configuraciones, con y sin modificación, son comparadas. Se muestra que la unión de traslape simple modificada, tiene una mayor resistencia que sin modificación cuando se remueve el exceso de adhesivo en la singularidad geométrica. Sin embargo, el bajo incremento en la resistencia de la unión y la complejidad para manufactura, deja a consideración del fabricante la decisión respecto a qué tipo de unión usar.  spa
dc.formatapplication/pdf
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dc.languageeng
dc.publisherEscuela de Postgrados de la Fuerza Aérea Colombianaspa
dc.relationhttps://publicacionesfac.com/index.php/cienciaypoderaereo/article/view/5/6
dc.relationhttps://publicacionesfac.com/index.php/cienciaypoderaereo/article/view/5/107
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dc.sourceCiencia y Poder Aéreo; Vol. 8 No. 1 (2013): Enero - Diciembre; 33-41eng
dc.sourceCiencia y Poder Aéreo; Vol. 8 Núm. 1 (2013): Enero - Diciembre; 33-41spa
dc.sourceCiencia y Poder Aéreo; v. 8 n. 1 (2013): Enero - Diciembre; 33-41por
dc.source2389-9468
dc.source1909-7050
dc.subjectAdherenteng
dc.subjectadhesiveeng
dc.subjectbond lineeng
dc.subjectcompositeeng
dc.subjectjointseng
dc.subjectAdherentspa
dc.subjectadhesivespa
dc.subjectbond linespa
dc.subjectcompositespa
dc.subjectjointsspa
dc.titleAdhesively bonded single lap joint of compositeseng
dc.titleUniones adhesivas de traslape simple de compuestosspa
dc.typeinfo:eu-repo/semantics/article
dc.typeinfo:eu-repo/semantics/publishedVersion


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