Análisis del comportamiento a fatiga de uniones adhesivas de acero recubierto

Los adhesivos se conocen y han sido utilizados en multitud de aplicaciones a lo lago de la historia. En la actualidad, la tecnología de la adhesión como método de unión de materiales estructurales está en pleno crecimiento. Los avances científicos han permitido comprender mejor los fenómenos de adhesión, así como, mejorar y desarrollar nuevas formulaciones poliméricas que incrementan el rango de aplicaciones de los adhesivos. Por otro lado, el desarrollo de nuevos materiales y la necesidad de aligerar peso, especialmente en el sector transporte, hace que las uniones adhesivas se introduzcan en aplicaciones hasta ahora reservadas a otros sistemas de unión como la soldadura o las uniones mecánicas, ofreciendo rendimientos similares y, en ocasiones, superiores a los aportados por estas. Las uniones adhesivas ofrecen numerosas ventajas frente a otros sistemas de unión. En la industria aeronáutica y en automoción, las uniones adhesivas logran una reducción en el número de componentes (tales como los tornillos, remaches, abrazaderas) consiguiendo como consecuencia diseños más ligeros y una disminución de los costes de manipulación y almacenamiento, así como una aceleración de los procesos de ensamblaje, y como consecuencia, un aumento de los procesos de producción. En el sector de la construcción y en la fabricación de equipos industriales, se busca la capacidad para soportar la expansión y contracción térmica. Por lo tanto, se usan las uniones adhesivas para evitar producir la distorsión del sustrato al no ser necesario el calentamiento ni la deformación de las piezas cuando se someten a un calentamiento elevado y muy localizado, como en el caso de la soldadura, o cuando se someten a esfuerzos mecánicos localizados, en el caso de montajes remachados. En la industria naval, se están desarrollando técnicas de reparación basadas en la unión adhesiva para distribuir de forma más uniforme y homogénea las tensiones con el objetivo de mejorar el comportamiento frente a fatiga y evitar los problemas asociados a las técnicas de reparación habituales de corte y soldadura. Las uniones adhesivas al no requerir importantes aportes de calor como la soldadura, no producen modificaciones microestructurales indeseables como sucede en la zona fundida o en la zona afectada térmicamente de las uniones soldadas, ni deteriora los recubrimientos protectores de metales de bajo punto de fusión o de naturaleza orgánica. Sin embargo, las uniones adhesivas presentan una desventaja que dificulta su aplicación, se trata de su durabilidad a largo plazo. La primera causa de rotura de los materiales es la rotura por fatiga. Este proceso de fallo es la causa del 85% de las roturas de los materiales estructurales en servicio. La rotura por fatiga se produce cuando se somete al material a la acción de cargas que varían cíclicamente o a vibraciones durante un tiempo prolongado. Las uniones y estructuras sometidas a fatiga pueden fallar a niveles de carga por debajo del límite de resistencia estática del material. La rotura por fatiga en las uniones adhesivas no se produce por un proceso de iniciación y propagación de grieta de forma estable, el proceso de fatiga va debilitando poco a poco la unión hasta que llega un momento que provoca una rotura de forma rápida. Underhill explica este mecanismo como un proceso de daño irreversible de los enlaces más débiles en determinados puntos de la unión. Cuando se ha producido el deterioro de estas zonas más débiles, su área se va incrementando hasta que llega un momento en que la zona dañada es tan amplia que se produce el fallo completo de la unión. En ensayos de crecimiento de grieta realizados sobre probetas preagrietadas en viga con doble voladizo (DCB), Dessureault identifica los procesos de iniciación y crecimiento de grietas en muestras unidas con adhesivo epoxi como una acumulación de microfisuras en la zona próxima al fondo de grieta que, luego, van coalesciendo para configurar la grieta principal. Lo que supone, igualmente, un proceso de daño del adhesivo en la zona de mayor concentración de tensiones que, posteriormente, conduce al fallo de la unión. La presente tesis surge con el propósito de aumentar los conocimientos existentes sobre el comportamiento a fatiga de las uniones adhesivas y especialmente las realizadas con dos tipos de adhesivos estructurales aplicados en aceros con diferentes acabados superficiales. El estudio incluye la obtención de las curvas de tensión frente al número de ciclos hasta el fallo del componente, curvas SN o curvas de Wöhler, que permitirán realizar una estimación de la resistencia a la fatiga de un determinado material o estructura. Los ensayos de fatiga realizados mediante ciclos predeterminados de carga sinusoidales, de amplitud y frecuencia constantes, han permitido caracterizar el comportamiento a la fatiga por el número de ciclos hasta la rotura, siendo el límite de fatiga el valor al que tiende la tensión cuando el número de ciclos es muy grande. En algunos materiales, la fatiga no tiende a un valor límite sino que decrece de forma constante a medida que aumenta el número de ciclos. Para estas situaciones, se ha definido la resistencia a la fatiga (o límite de resistencia) por la tensión en que se produce la rotura para un número de ciclos predeterminado. Todos estos aspectos permitirán un mejor diseño de las uniones y las condiciones de trabajo de los adhesivos con el fin de lograr que la resistencia a fatiga de la unión sea mucho más duradera y el comportamiento total de la unión sea mucho mejor, contribuyendo al crecimiento de la utilización de las uniones adhesivas respecto a otras técnicas. ABSTRACT Adhesives are well-known and have been used in many applications throughout history. At present, adhesion bonding technology of structural materials is experiencing an important growth. Scientific advances have enabled a better understanding of the phenomena of adhesion, as well as to improve and develop new polymeric formulations that increase the range of applications. On the other hand, the development of new materials and the need to save weight, especially in the transport sector, have promote the use of adhesive bonding in many applications previously reserved for other joining technologies such as welded or mechanical joints, presenting similar or even higher performances. Adhesive bonding offers many advantages over other joining methods. For example, in the aeronautic industry and in the automation sector, adhesive bonding allows a reduction in the number of components (such as bolts, rivets, clamps) and as consequence, resulting in lighter designs and a decrease in handling and storage costs, as well as faster assembly processes and an improvement in the production processes. In the construction sector and in the industrial equipment manufacturing, the ability to withstand thermal expansion and contraction is required. Therefore, adhesion bonding technology is used to avoid any distortion of the substrate since this technology does not require heating nor the deformation of the pieces when these are exposed to very high and localized heating, as in welding, or when are subjected to localized mechanical stresses in the case of riveted joints. In the naval industry, repair techniques based in the adhesive bonding are being developed in order to distribute stresses more uniform and homogeneously in order to improve the performance against fatigue and to avoid the problems associated with standard repair techniques as cutting and welding. Adhesive bonding does not require the use of high temperatures and as consequence they do not produce undesirable microstructural changes, as it can be observed in molten zones or in heat-affected zones in the case of welding, neither is there damage of the protective coating of metals with low melting points or polymeric films. However, adhesive bonding presents a disadvantage that limits its application, the low longterm durability. The most common cause of fractures of materials is fatigue fracture. This failure process is the cause of 85% of the fracture of structural materials in service. Fatigue failure occurs when the materials are subjected to the action of cyclic loads or vibrations for a long period of time. The joints and structures subjected to fatigue can fail at stress values below the static strength of the material. Fatigue failure do not occurs by a static and homogeneous process of initiation and propagation of crack. The fatigue process gradually weakens the bond until the moment in which the fracture occurs very rapidly. Underhill explains this mechanism as a process of irreversible damage of the weakest links at certain points of the bonding. When the deterioration in these weaker zones occurs, their area increase until the damage zone is so extensive that the full failure of the joint occurs. During the crack growth tests performed on precracked double-cantilever beam specimen, (DCB), Dessureault identified the processes of crack initiation and growth in samples bonded with epoxy adhesive as a process of accumulation of microcracks on the zone near the crack bottom, then, they coalesced to configure the main crack. This is a damage process of the adhesive in the zone of high stress concentration that leads to failure of the bond. This thesis aims to further the understanding of the fatigue behavior of the adhesive bonding, primarily those based on two different types of structural adhesives used on carbon-steel with different surface treatments. This memory includes the analysis of the SN or Wöhler curves (stress vs. number of cycles curves up to the failure), allowing to carry out an estimation of the fatigue strength of a specific material or structure. The fatigue tests carried out by means of predetermined cycles of sinusoidal loads, with a constant amplitude and frequency, allow the characterisation of the fatigue behaviour. For some materials, there is a maximum stress amplitude below which the material never fails for any number of cycles, known as fatigue limit. In the other hand, for other materials, the fatigue does not tend toward a limit value but decreases constantly as the number of cycles increases. For these situations, the fatigue strength is defined by the stress at which the fracture occurs for a predetermined number of cycles. All these aspects will enable a better joint design and service conditions of adhesives in order to get more durable joints from the fatigue failure point of view and in this way contribute to increase the use of adhesive bonding over other joint techniques.

Characterization Of Friction Stir Welded Joints Of Aa 2024-T351 - Native Vs. Treated By Laser Shock Processing

The paper presents a consistent set of results showing the ability of Laser Shock Processing (LSP) in modifying the overall properties of the Friction Stir Welded (FSW) joints made of AA 2024-T351. Based on laser beam intensities above 109 W/cm2 with pulse energies of several Joules and pulses durations of nanoseconds, LSP is able of inducing a compression residual stress field, improving the wear and fatigue resistance by slowing crack propagation and stress corrosion cracking, but also improving the overall behaviour of the structure. After the FSW and LSP procedures are briefly presented, the results of micro-hardness measurements and of transverse tensile tests, together with the corrosion resistance of the native joints vs. LSP treated are discussed. The ability of LSP to generate compressive residual stresses and to improve the behaviour of the FSW joints is underscored.

Optimum adhesive thickness in structural adhesives joints using statistical techniques base on Weibull distribution

The geometrical factors defining an adhesive joint are of great importance as its design greatly conditions the performance of the bonding. One of the most relevant geometrical factors is the thickness of the adhesive as it decisively influences the mechanical properties of the bonding and has a clear economic impact on the manufacturing processes or long runs. The traditional mechanical joints (riveting, welding, etc.) are characterised by a predictable performance, and are very reliable in service conditions. Thus, structural adhesive joints will only be selected in industrial applications demanding mechanical requirements and adverse environmental conditions if the suitable reliability (the same or higher than the mechanical joints) is guaranteed. For this purpose, the objective of this paper is to analyse the influence of the adhesive thickness on the mechanical behaviour of the joint and, by means of a statistical analysis based on Weibull distribution, propose the optimum thickness for the adhesive combining the best mechanical performance and high reliability. This procedure, which is applicable without a great deal of difficulty to other joints and adhesives, provides a general use for a more reliable use of adhesive bondings and, therefore, for a better and wider use in the industrial manufacturing processes.

Mode II fracture energy in the adhesive bonding of dissimilar substrates: carbon fibre composite to aluminium joints

The end-notched flexure (ENF) test calculates the value of mode II fracture energy in adhesive bonding between the substrates of same nature. Traditional methods of calculating fracture energy in the ENF test are not suitable in cases where the thickness of the adhesive is non-negligible compared with adherent thicknesses. To address this issue, a specific methodology for calculating mode II fracture energy has been proposed in this paper. To illustrate the applicability of the proposed method, the fracture energy was calculated by the ENF test for adhesive bonds between aluminium and a composite material, which considered two different types of adhesive (epoxy and polyurethane) and various surface treatments. The proposed calculation model provides higher values of fracture energy than those obtained from the simplified models that consider the adhesive thickness to be zero, supporting the conclusion that the calculation of mode II fracture energy for adhesives with non-negligible thickness relative to their adherents should be based on mathematical models, such as the method proposed in this paper, that incorporate the influence of this thickness.

Fracture propagation and stress corrosion in the case of dissimilar laser hybrid welded joints

The paper addresses the fracture propagation and stress corrosion behaviour of laser hybrid welds achieved between low carbon steel and stainless steel thin sheets. The crack propagation within these overmatched in strength welds was investigated by crack tip opening displacement (CTOD) on CT specimens notched transverse to the weld. A Digital Image Correlation System was used to qualify and estimate the initial crack length obtained by fatigue. The results are associated with the fractographic examinations of various regions of laser hybrid joints. Stress corrosion behaviour of the joint is also discussed.

Overall and local mechanical behaviour of dissimilar laser welded joints

The present investigation addresses the overall and local mechanical performance of dissimilar joints of low carbon steel (CS) and stainless steel (SS) thin sheets achieved by laser welding in case of heat source displacement from the weld gap centreline towards CS. Microstructure characterization and residua! strain scanning, carried out by neutron diffraction, were used to assess the joints features. It was found that the heat source position influences the base metals dilution and the residua! stress field associated to the welding process; the transverse residual stress is smaller than for the longitudinal component, of magnitudes close to the parent CS yield strength. Furthermore, compressive transverse residual stresses were encountered at the SS-weld interface. The tensile behavior of the joint different zones assessed by using a video-image based system (VIC-2D) reveals that the residual stress field, together with the positive difference in yield between the weld metal and the base materials protects the joint from being piastically deformed. The tensile loadings of flat transverse specimens generate the strain localization and failure in CS, far away from the weld.En este trabajo se exponen los resultados de una investigacion sobre el comportamiento mecanico de soldaduras disimiles acero inoxidable-acero al carbono, realizadas para unir chapas delgadas, desplazando la fuente de calor del eje longitudinal de la union soldada por laser sobre el acero al carbono. Se han determinado las caracteristicas microestructurales de la union soldada, las tensiones residuales generadas (mediante difraccion de neutrones) y las curvas tension-deformacion locales y globales, mediante medidas locales de deformacion empleando el sistema VIC-2D "video image correlation". El desplazamiento de la fuente de calor infiuye en la dilution de los metales base y el campo de tensiones residuales asociado al proceso de soldeo; las tensiones residuales medidas en direction longitudinal se aproximan al limite elastico del acero al carbono, mientras que las tensiones residuales transversales son menores, e incluso de compresion. El ensayo a traccion de la union soldada revela que las tensiones residuales y la diferencia de limite elastico entre los metales base y la soldadura propician que la rotura se produzca por inestabilidad plastica del acero al carbono, lejos de la soldadura, sin que la union plastifique.

Laser Shock Processing influence on local properties and overall tensile behavior of friction stir welded joints

Based on laser beam intensities above 109 W/cm2 with pulse energy of several Joules and duration of nanoseconds, Laser Shock Processing (LSP) is capable of inducing a surface compressive residual stress field. The paper presents experimental results showing the ability of LSP to improve the mechanical strength and cracking resistance of AA2024-T351 friction stir welded (FSW) joints. After introducing the FSW and LSP procedures, the results of microstructural analysis and micro-hardness are discussed. Video Image Correlation was used to measure the displacement and strain fields produced during tensile testing of flat specimens; the local and overall tensile behavior of native FSW joints vs. LSP treated were analyzed. Further, results of slow strain rate tensile testing of the FSW joints, native and LSP treated, performed in 3.5% NaCl solution are presented. The ability of LSP to improve the structural behavior of the FSW joints is underscored.

Mechanical Characterization of Lead-Free Sn-Ag-Cu Solder Joints by High-Temperature Nanoindentation

The reliability of Pb-free solder joints is controlled by their microstructural constituents. Therefore, knowledge of the solder microconstituents’ mechanical properties as a function of temperature is required. Sn-Ag-Cu lead-free solder alloy contains three phases: a Sn-rich phase, and the intermetallic compounds (IMCs) Cu6Sn5 and Ag3Sn. Typically, the Sn-rich phase is surrounded by a eutectic mixture of β-Sn, Cu6Sn5, and Ag3Sn. In this paper, we report on the Young’s modulus and hardness of the Cu6Sn5 and Cu3Sn IMCs, the β-Sn phase, and the eutectic compound, as measured by nanoindentation at elevated temperatures. For both the β-Sn phase and the eutectic compound, the hardness and Young’s modulus exhibited strong temperature dependence. In the case of the intermetallics, this temperature dependence is observed for Cu6Sn5, but the mechanical properties of Cu3Sn are more stable up to 200°C.

Residual stress distribution in ferritic-austenitic steel joints made by laser welding

The present investigation addresse the influence of laser welding process-ing parameters used for joining dis-similar metals (ferritic to austenitic steel), on the induced residual stress field. Welding was performed on a Nd:YAG laser DY033 (3300 W) in a continuous wave (CW), keyhole mode. The base metals (BM) employed in this study are AISI 1010 carbon steel (CS) and AISI 304L austenitic stainless steel (SS). Pairs of dissimilar plates of 200 mm x 45 mm x 3 mm were butt joined by laser welding. Different sets of parameters were used to engineer the base metals apportionment at joint formation, namely distinct dilution rates. Residual strain scanning, carried out by neutron diffraction was used to assess the joints. Through-thickness residual stress maps were determined for the laser welded samples of dis-similar steels using high spatial reso-lution. As a result, an appropriate set of processing parameters, able to mi-nimize the local tensile residual stress associated to the welding process, was found.

Characterisation of laser hybrid welded dissimilar joints

The investigation addresses the over-all performance of dissimilar joints of low carbon steel and stainless steel thin sheets achieved by laser hybrid welding. First, the technological de-velopment of dissimilar laser hybrid welding of thin sheets is briefly pre-sented. Joint characterisation by means of macro and microstructural examination and hardness tests is fur-ther described. Microhardness testing was used as an alternative and effi-cient mean of assessing the changes in mechanical properties of difficult to characterize areas, like HAZ and fu-sion zone of these thin sheets Laser-GMA dissimilar welded joints. The overall tensile performance of the joint is discussed together with the weld metal strength overmatching. The ten-sile tests results indicate that in case of transversally loaded joints, the po-sitive difference in yield strength between the weld metal and the base materials (overmatching welds) may reduce the weight of the structure, without diminishing its strength.

Residual stress distribution in ferritic to austenitic steel joints made by laser welding,

In this study, autogenous laser welding was used to join thin plates of low carbon ferritic and austenitic stainless steel. Due to the differences in the thermo-physical properties of base metals, this kind of weld exhibits a complex microstructure, which frequently leads to an overall loss of joint quality. Four welded samples were prepared by using different sets of processing parameters, with the aim of minimizing the induced residual stress field. The dissimilar austenitic-ferritic joints obtained under all welding conditions were uniform and free of defects. Variations in beam position did not influence the weld geometiy, which is a typical keyhole welding. Microstructural characterization and residual strain scanning (by neutron diffraction) were used to assess the features of the joints. By varying laser beam power density and by displacing the laser beam towards the carbon steel side, an optimum combination of processing parameters was found.

Mechanical behavior and residual stress field of dissimilar laser welded joints

The present investigation addresses the mechanical behavior and residual stress field of dissimilar joints produced by laser welding. Microstructure characterization and residual strain scanning, carried out by neutron diffraction, were used to assess the joints features. It was found that the heat source position influences the base metals dilution and the residual stress field associated to the welding process. The tensile behavior of the joint, different zones achieved by using a video-image based system (VIC-2D) reveals that the residual stress field, together with the positive difference in yield between the weld metal and the base materials protects the joint from being plastically deformed.

Effect of strain and magnetic field on the critical current and electric resistance of the joints between HTS coated conductors

Engineering of devices and systems such as magnets, fault current limiters or cables, based on High Temperature Superconducting wires requires a deep characterization of the possible degradation of their properties by handling at room temperature as well as during the service life thus establishing the limits for building up functional devices and systems. In the present work we report our study regarding the mechanical behavior of spliced joints between commercial HTS coated conductors based on YBCO at room temperature and service temperature, 77 K. Tensile tests under axial stress and the evolution of the critical current and the electric resistance of the joints have been measured. The complete strain contour for the tape and the joint has been obtained by using Digital Image Correlation. Also, tensile tests under external magnetic field have been performed and the effect of the applied field on the critical current and the electric resistance of the joints has been studied. Finally, a preliminary numerical study by means of Finite Element Method (FEM) of the mechanical behavior of the joints between commercial HTS is presented.

Effect of strain and magnetic field on the critical current and electric resistance of the joints between HTS coated conductors

Engineering of devices and systems such as magnets, fault current limiters or cables, based on High Temperature Superconducting wires requires a deep characterization of the possible degradation of their properties by handling at room temperature as well as during the service life thus establishing the limits for building up functional devices and systems. In the present work we report our study regarding the mechanical behavior of spliced joints between commercial HTS coated conductors based on YBCO at room temperature and service temperature, 77 K. Tensile tests under axial stress and the evolution of the critical current and the electric resistance of the joints have been measured. The complete strain contour for the tape and the joints has been obtained by using Digital Image Correlation. Also, tensile tests under external magnetic field have been performed and the effect of the applied field on the critical current and the electric resistance of the joints has been studied. Additionally, fatigue tests under constant cyclic stress and loading-unloading ramps have been carried out in order to evaluate the electromechanical behavior of the joints and the effect of maximum applied stress on the critical current. Finally, a preliminary numerical study by means of the Finite Element Method (FEM) of the electromechanical behavior of the joints between commercial HTS is presented.

LSP Influence on Mechanical Properties of Thin Dissimilar Laser Welded Joints

Assessment of laser shock processing effects on mechanical resistance of thin dissimilar laser welded joints