As applications for shape memory polymers (SMPs) become more advanced, it is necessary to have the ability to monitor both the actuation and thermal properties of structures made of such materials. In this paper, a method of using three stereo pairs of webcams and a single thermal camera is studied for the purposes of both tracking three dimensional motion of shape memory polymers, as well as the temperature of points of interest within the SMP structure. The method used includes a stereo camera calibration with integrated local minimum tracking algorithms to locate points of interest on the material and measure their temperature through interpolation techniques. The importance of the proposed method is that it allows a means to cost effectively monitor the surface temperature of a shape memory polymer structure without having to place intrusive sensors on the samples, which would limit the performance of the shape memory effect. The ability to monitor the surface temperatures of a SMP structure allows for more complex configurations to be created while increasing the performance and durability of the material. Additionally, as compared to the previous version, both the functionalities of the testbed and the user interface have been significantly improved.

In this study, four different NiTi-based shape memory alloys (SMAs) compositions were processed, shape-set, and characterized to evaluate their effectiveness as SMA actuation component for satellite antennas. Three of the compositions were commercially available NiTi wires (90°C Flexinol® actuator NiTi wire and Confluent ADB SE508 NiTi wire), NiTi SM495 plates (ATI Specialty Alloys and Components) and the other composition was in house lab-produced NiTiCu plate. Different shape-setting techniques were performed such as pin and plate, fixtures and dies, and finally a sandwich fixture. The two most promising outcomes were the SE NiTi 508 wire and the NiTiCu plate. A SE NiTi 508 wire was first heat-treated at 550 °C for 3 hours and then it was shape-set at 450 °C for 30 min using a Cu tube which was previously deformed to the desired deployment curvature and fixed on a steel rig. The wire was kept inside the Cu tube during the shape-setting process to obtain the desired curvature. After shape-setting, the wire was thermally cycled multiple times. The results showed that the SE NiTi 508 wire was able to retain its deployment shape successfully after each thermal cycle. Furthermore, a NiTiCu plate was sandwiched between two steel sheets which were shaped into the desired full-deployment shape beforehand. The NiTiCu plate was shape-set at 450 °C for 30 min and then thermally cycled multiple times to test its effectiveness. The NiTiCu plate retained its full-deployment shape successfully after every thermal cycle.

Dans ce travail, des modèles thermomécaniques basés sur une approche non-locale sont proposés pour décrire le comportement des Alliages à Mémoire de Forme (AMF) avec la prise en compte des effets de la localisation et de la chaleur latente lors de la transformation de phase. Ces modèles sont obtenus comme des extensions d’un modèle local existant. Pour décrire la localisation de la transformation de phase, l’extension du modèle initial a consisté à le réécrire dans un contexte non-local par l’introduction d’une nouvelle variable, définie comme la contrepartie non-locale de la fraction volumique de martensite déjà présente dans le modèle local. L’exploitation de ce modèle a nécessité le développement d’un élément fini spécial dans ABAQUS avec la fraction volumique non-locale de martensite comme un degré de liberté supplémentaire. Les simulations réalisées montrent la pertinence d’une telle approche dans la description de la transformation de phase dans des structures minces en AMF, soumises à des chargements thermomécaniques. Pour décrire les effets de la chaleur latente, une équation d’équilibre thermique ayant comme terme source des contributions dépendant de la transformation de phase a été adjointe au modèle initial. Là encore, l’exploitation du modèle a nécessité le développement d’un élément fini qui prend en compte le couplage thermomécanique et la formulation proposée pour l’équilibre thermique. Les simulations numériques réalisées ont montré l’effet retardant sur la transformation de phase de la chaleur latente, et le caractère hétérogène possible de la transformation dans ce cas. Ces effets sont d’autant plus importants que la vitesse de déformation est élevée / In this Phd thesis, thermo-mechanical models based on a nonlocal approach are proposed in order to describe the behavior of Shape Memory Alloys (SMA), taking into account localization and latent heat effects during phase transformation. These models are obtained as extensions of an existing local model. In order to describe the localization of phase transformation, the extension of the initial model consisted of rewriting it in a nonlocal context through the introduction of a new variable, defined as the nonlocal counterpart of the martensite volume fraction. The use of this model has required the development of a specific finite element in ABAQUS with the nonlocal martensite volume fraction as an additional degree of freedom. The simulations show the relevance of such an approach in the description of the phase transformation occurring in thin SMA structures subjected to thermo-mechanical loadings. To achieve the description of the latent heat effects, a heat balance equation with a source term depending on contributions of the phase transformation was added to the constitutive equations of the initial model. Even there, the use of the model required the development of a finite element which takes into account the thermo-mechanical coupling and considers the proposed formulation for the thermal balance. Numerical simulations have shown the delaying effect of the latent heat on phase transformation and the possible heterogeneous character of the phase transformation in this case. These effects are even more important as the strain rate is high

Les polymères à mémoire de forme (SMP) sont des matériaux qui peuvent revenir à leur forme d'origine lorsqu'un stimulus approprié (par exemple de la chaleur) est prévu. Ces polymères sont programmés par cycle de mémoire de forme qui se compose de deux parties: une partie de la programmation qui donne un effet mémoire de forme (SME) à savoir la forme temporaire pour le polymère et la partie de récupération où il revient à sa forme initiale. Les SMP ont une faible rigidité, donc, produisent de grandes déformations récupérables, mais produisent des forces de récupération faibles. Cependant, les composites SMP produisent des forces de récupération plus grandes car ils sont relativement rigide mais ont des souches moins récupérables. En outre, de forts actionneurs à mémoire de forme peuvent être produits si deux effets différents peuvent être combinés dans une structure unique. Une structure déjà active (par exemple des alliages à mémoire de forme) peut être intégré dans SMP. Par conséquent, un fort actionneur couplé peut être obtenu. [...] / Shape memory polymers (SMPs) are the materials which can return to their original shape when a suitable stimulus (e.g. heat) is provided. These polymers are programmed through shape memory cycle that consists of two parts: programming part which gives shape memory effect (SME) i.e. temporary shape to the polymer and the recovery part which return it to its original shape. SMPs have low stiffness, therefore, produce large recoverable strains, but produce low recovery forces. However, SMP composites produce larger recovery forces as they are relatively rigid but have less recoverable strains. Moreover, strong shape memory actuators can be produced if two different effects can be combined in a single structure. An already active structure (e.g shape memory alloys) can be embedded in SMP. Consequently, a strong coupled actuator can be obtained. In this work, the shape memory property of CBCM composite (an active composite that works on bimetallic affect) has been studied. CBCM stands for controlled behavior of composite material. CBCM activeness and its SM property has been coupled together to obtain a strong actuator. SM property has been obtained through thermo-mechanical programming at a temperature higher than glass transition temperature (Tg) of Epoxy resin used for its fabrication. The CBCM actuating properties have been studied through different one-step recoveries (unconstrained, constrained and recovery under load). Moreover, different asymmetrical CBCM composites have been developed by changing the position and orientation of the different layers used. These have been studied for their different actuation properties. Similarly, multi-step recoveries (unconstrained and constrained) have also been performed to show multi step actuation capabilities in CBCM. The actuating properties of CBCM have also been compared with symmetrical composite (SYM) to show the advantage of coupled properties in CBCM. It has been found that CBCM has the ability to give high strain, high recovery forces. Also, it can recover under load and recover to its original position at the temperatures lower than the deforming temperature used in the programming cycle.

Disertace analyzuje vliv koncentrátorů napětí na průběh martensitické transformace, vznik plastické deformace a její vliv na přerozdělení napětí a vznik zbytkového pnutí a reziduálního martenzitu v okolí koncentrátorů v prvcích ze slitin s tvarovou pamětí NiTi. Vliv je analyzován v režimech superelastického isotermálního cyklování a aktuačního cyklování, t.j. teplotního cyklování pod vnějším napětím. Disertace využívá pro vyhodnocení vlivu experimentální přístup spolu s numerickými simulacemi metodou konečných prvků na modelových případech tenkých pásků ze slitin NiTi opatřených půlkruhovými vruby. V experimentální části je vyhodnocován vliv koncentrátorů pomocí termomechanických experimentů s využitím metod obrazové korelace a rentgenové mikrodifrakce pro lokální analýzu deformací a fázových objemových podílů v průběhu cyklování v okolí vrubů. Simulace metodou konečných prvků poskytují komplementární informace o průběhu napětí, deformací a martensitické transformaci, zejména o vývoji jednotlivých složek celkové deformace, tj. elastické a plastické, a vývoji zbytkového pnutí a s ním souvisejícím zbytkovým martensitem.Disertace je dále doplněna o numerickou analýzu vlivu konstrukce stentů na lokální cyklický průběh martensitické transformace a jeho vliv na únavové vlastnosti.

Le comportement des alliages à mémoire de forme (AMF) et des alliages à mémoire de forme magnétiques (AMFM) est régi par les mécanismes de transformation martensitique à l'échelle de la microstructure, à l'origine de leurs propriétés remarquables (mémoire de forme, superélasticité, grandes déformations associées à la réorientation martensitique sous champ magnétique). Les mécanismes de transformation et de réorientation martensitique peuvent être induits par des sollicitations thermiques, magnétiques et / ou mécaniques et de manière couplée. La mise au point d'outils de conception fiables nécessite une meilleure prédictibilité du comportement réel des alliages à mémoire de forme sous sollicitations thermo - magnéto - mécaniques complexes.Le choix d'une modélisation multiaxiale et multi échelle est pertinent. Le modèle reporté présente une formulation unifiée, permettant de simuler aussi bien le comportement des AMF que celui des AMFM.Parallèlement au développement de ce modèle, une étude expérimentale est nécessaire afin d'une part d'identifier les propriétés intrinsèques des matériaux étudiés, et d'autre part de valider les estimations de la modélisation. A cette fin, des mesures de fractions volumiques de phase par diffraction des rayons X in situ ont été entreprises lors de sollicitations thermiques (cycles de chauffage-refroidissement), mécaniques (traction, compression, essais biaxiaux) et magnétiques (champ magnétique unidirectionnel). L'exploitation des résultats de diffractométrie permet une analyse quantitative des fractions volumiques des phases en présence. Celles-ci sont comparées aux estimations du modèle à des fins de validation. / The behavior of shape memory alloys (SMA) and magnetic shape memory alloys (MSMA) is governed by the martensitic transformation mechanisms at the scale of the microstructure. This transformation is at the origin of their remarkable properties (memory effect, superelasticity, large deformations associated with the martensitic reorientation under magnetic field). The martensitic transformation and reorientation mechanisms can be induced by thermal, magnetic and / or mechanical stresses and in a coupled manner. The development of reliable design tools requires a better predictability of the actual behavior of shape memory alloys under complex thermal-magneto-mechanical loading.The choice of multiaxial and multiscale modeling is relevant. The model proposed in this work presents a unified formulation, making possible to simulate both the behavior of SMA and MSMA.In parallel with the development of this model, an experimental study is necessary in order to identify the intrinsic properties of the materials studied and to validate the estimates of the modeling. For this purpose, measurements of phase fractions by in-situ X-ray diffraction were carried out during thermal (heating-cooling cycles), mechanical (tensile, compressive, biaxial) and magnetic (unidirectional magnetic field) loadings. The diffraction patterns allow a quantitative estimation of the volume fractions of the phases. These are compared to model estimates for validation purposes.

Deformation phenomena in shape memory alloys involve stress-, temperature-induced phase transformations and crystallographic variant conversion or reorientation, equivalent to a twinning operation. In near equiatomic NiTi, Ti rich compositions can exist near room temperature as a monoclinic B19' martensitic phase, which when deformed undergoes twinning resulting in strains as large as 8%. Upon heating, the martensite transforms to a cubic B2 austenitic phase, thereby recovering the strain and exhibiting the shape memory effect. Ni rich compositions on the other hand can exist near room temperature in the austenitic phase and undergo a reversible martensitic transformation on application of stress. Associated with this reversible martensitic transformation are macroscopic strains, again as large as 8%, which are also recovered and resulting in superelasticity. This work primarily focuses on neutron diffraction measurements during loading at the Los Alamos Neutron Science Center at Los Alamos National Laboratory. Three phenomena were investigated: First, the phenomena of hysteresis reduction and increase in linearity with increasing plastic deformation in superelastic NiTi. There is usually a hysteresis associated with the forward and reverse transformations in superelastic NiTi which translates to a hysteresis in the stress-strain curve during loading and unloading. This hysteresis is reduced in cold-worked NiTi and the macroscopic stress-strain response is more linear. This work reports on measurements during loading and unloading in plastically deformed (up to 11%) and cycled NiTi. Second, the tension-compression stress-strain asymmetry in martensitic NiTi. This work reports on measurements during tensile and compressive loading of polycrystalline shape-memory martensitic NiTi with no starting texture. Third, a heterogeneous stress-induced phase transformation in superelastic NiTi. Measurements were performed on a NiTi disc specimen loaded laterally in compression and associated with a macroscopically heterogeneous stress state. For the case of superelastic NiTi, the experiments related the macroscopic stress-strain behavior (from an extensometer or an analytical approach) with the texture, phase volume fraction and strain evolution (from neutron diffraction spectra). For the case of shape memory NiTi, the macroscopic connection was made with the texture and strain evolution due to twinning and elastic deformation in martensitic NiTi. In all cases, this work provided for the first time insight into atomic-scale phenomena such as mismatch accommodation and martensite variant selection. The aforementioned technique of neutron diffraction for mechanical characterization was also extended to engineering components and focused mainly on the determination of residual strains. Two samples were investigated and presented in this work; first, a welded INCONEL 718 NASA space shuttle flow liner was studied at 135 K and second, Ti-6Al-4V turbine blade components were investigated for Siemens Westinghouse Power Corporation. Lastly, also reported in this dissertation is a refinement of the methodology established in the author's masters thesis at UCF that used synchrotron x-ray diffraction during loading to study superelastic NiTi. The Los Alamos Neutron Science Center is a national user facility funded by the United States Department of Energy, Office of Basic Energy Sciences, under Contract No. W-7405-ENG-36. The work reported here was made possible by grants to UCF from NASA (NAG3-2751), NSF CAREER (DMR-0239512), Siemens Westinghouse Power Corporation and the Space Research Initiative.

No description available.

Magnetic shape memory alloys are active materials which deform under the application of a magnetic field or an external stress. Due to their internal friction, recognizable from the strain-stress hysteresis, this new material technology allows the design of multistable actuators. This paper describes and characterizes an innovative airflow control valve whose aperture is proportional to the deformation of the active material and thus controllable by the input voltage. The multistability of the material is partially exploited within an airflow control loop to reduce the energy losses of the valve when a specific airflow value must be hold.

A study on shape memory alloy materials as vibration dampers is reported. An important component is the strain rate-dependent and temperature-dependent constitutive behavior of shape memory alloy, which can significantly change its energy dissipation capacity under cyclic loading. The constitutive model used accounts for the thermo-mechanical strain rate-dependent behavior and phase transformation. With increasing structural flexibility, the hysteretic loop size of shape memory alloy dampers increases due to increasing strain rates, thus further decreasing the response of the structure to cyclic excitation. The structure examined is a beam, and its behavior with shape memory alloy dampers is compared to the same beam with conventional dampers. Parametric studies reveal the superior performance of the shape memory alloy over the conventional dampers even at the resonance frequency of the beam-damper system. An important behavior of the shape memory alloy dampers is discovered, in that they absorb energy from the fundamental and higher vibration modes. In contrast, the conventional dampers transfer energy to higher modes. For the same beam control, the stiffness requirement for the shape memory alloy dampers is significantly less than that of the conventional dampers. Response quantities of interest show improved performance of the shape memory alloy over the conventional dampers under varying excitation intensity, frequency, temperature, and strain rate.