979 resultados para percutaneous mitral balloon valvuloplasty


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OBJECTIVES We sought to assess the safety and efficacy of percutaneous closure of atrial septal defects (ASDs) under fluoroscopic guidance only, without periprocedural echocardiographic guidance. BACKGROUND Percutaneous closure of ASDs is usually performed using simultaneous fluoroscopic and transthoracic, transesophageal (TEE), or intracardiac echocardiographic (ICE) guidance. However, TEE requires deep sedation or general anesthesia, which considerably lengthens the procedure. TEE and ICE increase costs. METHODS Between 1997 and 2008, a total of 217 consecutive patients (age, 38 ± 22 years; 155 females and 62 males), of whom 44 were children ≤16 years, underwent percutaneous ASD closure with an Amplatzer ASD occluder (AASDO). TEE guidance and general anesthesia were restricted to the children, while devices were implanted under fluoroscopic guidance only in the adults. For comparison of technical safety and feasibility of the procedure without echocardiographic guidance, the children served as a control group. RESULTS The implantation procedure was successful in all but 3 patients (1 child and 2 adults; 1.4%). Mean device size was 23 ± 8 mm (range, 4-40 mm). There was 1 postprocedural complication (0.5%; transient perimyocarditis in an adult patient). At last echocardiographic follow-up, 13 ± 23 months after the procedure, 90% of patients had no residual shunt, whereas a minimal, moderate, or large shunt persisted in 7%, 1%, and 2%, respectively. Four adult patients (2%) underwent implantation of a second device for a residual shunt. During a mean follow-up period of 3 ± 2 years, 2 deaths and 1 ischemic stroke occurred. CONCLUSION According to these results, percutaneous ASD closure using the AASDO without periprocedural echocardiographic guidance seems safe and feasible.

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Sunrise is a solar telescope, successfully flown in June 2009 with a long duration balloon from the Swedish Space Corporation Esrange launch site. The design of the thermal control of SUNRISE was quite critical because of the sensitivity to temperature of the optomechanical devices and the electronics. These problems got more complicated due the size and high power dissipation of the system. A detailed thermal mathematical model of SUNRISE was set up to predict temperatures. In this communication the thermal behaviour of SUNRISE during flight is presented. Flight temperatures of some devices are presented and analysed. The measured data have been compared with the predictions given by the thermal mathematical models. The main discrepancies between flight data and the temperatures predicted by the models have been identified. This allows thermal engineers to improve the knowledge of the thermal behaviour of the system for future missions.

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Las enfermedades arteriales vienen presididas por la aterosclerosis, que es un proceso crónico de degeneración, que evoluciona hacia la obstrucción de la luz arterial. La pared de la arteria se engrosa debido al depósito de elementos grasos tales como el colesterol. Los stents intraluminales son diminutas estructuras tubulares autoexpandibles de malla de metal, que se colocan dentro de la arteria coronaria después de una angioplastia con balón para prevenir el cierre de dicha arteria. A pesar de estar diseñados para ser compatibles con el tejido humano, a menudo se da una reacción en cadena de consecuencias indeseables. La reestenosis intra-stent es un problema creciente debido al importante incremento que se ha producido en la utilización del stent intracoronario como forma de revascularización percutánea. Se habla de una incidencia global del 28%, siendo la causa principal de su aparición la proliferación neointimal a través de una compleja cascada de sucesos que pueden tardar meses en desarrollarse. Una de las reacciones más importantes es la trombosis o la formación de una fina capa de coágulo como respuesta a la presencia de un material extraño. Este proceso es multifactorial, y en él intervienen la regresión de la pared como consecuencia del estiramiento previo, la denudación endotelial, lo que permite la agregación plaquetaria, la proliferación neointimal, lo que facilita a los receptores de membrana desencadenar un proceso de agregación posterior y, por último, el remodelado negativo inadecuado de la pared, lo que produce pérdida de luz arterial. Se ha observado frecuentemente que el depósito de ateroma en la pared arterial está relacionado con el valor de los esfuerzos cortantes en la misma. Hay mayores probabilidades de engrosamiento de la pared en las zonas donde son bajos los esfuerzos cortantes, quizá por el mayor tiempo de residencia de las partículas circulantes por el torrente sanguíneo. Si nos centramos en la afirmación anterior, el siguiente paso sería buscar las zonas susceptibles de presentar un valor bajo de dichos esfuerzos. Las zonas potencialmente peligrosas son los codos y bifurcaciones, entre otras. Nos hemos centrado en una bifurcación coronaria, ya que los patrones de flujo que se suelen presentar, tales como recirculación y desprendimiento de vórtices están íntimamente relacionados con las técnicas de implantación de stents en esta zona. Proyectamos nuestros esfuerzos en el estudio de dos técnicas de implante, utilizando un único stent y una tercera a través de una configuración de culotte con el uso de dos stents. El primer caso trata de una bifurcación con un único stent en la rama principal cuyos struts cierran el orificio lateral que da salida a la rama secundaria de la bifurcación, es decir sería un stent sin orificio. El segundo consiste en un único stent también, pero con la diferencia de que éste presenta un orificio de comunicación con la rama lateral. Todas estas técnicas se aplicaron a bifurcaciones de 45º y de 90º. Introdujimos las geometrías -una vez confeccionadas con el código comercial Gambit- en el programa Ansys-Fluent contemplando régimen estacionario. Los resultados obtenidos fueron cotejados con los experimentales, que se realizaron paralelamente, con el fin de corroborarlos. Una vez validados, el estudio computacional ya contó con la fiabilidad suficiente como para abordar el régimen no estacionario, tanto en la versión de reposo como en la de ejercicio –hiperemia- El comportamiento reológico de la sangre para régimen no estacionario en estado de reposo es otra de las tareas abordadas, realizando una comparativa de los modelos Newtoniano, Carreau y Ley de Potencias. Finalmente, en una última etapa, debido a la reciente incursión de los stents diseñados específicamente frente a los convencionales, se aborda el comportamiento hemodinámico de los mismos. Concretamente, se comparó el patrón de flujo en un modelo de bifurcación coronaria con los nuevos stents (Stentys) y los convencionales. Se estudiaron cuatro modelos, a saber, stent simple en la rama principal, stent simple en la rama secundaria, culotte desplegando el primer stent en la rama principal y culotte desplegando el primer stent en la rama secundaria. La bifurcación estudiada presenta un ángulo de apertura de 45º y la relación de diámetros de las ramas hija se ajustaron de acuerdo a la ley de Finet. Se recogieron resultados experimentales en el laboratorio y se corrieron simulaciones numéricas con Ansys Fluent paralelamente. Las magnitudes que se tuvieron en cuenta con el fin de ubicar las regiones potencialmente ateroscleróticas fueron los esfuerzos cortantes, vorticidad y caída de presión. ABSTRACT Nowadays, restenosis after percutaneous dilation is the major drawback of coronary angioplasty. It represents a special form of atherosclerosis due to the healing process secondary to extensive vessel trauma induced after intracoronary balloon inflation. The use of coronary stents may decrease the incidence of this phenomenon. Unfortunately, intra-stent restenosis still occurs in 20-30% of the cases following the stent implantation. Most experiments suggest a correlation between low wall shear stress and wall thickness. The preferential locations for the atherosclerotic plaque are bifurcations. The objective of this work is to analyze the local hemodynamic changes caused in a coronary bifurcation by three different stenting techniques: simple stenting of the main vessel, simple stenting of the main vessel with kissing balloon in the side branch and culotte. To carry out this study an idealized geometry of a coronary bifurcation is used, and two bifurcation angles, 45º and 90º, are chosen as representative of the wide variety of real configurations. Both numerical simulations and experimental measurements are performed. First, steady simulations are carried out with the commercial code Ansys-Fluent, then, experimental measurements with PIV (Particle Image Velocimetry), obtained in the laboratory, are used to validate the numerical simulations. The steady computational simulations show a good overall agreement with the experimental data. Then, pulsatile flow is considered to take into account the transient effects. The time averaged wall shear stress, oscillatory shear index and pressure drop obtained numerically are used to compare the behavior of the stenting techniques. In a second step, the rheologic behavior of blood was considered comparing Newtonian, Carreau and Power Law models. Finally, as a result of previous investigations with conventional stents and after the recent emergence of several devices specifically designed for coronary bifurcations angioplasty, the hemodynamic performance of these new devices (Stentys) was compared to conventional ones and techniques in a coronary bifurcation model. Four different stenting techniques: simple stenting of the main vessel, simple stenting of the side vessel, culotte deploying the first stent in the main vessel and culotte deploying the first stent in the side vessel have been considered. To carry out this study an idealized geometry of a coronary bifurcation is used. A 45 degrees bifurcation angle is considered and the daughter branches diameters are obtained according to the Finet law. Both experiments in the laboratory and numerical simulations were used , focusing on important factors for the atherosclerosis development, like the wall shear stress, the oscillation shear index, the pressure loss and the vorticity.

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SUNRISE is a balloon-borne solar telescope flown with a long-duration balloon by NASA's Columbia Scientific Balloon Facility team from Esrange (Swedish Space Corporation), on 8 June 2009. SUNRISE has been a challenging mission from the thermal point of view because of its size and power dissipation. Thus, a dedicated thermal analysis has been carried out to find a solution that allows all the devices to be kept within their appropriate temperature ranges, without exceeding the allowable temperature gradients, critical for optical devices. In this article, the thermal design of SUNRISE is described. A geometrical mathematical model and a thermal mathematical model of the whole system have been set up for the different load cases in order to obtain the temperature distribution and gradients in the system. Some trade-offs have been necessary to fulfil all the thermal requirements. The thermal hardware used to achieve it is described. Finally, the temperatures obtained with the models have been compared with flight data.

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SUNRISE is a balloon-borne solar telescope flown with a long-duration balloon by NASA's Columbia Scientific Balloon Facility team from Esrange (Swedish Space Corporation), on 8 June 2009. SUNRISE has been a challenging mission from the thermal point of view because of its size and power dissipation. Thus, a dedicated thermal analysis has been carried out to find a solution that allows all the devices to be kept within their appropriate temperature ranges, without exceeding the allowable temperature gradients, critical for optical devices. In this article, the thermal design of SUNRISE is described. A geometrical mathematical model and a thermal mathematical model of the whole system have been set up for the different load cases in order to obtain the temperature distribution and gradients in the system. Some trade-offs have been necessary to fulfil all the thermal requirements. The thermal hardware used to achieve it is described. Finally, the temperatures obtained with the models have been compared with flight data.

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The thermal design of stratospheric balloon payloads usually focuses on the cruise phase of the missions, that is, the floating altitude conditions. The ascent phase usually takes between 2 and 4 h, a very small period compared to the duration of the whole mission, which can last up to 4 weeks. However, during this phase payloads are subjected to very harsh conditions due mainly to the convective cooling that occurs as the balloon passes through the cold atmosphere, with minimum temperatures in the tropopause. The aim of this work is to study the thermal behaviour of a payload carried by a long duration balloon during the ascent phase. Its temperature has been calculated as a function of the altitude from sea level to floating conditions. To perform this analysis it has been assumed that the thermal interactions (convection and radiation) depend on the altitude, on the environmental conditions (which in turn depend also on the altitude) and on the temperature of the system itself. The results have been compared with the measurements taken during the SUNRISE test flight, launched in October 2007 by CSBF from Fort Sumner (New Mexico).