Proof of Concept of Impact Detection in Composites Using Fiber Bragg Grating Arrays

Impact detection in aeronautical structures allows predicting their future reliability and performance. An impact can produce microscopic fissures that could evolve into fractures or even the total collapse of the structure, so it is important to know the location and severity of each impact. For this purpose, optical fibers with Bragg gratings are used to analyze each impact and the vibrations generated by them. In this paper it is proven that optical fibers with Bragg gratings can be used to detect impacts, and also that a high-frequency interrogator is necessary to collect valuable information about the impacts. The use of two interrogators constitutes the main novelty of this paper.

Nuevos phased arrays

[ES]El sistema PAMELA III, con sus correspondientes phased arrays, se diseñó para la detección de daños en aeronaves mediante la tecnología SHM (structural health monitoring). Sin embargo, según los estudios del profesor Tadeusz Stepinski, la distribución de los piezoélectricos utilizada en estos phase arrays producen interferencias. Por ello, este proyecto se basa en el diseño de cuatro phased arrays diferentes, utilizando una de las distribuciones de piezoélectricos estudiada por el profesor Tadeusz. La distribución utilizada es la de cross-shaped (en forma de cruz), con lo que se consigue disminuir las interferencias producidas en los antiguos phased arrays. Además, se ha producido un diseño que es compatible tanto con PAMELA III, como con una futura actualización a PAMELA IV. Con lo que se ha conseguido que se pueda aumentar el tamaño de almacenamiento de la memoria utilizada cambiando la tecnología 1-wire por la de I2C, que sería utilizada solo en el sistema PAMELA IV. Aparte del diseño de los PCBs, también se han diseñado unas piezas de plástico que aportan rigidez a los phased arrays y además, hace que la parte inferior de la tarjeta quede toda a la misma altura y no sobresalgan los piezoélectricos, con lo que aumentará la facilidad de instalación.

Microcantilever arrays functionalised with spiropyran photoactive moieties as systems to measure photo-induced surface stress changes

[EN] Herein we investigate the feasibility of detecting photo-induced surface stress changes using the deflection response of cantilevers. For this purpose, silicon microcantilevers have been functionalised with spiropyran photochromic molecules, using both a monolayer and a polymeric brushes approach. Uponultraviolet light irradiation, the spiropyran unit is converted to the merocyanine form due to the photo-induced cleavage of the Cspiro-O bond. The two forms of the molecule have dramatically different charge,polarity and molecular conformations. This makes spiropyrans an ideal system to study the correlation between photo-induced molecular changes and corresponding changes in surface stress. Our investigations include monitoring the changes in static cantilever deflection, and consequently, surface stress of the spiropyran functionalised cantilevers on exposure to ultraviolet light. Cantilever deflection data reveals that ultraviolet induced conformational changes in the spiropyran moiety cause a change incompressive surface stress and this varies with the type of functionalisation method implemented. The change in surface stress response from the spiropyran polymer brushes functionalised cantilevers gives an average surface stress change of 98 Nm−1(n = 24) while the spiropyran monolayer coated cantilevers have an average surface stress change of about 446 Nm−1(n = 8) upon irradiation with UV light.