The final objective of the study herein reported is the preliminary evaluation of the capability of an original, real-time SHM system applied to a full-scale wing-box section as a significant aircraft component, during an experimental campaign carried out at the Piaggio Lab in Villanova D'Albenga, Italy. In previous works, the authors have shown that such a system could be applied to composite beams, to reveal damage along the bonding line between a longitudinal stiffening element and the cap. Utilizing a suitable scaling process, such work has then been exported to more complex components, in order to confirm the outcomes that were already achieved, and, possibly, expanding the considerations that should drive the project towards an actual implementation of the proposed architecture.
View Article and Find Full Text PDFThe present paper reports the outcomes of activities concerning a real-time SHM system for debonding flaw detection based on ground testing of an aircraft structural component as a basis for condition-based maintenance. In this application, a damage detection method unrelated to structural or load models is investigated. In the reported application, the system is applied for real-time detection of two flaws, kissing bond type, artificially deployed over a full-scale composite spar under the action of external bending loads.
View Article and Find Full Text PDF1. The effects of ATP, the stable ATP analogues alpha,beta-methylene ATP (alpha,beta-mATP), 2-methylthioATP (2meSATP) and adenosine tetraphosphate (ATP4), the pyrimidine nucleotide uridine 5'-triphosphate (UTP) and the alpha1-adrenoceptor agonist phenylephrine were examined on the isolated perfused uterine vasculature of dioestrous, oestradiol-treated, dexamethasone-treated and late-pregnant guinea-pigs. 2.
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