MASS

Load Monitoring of Aerospace Structures Through Shape Changes

Coordinatore	TECHNISCHE UNIVERSITEIT DELFT    more  Organization address address: Stevinweg 1 city: DELFT postcode: 2628 CN contact info Titolo: Mr. Nome: Martin Cognome: Hoekstra Email: send email Telefono: 31152785214
Nazionalità Coordinatore	Netherlands [NL]
Totale costo	100˙000 €
EC contributo	100˙000 €
Programma	FP7-PEOPLE Specific programme "People" implementing the Seventh Framework Programme of the European Community for research, technological development and demonstration activities (2007 to 2013)
Code Call	FP7-PEOPLE-2013-CIG
Funding Scheme	MC-CIG
Anno di inizio	2013
Periodo (anno-mese-giorno)	2013-10-01   -   2017-09-30

 Partecipanti

#	participant	country	role	EC contrib. [€]
1	TECHNISCHE UNIVERSITEIT DELFT  Organization address address: Stevinweg 1 city: DELFT postcode: 2628 CN contact info Titolo: Mr. Nome: Martin Cognome: Hoekstra Email: send email Telefono: 31152785214	NL (DELFT)	coordinator	100˙000.00

Mappa

 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

 Obiettivo del progetto (Objective)

'Aerospace structures age and degrade due to regular service usage which fleet operators are tasked with monitoring. Understanding the structural problems that may arise requires a comprehensive vision of the loads supported by the structure, the initial structural conditions, environmental effects on the structural performance, and the material conditions of the components composing the structure. Furthermore, all of these factors can interact, making it difficult to assess the degradation, and more importantly determining the remaining useful structural life. Traditionally, fleet operators monitored and made decisions for their fleet based on an average or typical usage profile, thus neglecting variations within the fleet and within the factors affecting the fleet. The primary objective of this proposal is to Monitor Aerospace Structural Shapes (MASS) in order to compute strain and stress distribution on the structure in real or quasi‐real time.'