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DIMES SIGNED

Development of Integrated MEasurement Systems

Total Cost €

EC-Contrib. €

Partnership

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DIMES project word cloud

Explore the words cloud of the DIMES project. It provides you a very rough idea of what is the project "DIMES" about.

shown propagation sensor amalgamate philosophy bench board crack structure integrating outcome primary least demonstrated delamination acquisition demonstration line metallic aircraft structural diverse conduct innovative data innovations tests representing evaluation incorporates emission detect instructive passenger caused destructive monitoring techniques structures acoustic composite generation prototype technologies designed independent disturbance infrared gauges strain detecting health smaller assembly mature damage track consisting disruptive cs2 sensors capability cracks technique trl

Project "DIMES" data sheet

The following table provides information about the project.

Coordinator	THE UNIVERSITY OF LIVERPOOL Organization address address: BROWNLOW HILL 765 FOUNDATION BUILDING city: LIVERPOOL postcode: L69 7ZX website: www.liverpool.ac.uk contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.
Coordinator Country	United Kingdom [UK]
Total cost	1˙320˙261 €
EC max contribution	1˙199˙901 € (91%)
Programme	1. H2020-EU.3.4.5.4. (ITD Airframe)
Code Call	H2020-CS2-CFP07-2017-02
Funding Scheme	CS2-IA
Starting year	2019
Duration (year-month-day)	from 2019-01-01 to 2020-12-31

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	THE UNIVERSITY OF LIVERPOOL THE UNIVERSITY OF LIVERPOOL Organization address address: BROWNLOW HILL 765 FOUNDATION BUILDING city: LIVERPOOL postcode: L69 7ZX website: www.liverpool.ac.uk contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UK (LIVERPOOL)	coordinator	505˙936.00
2	EIDGENOSSISCHE MATERIALPRUFUNGS- UND FORSCHUNGSANSTALT EIDGENOSSISCHE MATERIALPRUFUNGS- UND FORSCHUNGSANSTALT Organization address address: UEBERLANDSTRASSE 129 city: DUBENDORF postcode: 8600 website: www.empa.ch contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	CH (DUBENDORF)	participant	413˙125.00
3	Dantec Dynamics GmbH Dantec Dynamics GmbH Organization address address: KAESSBOHRERSTRASSE 18 city: Ulm postcode: 89077 website: www.dantecdynamics.com contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (Ulm)	participant	201˙075.00
4	STRAIN SOLUTIONS LIMITED STRAIN SOLUTIONS LIMITED Organization address address: DUNSTON ROAD DUNSTON INNOVATION city: CHESTERFIELD postcode: S41 8NG website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UK (CHESTERFIELD)	participant	79˙765.00

Map

Project objective

The aim of the project is to develop advanced integrated testing methods that have the capability to detect a crack or delamination in a metallic or composite structure and have the potential to be deployed as part of an on-board structural health monitoring system for passenger aircraft. The proposal incorporates a new philosophy for monitoring damage in which the disturbance to the strain field in the structure caused by the damage is used to identify significant damage and to track its propagation. Recently, this approach has been demonstrated to be at least as effective in composite structures as traditional non-destructive evaluation techniques and, in CS2 project INSTRUCTIVE using infrared technology, it has been shown to be capable of identifying smaller cracks in metallic structures than any other available technique. In this project, it is proposed to amalgamate these innovations with more established techniques, such as strain gauges and acoustic emission, and to demonstrate an integrated testing method. The objectives are designed to mature technologies from TRL 4 to 6 that are likely to have a disruptive impact on the structural health monitoring of next generation large passenger aircraft The objectives are: i) to develop a robust and innovative concept for integrating a diverse set of sensors and data acquisition systems for detecting and monitoring damage in an aircraft assembly; ii) to produce an integrated system of sensors and data acquisition systems deployed on a test bench representing an aircraft assembly, and; iii) to conduct prototype demonstration and evaluation tests of the integrated system and test bench using independent systems. The primary outcome will be the demonstration, on a test bench consisting of an aircraft assembly, of an integrated measurement system for ‘on-line’ detecting and monitoring damage based on a diverse range of sensor systems.

Publications

List of publications.
year	authors and title	journal	last update
2019	Melissa Weihrauch, Ceri Middleton, Richard J Greene and Eann A Patterson Low-cost thermoelastic stress analysis published pages: , ISSN: , DOI:	2019 SEM Annual Conference & Exposition on Experimental & Applied Mechanics, Reno NV 3-6 June 2019	2020-02-05

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The information about "DIMES" are provided by the European Opendata Portal: CORDIS opendata.