PLASMACLEAN

Surface mapping and control during atmospheric plasma treatments

 Coordinatore UNIVERSITY COLLEGE DUBLIN, NATIONAL UNIVERSITY OF IRELAND, DUBLIN 

 Organization address address: BELFIELD
city: DUBLIN
postcode: 4

contact info
Titolo: Dr.
Nome: Denis
Cognome: Dowling
Email: send email
Telefono: 35317161747

 Nazionalità Coordinatore Ireland [IE]
 Totale costo 189˙852 €
 EC contributo 142˙389 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2010-05
 Funding Scheme JTI-CS
 Anno di inizio 2011
 Periodo (anno-mese-giorno) 2011-12-01   -   2013-07-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    UNIVERSITY COLLEGE DUBLIN, NATIONAL UNIVERSITY OF IRELAND, DUBLIN

 Organization address address: BELFIELD
city: DUBLIN
postcode: 4

contact info
Titolo: Dr.
Nome: Denis
Cognome: Dowling
Email: send email
Telefono: 35317161747

IE (DUBLIN) coordinator 142˙389.60

Mappa


 Word cloud

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

contaminants    spectroscopy    diagnostic    real    pressure    composite    adhesive    bonds    contact    organic    oes    adhesion    treatment    combined    contaminant    time    aerospace    mapping    surfaces    atmospheric    surface    composites    integrity    materials    treatments    performance    removal    chemical    plasma    technique    addition    techniques   

 Obiettivo del progetto (Objective)

'The objective of this project is to develop a novel non contact diagnostic technique for the determination of the chemical species present on the surface of metallic materials and composites. The use of atmospheric plasma techniques for the removal of contaminants will be investigated. The performance of the novel non contact diagnostic technique will be benchmarked based on conventional surface chemical analysis techniques (i.e. XPS), in addition to paint / sealant adhesion testing. It is planned to use LabVIEW software to facilitate real-time process control based on the output data provided by the non contact surface analysis technique.'

Introduzione (Teaser)

Removal of organic contaminants from composite surfaces is critical to the integrity of adhesive bonds. EU funding supported development of novel process control technology to ensure performance of a promising surface treatment technique.

Descrizione progetto (Article)

Failure of bonds on titanium and composite materials used for structural components in the aerospace sector can have catastrophic results. Atmospheric pressure plasma jets that generate plasmas at ambient temperature and pressure are increasingly used to remove organic contaminants to increase bond integrity. However, as a relatively new technique, there is currently no available process control technology.

EU-funded scientists investigated the feasibility of organic contaminant removal via atmospheric plasma treatments, simultaneously validating appropriate technology for process control. Within the scope of the project 'Surface mapping and control during atmospheric plasma treatments' (PLASMACLEAN), researchers evaluated reflectance infra-red spectroscopy combined with optical emission spectroscopy (OES) and acoustic techniques. Composites were then spray-painted followed by adhesion testing to determine if the plasma-treated surfaces meet requirements for adhesive bonding.

The study supported the excellent potential of atmospheric plasma treatment combined with OES for controlled contaminant removal during manufacture of aerospace composites. In addition, the team developed the required surface mapping and control technology to accompany the OES during atmospheric plasma treatment. The OES tool can also identify any thermal damage to the composite caused by the air jet.

These advances should lead to real-time process control of an important new technique to enhance the integrity of adhesive bonds. Outcomes are set to have a positive impact on high-end manufacturing industries such as aviation as well as on the safety of large composite structures.

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