Evaluation of functionalized coatings for the prevention of ice accretion by using icing wind tunnel tests

dc.contributor.authorRivero Fuente, Pedro J.
dc.contributor.authorRodríguez Trías, Rafael
dc.contributor.authorLarumbe Abuin, Silvia
dc.contributor.authorMonteserín, María
dc.contributor.departmentIngeniaritzaeu
dc.contributor.departmentInstitute for Advanced Materials and Mathematics - INAMAT2en
dc.contributor.departmentIngenieríaes_ES
dc.contributor.funderUniversidad Pública de Navarra / Nafarroako Unibertsitate Publikoa, PJUPNA1929es
dc.date.accessioned2021-01-11T11:43:53Z
dc.date.available2021-01-11T11:43:53Z
dc.date.issued2020
dc.description.abstractIce accretion presents serious safety issues, as airplanes are exposed to supercooled water droplets both on the ground and while flying through clouds in the troposphere. Prevention of icing is a main concern for both developers and users of aircraft. The successful solution of this problem implies the combination of active and passive methods and the use of advanced sensors for early detection of icing and monitoring of ice accretion and de-icing processes. This paper focuses on the development of passive solutions. These include advanced anti-icing coatings deposited by a variety of chemical methods including sol-gel, advanced paints based on polyester combined with fluorinated derivatives and applied by electrostatic spray deposition and conventional silicone-based paints modified by adding alumina nanoparticles. Water contact angle has been measured in all cases, demonstrating the hydrophobic character of the coatings. An ice accretion test has been carried out in a laboratory scale icing wind tunnel (IWT) located in a cold climate chamber. Three different studies have been undertaken: ice accretion measurement, durability of the anti-icing behavior after several icing/de-icing cycles and ice adhesion testing by means of the double lap shear test (DLST) methodology. All the studied coatings have shown significant anti-icing behavior which has been maintained, in some cases, beyond 25 cycles. Although these results are still far from any possible application for aeronautic components, they provide interesting insights for new developments and validate the laboratory scale tests.en
dc.description.sponsorshipThis research was funded by the Ministerio de Ciencia, Innovación y Universidades -Retos (Project RTI2018-096262-B-C41–MAITAI, Multidisciplinary Approach for the Implementation of new Technologies to RTI2018-096262-B-C41–MAITAI, Multidisciplinary Approach for the Implementation of new Technologies to prevent Accretion of Ice on aircraft), and by the Public University of Navarre (Project PJUPNA1929).en
dc.format.extent17 p.
dc.format.mimetypeapplication/pdfen
dc.identifier.doi10.3390/coatings10070636
dc.identifier.issn2079-6412
dc.identifier.urihttps://academica-e.unavarra.es/handle/2454/38982
dc.language.isoengen
dc.publisherMDPIen
dc.relation.ispartofCoatings, 2020, 10(7):636en
dc.relation.publisherversionhttps://doi.org/10.3390/coatings10070636
dc.rights© 2020 by the author. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license.en
dc.rights.accessRightsinfo:eu-repo/semantics/openAccess
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.subjectIce accretionen
dc.subjectIce adhesionen
dc.subjectIcing wind tunnelen
dc.subjectHydrophobicityen
dc.subjectNanoparticlesen
dc.subjectCoatingsen
dc.titleEvaluation of functionalized coatings for the prevention of ice accretion by using icing wind tunnel testsen
dc.typeinfo:eu-repo/semantics/article
dc.type.versioninfo:eu-repo/semantics/publishedVersion
dspace.entity.typePublication
relation.isAuthorOfPublicationccf8da2b-8e86-4e57-835a-358562d70571
relation.isAuthorOfPublicationc2c9f4e4-e7ea-4d7b-8cf6-a529e456dc3e
relation.isAuthorOfPublicationa65f5238-3c22-46ad-a982-34cf82016864
relation.isAuthorOfPublication.latestForDiscoveryccf8da2b-8e86-4e57-835a-358562d70571

Files

Original bundle
Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
2020100151_Rivero_EvaluationFunctionalized.pdf
Size:
6.25 MB
Format:
Adobe Portable Document Format
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.71 KB
Format:
Item-specific license agreed to upon submission
Description: