The present invention relates to an erosion resistant construction comprising an element of an aircraft comprising an aircraft skin segment having an external surface, and a deicing mechanism associated with said aircraft skin segment capable of heating said external surface to temperatures in excess of 65°C, a tape comprising at least one layer comprising a crosslinked elastomeric polymer, and an adhesive layer, wherein the tape is bonded to the external surface of the aircraft skin segment by the adhesive layer.
EROSION RESISTANT FILMS FOR USE ON HEATED AERODYNAMIC SURFACES
EROSIONSRESISTENTE FILME ZUR VERWENDUNG AUF ERHITZTEN AERODYNAMISCHEN FLÄCHEN
FILMS RÉSISTANTS À L'ÉROSION UTILISABLES SUR DES SURFACES AÉRODYNAMIQUES PORTÉES À HAUTE TEMPÉRATURE
2016-10-26
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / C08G MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING CARBON-TO-CARBON UNSATURATED BONDS , Makromolekulare Verbindungen, anders erhalten als durch Reaktionen, an denen nur ungesättigte Kohlenstoff-Kohlenstoff-Bindungen beteiligt sind / C09J ADHESIVES , Klebstoffe |
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