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Summary: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.
Bibliography:Application Number: BR2008PI15107