A device comprises an active element panel (14) and a pressure sensitive adhesive layer (16). The pressure sensitive adhesive layer is bonded to the active element panel and defines a bonding surface (22) that is bondable to an aircraft structure. The pressure sensitive adhesive layer comprises a mixture of a pressure sensitive adhesive and a solid solvent.In a preferred embodiment, the solid solvent is selected from a group consisting of carboxylic acids and L-lactide.
THERMALLY SWITCHABLE HIGH SHEAR PRESSURE SENSITIVE ADHESIVE
THERMISCH SCHALTBARER DRUCKEMPFINDLICHER KLEBSTOFF MIT HOHEN SCHEREIGENSCHAFTEN
ADHÉSIF SENSIBLE À LA PRESSION DE CISAILLEMENT ÉLEVÉE COMMUTABLE THERMIQUEMENT
15.04.2020
Patent
Elektronische Ressource
Englisch
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