A sealed component assembly within an aircraft, comprising first 10 and second 12 components each facing surfaces, and a sealing member 20 extending between the facing surfaces. The sealing member includes a conductive portion 22 sandwiched between first 24 and second 26 sealing portions. The sealing portions extend between and in contact with the facing surfaces, and are made of a sealing material. The conductive portion is in contact with conductive regions of the facing surfaces and defines an electrical connection therebetween. The conductive portion is more conductive than the sealing portions. In a particular embodiment, the components are a floor panel and a floor beam. A sealing member 20 for a connection between two aircraft components is also discussed.
CONDUCTIVE SEALING MEMBER
LEITENDES DICHTUNGSELEMENT
ÉLÉMENT D'ÉTANCHÉITÉ CONDUCTEUR
04.09.2019
Patent
Elektronische Ressource
Englisch