An aircraft door system (1) is disclosed which includes a frame structure (10) defining an aperture (11), an aircraft door (20) including an area member (21) formed as a multi-layered composite structure including multiple actuator layers (21A; 21B) each of which comprising an electroactive polymer material that is excitable to an excited state by an electrical voltage, and an electrical connection interface (22), and a pivoting device (30) being coupled to the frame structure (10) and the aircraft door (20). Further, a method for opening and closing an aircraft door (20) and an use of an area member (21) including an electroactive polymer as an aircraft door (20) disclosed.
AIRCRAFT DOOR SYSTEM AND METHOD FOR OPENING AND CLOSING AN AIRCRAFT DOOR
FLUGZEUGTÜRSYSTEM UND VERFAHREN ZUM ÖFFNEN UND SCHLIESSEN EINER FLUGZEUGTÜR
SYSTÈME DE PORTE D'AÉRONEF ET PROCÉDÉ D'OUVERTURE ET DE FERMETURE D'UNE PORTE D'AÉRONEF
16.05.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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