The invention relates to a rotary wing aircraft (1) with a fuselage (1a) that is equipped with at least one rail (2b), comprising at least one sliding element (4), in particular a sliding door or a sliding window, that is slidably supported by the at least one rail (2b), wherein the at least one sliding element (4) is at least slidable along the at least one rail (2b) by means of an opening sliding movement into an opening movement direction (4c) from a fully closed position into a fully opened position, wherein a dampening unit (6) is provided that dampens the opening sliding movement of the at least one sliding element (4) upon reaching of the fully opened position.
A ROTARY WING AIRCRAFT WITH A SLIDING ELEMENT, IN PARTICULAR A SLIDING DOOR OR A SLIDING WINDOW
DREHFLÜGELFLUGZEUG MIT EINEM GLEITELEMENT, INSBESONDERE EINER SCHIEBETÜR ODER EINEM SCHIEBEFENSTER
AÉRONEF À VOILURE TOURNANTE AYANT UN ÉLÉMENT COULISSANT, EN PARTICULIER UNE PORTE COULISSANTE OU UNE FENÊTRE COULISSANTE
26.10.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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