Aircraft door including a support arm (10) connecting a door leaf (5) and a door frame (13), the locking/unlocking mechanism of which includes: a control shaft (17) extending along a substantially vertical axis; a guide track (29); an actuating finger (32) attached to the support arm (10); the locking/unlocking mechanism having: an actuating configuration in which the actuating finger (32) is inserted into the guide track (29), the rotation of the control shaft (17) causing the actuating finger (32) to move along the guide track (29); a release configuration in which the actuating finger (32) is outside the guide track (29).
PORTE D'AERONEF A MECANISME DE COMMANDE VERTICAL
AIRCRAFT DOOR WITH VERTICAL CONTROL MECHANISM
FLUGZEUGTÜR MIT VERTIKALEM STEUERMECHANISMUS
2023-08-09
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |