A discharge valve for an aircraft includes a cylindrical body having an inlet and an outlet, a first valve, and a second valve arranged inside the body. The first and the second valves are rotatable around a first axle and a second axle, respectively, between a closed position and an open position. A mechanism for locking the second valve in the closed position includes a control lever arranged around a third axle, an interface arranged on the second valve, and a device for rotating the third axle. The control lever is rotatably movable around the third axle between an unlocking position, in which the interface is in abutment against the drive device, and a locking position, in which the interface is engaged in the drive device.
VANNE DE VIDANGE POUR AERONEF ET PROCEDE ASSOCIE
DRAIN VALVE FOR AIRCRAFT AND CORRESPONDING METHOD
ABLASSVENTIL FÜR LUFTFAHRZEUGE UND ENTSPRECHENDES VERFAHREN
25.06.2025
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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