DISCHARGE VALVE FOR AN AIRCRAFT AND ASSOCIATED METHOD

    公开(公告)号:US20230406507A1

    公开(公告)日:2023-12-21

    申请号:US18248550

    申请日:2021-10-15

    CPC classification number: B64D11/02

    Abstract: 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.

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