| 摘要 |
An outflow valve for an aircraft has a frame for arrangement in an opening of an outer shell of the aircraft, a first flap pivotably arranged in the frame for controlling a flow cross-section of at least one first inflow opening and at least one outflow opening. To achieve a simplified construction of the ventilation system of the aircraft, the outflow valve has a second inflow opening configured to be closable by means of a drivable adjustable member.
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