The invention relates to a discharge device for a tank of an aircraft, comprising: a discharge duct (18); a drain valve (20) positioned between the upstream end and the downstream end of the drain conduit (18); a housing (22) sized to accommodate at least the downstream end (18.1) of the discharge conduit (18); and a flap (24) movable between an open position and a closed position in which the flap (24) closes the housing (22). According to the invention, the flap (24) comprises a liquid reservoir (34) positioned on the inner face (F24) thereof, which liquid reservoir leads to the discharge duct (18) when the flap (24) is in the closed position. The liquid reservoir (34) is designed to collect and store any liquid flowing out of the drain conduit (18) in the event of leakage from the drain valve. The invention also relates to an aircraft comprising such a discharge device.
本发明涉及一种用于飞行器的箱的排放装置,该排放装置包括:排放管道(18);排放阀(20),该排放阀定位在排放管道(18)的上游端与下游端之间;壳体(22),该壳体的尺寸被确定为至少容纳所述排放管道(18)的下游端(18.1);以及翻盖(24),该翻盖能够在打开位置与关闭位置之间运动,在该关闭位置,翻盖(24)封闭壳体(22)。根据本发明,翻盖(24)包括定位在其内部面(F24)上的液体储存器(34),当翻盖(24)处关闭位置时,排放管道(18)通向该液体储存器。液体储存器(34)被设计成在从排放阀泄漏的情况下收集和储存从排放管道(18)流出的任何液体。本发明还涉及一种包括这种排放装置的飞行器。
Device for discharging waste water tank and aircraft with discharging device
用于对废水箱进行排放的装置及具有该排放装置的飞行器
2024-08-30
Patent
Electronic Resource
Chinese
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