The invention discloses a water tank pressurization system for an airplane. Comprising a water tank, a pressure switch, an air header pipe assembly, an air compression pump and a controller. The upper part of the water tank is provided with a pressure switch and an air inlet, the air inlet is connected with the air header pipe assembly, and the pressure switch is electrically connected with the controller; the air header pipe assembly comprises a reciprocating valve, two inlet ends of the reciprocating valve are connected with an engine air entraining system and an air compression pump respectively, and an outlet end of the reciprocating valve is connected with an air inlet of the water tank. And the air compression pump is electrically connected with the controller. According to the invention, the gas pressure in the water tank on the airplane can be monitored, and the pressure stability of pressurized gas in the water tank is ensured.
本发明公开了一种飞机用水箱增压系统。包括:水箱、压力开关、空气总管组件、空气压缩泵和控制器;水箱上部安装压力开关,并设有进气口,进气口与空气总管组件连接,压力开关与控制器电连接;空气总管组件包括往复阀,往复阀的两个入口端分别连接发动机引气系统和空气压缩泵,往复阀的出口端与水箱的进气口连接;空气压缩泵与控制器电连接。本发明能实现飞机上水箱内气体压力的监控及保证水箱内增压气体压力的稳定。
Water tank pressurization system for airplane
一种飞机用水箱增压系统
2023-03-28
Patent
Electronic Resource
Chinese
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