A fuel tank (10) for an aircraft (1) and an aircraft, the fuel tank comprising a fuel pumping system comprising:-a set of hoses (12a... 12d), the first ends of which are distributed over a lower portion (28) of the tank; -a manifold (16) to which the second ends of different hoses (12a... 12d) of the set are connected as input, the output of which is connected to a fuel pump (18); -a fuel level sensor (14a... 14d) associated with each hose of the set of hoses and placed near a first end of said hose; and-a valve associated with each hose and controlled by a control system (24) in such a way that when a fuel level sensor associated with the hose detects a low fuel level, the valve is controlled into a closed position and otherwise into an open position.
一种用于飞行器(1)的燃料箱(10)及飞行器,该燃料箱包括燃料泵送系统,该燃料泵送系统包括:‑一组软管(12a…12d),该组软管的第一端分布在箱的下部部分(28)上;‑歧管(16),该组软管中的不同软管(12a…12d)的第二端作为输入连接到该歧管,该歧管的输出连接到燃料泵(18);‑燃料液位传感器(14a…14d),该燃料液位传感器与该组软管中的每根软管相关联,并且被放置在所述软管的第一端附近;以及‑阀,该阀与每根软管相关联,并由控制系统(24)控制,其方式为使得当与该软管相关联的燃料液位传感器检测到低燃料液位时,该阀受控进入关闭位置,否则该阀受控进入打开位置。
Fuel tank for aircraft and aircraft
用于飞行器的燃料箱及飞行器
2024-04-09
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Aircraft fuel tank access cover and an aircraft fuel tank
European Patent Office | 2015
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