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    • 2. 发明公开
    • FUEL TANK OF AIRCRAFT
    • TREIBSTOFFTANKFÜREIN LUFTFAHRZEUG
    • EP2354003A1
    • 2011-08-10
    • EP09830233.4
    • 2009-06-24
    • Mitsubishi Heavy Industries, Ltd.
    • YAMAGUCHI, HiroakiKAMINO, YuichiroHASHIGAMI, TooruOGURI, Kazuyuki
    • B64D37/32B64D45/02
    • B64D37/32B64C3/34B64D45/02
    • An aircraft fuel tank that is capable of suppressing the occurrence of sparks on a pipe caused by a lightning current through the pipe during a lightning strike, and also suppressing static electricity charging of a pipe caused by flow electrification generated by the fuel. An aircraft fuel tank (1) in which a storage section is formed using a conductive upper skin (5), a conductive lower skin (7) and conductive spars (9), the tank comprising: pipes inside the tank, such as a refuel pipe (17), an engine feed pipe (19) and an inert gas pipe (21), which are disposed inside the storage section and are earthed (27) at a plurality of locations, and pipe outer surface layers (31) having semiconductor properties that are formed in an integrated manner on the outer surfaces of the pipes inside the tank such as the replenishing pipe (17), the supply pipe (19) and the gas pipe (21).
    • 一种飞机燃料箱,其能够抑制由于在雷击期间通过管道的雷电流引起的管道上的火花的发生,并且还抑制由燃料产生的流动电气引起的管道的静电充电。 一种飞机燃料箱(1),其中使用导电上皮(5),导电下皮(7)和导电柱(9)形成存储部分,所述罐包括:罐内的管,例如加油 管道(17),发动机供给管(19)和惰性气体管道(21),其设置在存储部分的内部并在多个位置处接地(27),以及具有半导体的管外表面层 在补充管(17),供给管(19)和气管(21)内的槽内的管的外表面上一体形成的特性。