发明名称 Aircraft fuel tank system
摘要 An aircraft fuel tank system is disclosed in which a vent tank is provided with a compact vent pipe comprising one or more built-in flame barrier elements providing high liquid fuel outflow rate.
申请公布号 US9440728(B2) 申请公布日期 2016.09.13
申请号 US201012870496 申请日期 2010.08.27
申请人 AIRBUS OPERATIONS LIMITED 发明人 Lynas Christopher;James Peter William;Melville Robert A
分类号 B65D90/22;B64C3/34;B64D37/32 主分类号 B65D90/22
代理机构 Hauptman Ham, LLP 代理人 Hauptman Ham, LLP
主权项 1. An aircraft fuel tank system comprising: one or more aircraft fuel tanks for holding and supplying aircraft fuel to aircraft engines within said aircraft; an aircraft vent tank comprising an inlet connected to said one or more fuel tanks and an ullage vent means in a lower surface of said aircraft fuel tank, said aircraft vent tank being arranged to provide a predetermined maximum fuel capacity and having a minimal ullage at said maximum fuel capacity; a vent pipe having a first open end in fluid communication with said ullage vent means and a second open end positioned within said minimal ullage of said aircraft vent tank, said vent pipe being arranged to provide a substantially direct nominally vertical fluid flow path between said minimal ullage and said ullage vent means; and flame barrier means arranged within said vent pipe so as to provide a barrier to ingress to said vent tank of a flame front external to said vent tank and to enable egress of liquid fuel from said vent tank though said ullage vent means via said vent pipe.
地址 Bristol GB