发明名称 BAFFLE
摘要 BAFFLE Disclosed is a baffle (40) for locating in a tank (16) for containing liquid (e.g. an aircraft fuel tank). The baffle (40) is a tubular member through which a liquid may flow. The baffle (40) comprises: a first tubular portion (42) providing a tubular outer wall, and a second tubular portion (44) located within the first tubular portion (42) and providing a tubular inner wall. The first and second tubular portions (42, 44) are substantially parallel. The first and second tubular portions (42, 44) are spaced apart to define a chamber (46)therebetween. The baffle (42, 44) further comprises radial side walls between the first and second tubular portions (42, 44) such that the chamber (46) is a sealed chamber. The chamber (46) may be filled with a compressible gas or gaseous mixture.
申请公布号 US2017050742(A1) 申请公布日期 2017.02.23
申请号 US201515307419 申请日期 2015.05.06
申请人 BAE Systems PLC 发明人 Bingham Christopher Steven;Irwin Andrew James
分类号 B64D37/32;B60K15/077;F41H5/04;B64D37/08 主分类号 B64D37/32
代理机构 代理人
主权项 1. An aircraft fuel tank and baffle system comprising: an aircraft wing fuel tank located in an aircraft wing, said fuel tank enclosing a fuel storage space; and one or more baffles located within the fuel storage space, wherein each baffle is a tubular member through which a liquid may flow; the one or more baffles are aligned along a length of the aircraft wing; each baffle comprises: a first tubular portion providing a tubular outer wall; anda second tubular portion located within the first tubular portion and providing a tubular inner wall; for each baffle, the first and second tubular portions of that baffle are substantially parallel; for each baffle, the first and second tubular portions of that baffle are spaced apart to define a chamber therebetween; and each baffle further comprises radial side walls between its first and second tubular portions such that the chamber of that baffle is a sealed chamber.
地址 London GB