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 |