公开(公告)号：US20110290943A1

公开(公告)日：2011-12-01

申请号：US12786474

申请日：2010-05-25

申请人： Andrew WILDE ,  Jean-claude BOSSUT ,  Marc REVEL ,  Alan John HAYLES ,  Ruchir DAYAL ,  Hannah KENDALL

发明人： Andrew WILDE ,  Jean-claude BOSSUT ,  Marc REVEL ,  Alan John HAYLES ,  Ruchir DAYAL ,  Hannah KENDALL

IPC分类号： B64D37/04 ,  B64D13/08

CPC分类号： B64D37/04 ,  B64D37/02 ,  B64D37/06 ,  B64D37/32 ,  B64D2013/0659 ,  B64D2241/00

摘要： Fuel in an aircraft fuselage fuel tank is cooled by means of cold air flowing from the exterior of the aircraft to a cooling region inside the aircraft. The cooling region may be (a) located to the exterior of the fuel tank, (b) in thermal communication with the fuel tank and (c) in fluid communication with a region downstream of, and remote from, said cooling region, for example, an exhaust port on the outside of the aircraft. The flow of air may be caused by air entering a ram air intake, into which air passes as a result of the motion of the airborne aircraft relative to the surrounding air.

摘要翻译： 飞机机身燃料箱中的燃料通过从飞机外部流到飞机内的冷却区域的冷空气冷却。 冷却区域可以是（a）位于燃料箱的外部，（b）与燃料箱热连通，（c）与所述冷却区域的下游和远离区域流体连通，例如 ，飞机外侧的排气口。 空气流可能是空气进入冲击空气进气口，由于空中飞行器相对于周围空气的运动，空气通过。

公开(公告)号：US08757550B2

公开(公告)日：2014-06-24

申请号：US12786474

申请日：2010-05-25

申请人： Andrew Wilde ,  Jean-Claude Bossut ,  Marc Revel ,  Alan John Hayles ,  Ruchir Dayal ,  Hannah Kendall

发明人： Andrew Wilde ,  Jean-Claude Bossut ,  Marc Revel ,  Alan John Hayles ,  Ruchir Dayal ,  Hannah Kendall

IPC分类号： B64D15/04 ,  B64D15/16 ,  B64F5/00 ,  B64D37/04 ,  B64D37/32 ,  B64D37/02 ,  B64D37/06

CPC分类号： B64D37/04 ,  B64D37/02 ,  B64D37/06 ,  B64D37/32 ,  B64D2013/0659 ,  B64D2241/00

摘要： Fuel in an aircraft fuselage fuel tank is cooled by means of cold air flowing from the exterior of the aircraft to a cooling region inside the aircraft. The cooling region may be (a) located to the exterior of the fuel tank, (b) in thermal communication with the fuel tank and (c) in fluid communication with a region downstream of, and remote from, said cooling region, for example, an exhaust port on the outside of the aircraft. The flow of air may be caused by air entering a ram air intake, into which air passes as a result of the motion of the airborne aircraft relative to the surrounding air.

摘要翻译： 飞机机身燃料箱中的燃料通过从飞机外部流到飞机内的冷却区域的冷空气冷却。 冷却区域可以是（a）位于燃料箱的外部，（b）与燃料箱热连通，（c）与所述冷却区域的下游和远离区域流体连通，例如 ，飞机外侧的排气口。 空气流可能是空气进入冲击空气进气口，由于空中飞行器相对于周围空气的运动，空气通过。