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    • 1. 发明授权
    • Aircraft refueling system
    • 飞机加油系统
    • US5839693A
    • 1998-11-24
    • US808431
    • 1997-02-28
    • Michael StalawIlana Hecht
    • Michael StalawIlana Hecht
    • B63B35/50B64F1/00B64F1/28B63B35/53
    • B64F1/00B63B35/50B64F1/28Y02T50/82
    • A refuelling system for aircraft, and in particular to a cellular system for refuelling long range aircraft crossing oceans. A floating refuelling station for aircraft includes at least one container hull which is movable and a sloping platform supported by the container. The sloping platform has at least one runway thereon for take off and landing of aircraft. The container hull may be used to store aviation fuel for refuelling the aircraft, the movability of the hull may be used to orient the runway with respect to the direction of the wind and the runway has a ramp section inclined at an angle to help slow down landing aircraft and/or to help speed up aircraft taking off. The height of the runway above the sea surface needs to be sufficient to accommodate any loss of buoyancy due to outpourings of gas from the sea bed.
    • 用于飞机的加油系统,特别是用于加油跨越海洋的长程飞机的蜂窝系统。 用于飞行器的浮动加油站包括至少一个可移动的容器壳体和由容器支撑的倾斜平台。 倾斜平台至少有一条跑道,用于飞机起飞和着陆。 集装箱船体可以用于存储用于加油的航空燃料,船体的可移动性可用于相对于风向定向跑道,并且跑道具有以一定角度倾斜的斜坡部分以帮助减速 着陆飞机和/或帮助加速飞机起飞。 海面以上跑道的高度需要足以应付由于从海床冒出气体而导致的任何浮力损失。