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Aerial refueling system with telescoping refueling probe

机译:带有伸缩加油探头的空中加油系统

摘要

A refueling tank (16) has a telescopic refueling probe formed by a plurality of telescoping tubes (27,18,30) which are actuable for extension and retraction from an existing pylon mounted jettisonable external fuel tank (16) on the wing (17) of an aircraft. The telescopic drive action is achieved by a drive mechanism including a motor (14) and a jack screw mechanism which operates to extend and retract the telescoping tubes (27,18,30) slidably mounted, one on the other. The probe when fully retracted is completely enclosed within the associated fuel tank assembly (16) resulting in no additional drag or lift on the aircraft and keeping the probe concealed.
机译:加油箱(16)具有由多个伸缩管(27、18、30)形成的伸缩式加油探针,所述伸缩管可致动以从机翼(17)上的现有塔架安装的可抛弃外部燃油箱(16)伸出和缩回。一架飞机。伸缩驱动作用是通过一种驱动机构来实现的,该驱动机构包括一个电动机(14)和一个顶杆机构,该顶杆机构的作用是使可滑动安装的伸缩管(27、18、30)彼此伸缩。当探针完全缩回时,它完全封闭在相关的燃油箱组件(16)中,不会在飞机上产生额外的阻力或升力,并且使探针保持隐藏状态。

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