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Refuelling device for helicopters and vertical take-off aircraft in hovering flight

机译:悬停飞行中的直升机和垂直起飞飞机的加油装置

摘要

This device 100 comprises a base flange 10 equipped with a supply hose 11 for the delivery of fuel, and pipework 20 for refuelling in vertical position, elastically linked to the hose 11, and which can be automatically placed in vertical position from an offset or folded position, this pipework for refuelling in vertical position is composed of a flexible part 25 without spiral of a pressurised reservoir for the refuelling of aircraft and of an elastic winding 21 placed around the flexible part of the pressurised reservoir, this winding is fixed by its two ends 21a, 21b in the vicinity of the two ends 25a, 25b of the flexible part 25 of the pressurised reservoir in order to prevent any movement, and this flexible part 25 is equipped at its upper part 25a with a connector 30 which is itself equipped with a coupling device 31 for in-flight refuelling. This device, mounted on a bowser or a ship, makes it possible to easily refuel helicopters or vertical take-off aircraft in hovering flight above the said bowser or bridge of the said ship, in the event of it being impossible to land. IMAGE
机译:该装置100包括配备有用于输送燃料的供应软管11的基础凸缘10和用于在垂直位置加油的管道20,该管道弹性地连接到软管11,并且可以偏移或折叠地自动地置于垂直位置。在垂直位置加油时,该管道由一个不带螺旋部分的挠性部分25组成,该螺旋部分用于为飞机加油,还具有一个弹性绕组21,该螺旋绕组围绕着两个端部21a,21b位于加压容器的柔性部分25的两个端部25a,25b附近,以防止任何运动,并且该柔性部分25在其上部25a上配备有连接器30,该连接器30自身配备有具有用于空中加油的联接装置31。安装在mounted船或轮船上的该装置使得在无法降落的情况下,能够在所述船的bow船或桥上方悬停飞行时容易地给直升机或垂直起飞飞机加油。 <图像>

著录项

  • 公开/公告号FR2568852A3

    专利类型

  • 公开/公告日1986-02-14

    原文格式PDF

  • 申请/专利权人 BABEURS JEAN;

    申请/专利号FR19850007145

  • 发明设计人

    申请日1985-05-10

  • 分类号B64D39/00;

  • 国家 FR

  • 入库时间 2022-08-22 07:31:17

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