首页> 外国专利> METHOD FOR INSTALLATION OF SHORT-CIRCUIT INDICATOR (SCI) ON WIRE OF OVERHEAD TRANSMISSION LINE AND ITS REMOVAL FROM WIRE AND DEVICE FOR ITS IMPLEMENTATION

METHOD FOR INSTALLATION OF SHORT-CIRCUIT INDICATOR (SCI) ON WIRE OF OVERHEAD TRANSMISSION LINE AND ITS REMOVAL FROM WIRE AND DEVICE FOR ITS IMPLEMENTATION

机译:在架空输电线路的电线上安装短路指示器(SCI)的方法及其从电线和设备上的拆除及其实现

摘要

FIELD: electric power engineering.;SUBSTANCE: use in power engineering for installation of short-circuit indicator (SCI) on overhead power line (OL) wire and its dismantling from OL wire. Method consists in the fact that helicopter type aircraft is used, in the barrel of which before take-off SCI is fixed in position, at which arrangement of locking lever SCI is located above the upper edge of the shell, after which the aircraft flies from below to the wire in the place where SCI is to be installed, continues to move upwards to position when wire gets into narrow part between guides installed on aircraft, distance between which is somewhat larger than wire diameter, and, continuing upward movement, introduces wire into space between SCI clamping and thrust clamps, with further upward movement of aircraft, wire presses on guard, clamp is released and presses wire to thrust clamp, dismantling of SCI from wire is carried out by approach of aircraft to hanging on SCI wire, using guides and slopes, SCi body is inserted upwards inside sleeve, and with further movement of aircraft up upper edge of cartridge presses on locking lever, which is turned from it, releasing thrust bracket for its rotation, after which the aircraft starts to move downward, SCI under action of its gravity, as well as friction forces of spring clamps on its housing slides off the wire and is fixed in the barrel, the aircraft returns SCI to the ground. A corresponding device is also disclosed.;EFFECT: high safety of the SCI installation process and its dismantling from the OL wire.;4 cl, 5 dwg
机译:领域:电力工程。实体:在电力工程中用于在架空电力线(OL)电线上安装短路指示器(SCI)并将其从OL电线拆除。该方法包括以下事实:使用直升飞机型飞机,在其筒中将起飞SCI固定在适当的位置之前,锁定杆SCI的布置位于机壳的上边缘上方,然后飞机从到要安装SCI的位置的导线下方,当导线进入飞机上安装的导向装置之间的狭窄部分时,导线继续向上移动到一定位置,导线之间的距离略大于导线直径,并且继续向上移动,将导线引入进入SCI夹紧装置和推力夹紧装置之间的空间,随着飞机的进一步向上移动,将金属丝压在护板上,释放夹紧装置并将金属丝压入推力夹紧装置,通过飞机接近SCI钢丝的方式将SCI从金属丝上拆卸下来,方法是:引导和倾斜时,SCi主体向上插入套筒内,并且随着飞机的进一步移动,向上推锁定杆上弹药筒压力机的上边缘,然后将其转动,释放推力br旋转的支架,之后飞机开始向下移动,SCI在其重力作用下以及其外壳上的弹簧夹的摩擦力从钢丝上滑落并固定在机筒中,飞机将SCI返回地面。还公开了相应的设备。效果:SCI安装过程的高度安全性以及从OL电线上拆卸的安全性; 4 cl,5 dwg

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