CN103368103B - For hanging flight instruments and the method for sag rope to transmission line - Google Patents
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- 238000004891 communication Methods 0.000 claims abstract description 33
- 230000007246 mechanism Effects 0.000 claims description 52
- 239000004020 conductor Substances 0.000 claims description 5
- 238000003384 imaging method Methods 0.000 claims 4
- 238000007665 sagging Methods 0.000 abstract description 4
- 238000012423 maintenance Methods 0.000 description 6
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Abstract
本发明提供了一种用于向输电线路挂弧垂绳的飞行装置和方法,该飞行装置包括:无人飞行器;悬挂装置;通信装置;设有用于显示图像的显示器的控制终端;摄像装置。基于该飞行装置向输电线路挂弧垂绳的方法包括:在飞行装置起飞前,将弧垂绳挂载在飞行装置上;在飞行装置起飞后,使飞行装置实时拍摄弧垂绳和输电线路的图像,并在图像的中心位置处添加标记且显示图像;检测标记的位置,当标记位置从输电线路的导线一侧移至另一侧时,使飞行装置松开弧垂绳以向输电线路挂弧垂绳。本发明通过飞行装置将弧垂绳悬挂在输电线路上,不但可以提高工作效率,以及提高作业人员的安全系数,还可以在任何高度的输电线路上悬挂弧垂绳。
The invention provides a flying device and method for hanging a vertical rope to a power transmission line. The flying device includes: an unmanned aerial vehicle; a suspension device; a communication device; a control terminal equipped with a display for displaying images; and a camera device. The method for hanging the sag rope to the power transmission line based on the flying device includes: before the flying device takes off, the sagging rope is mounted on the flying device; image, and add a mark at the center of the image and display the image; detect the position of the mark, and when the mark position moves from one side of the wire of the power line to the other, the flying device releases the sag rope to hang to the power line Sagging rope. The invention suspends the sag rope on the transmission line through the flying device, which not only can improve the work efficiency and the safety factor of operators, but also can hang the sag rope on the transmission line at any height.
Description
技术领域technical field
本发明涉及输电线路维护领域,特别涉及一种用于向输电线路挂弧垂绳的飞行装置和方法。The invention relates to the field of power transmission line maintenance, in particular to a flying device and method for hanging a vertical line to a power transmission line.
背景技术Background technique
在输电线路巡视维修过程中,总是需要有直接接触导线的作业,比如带电测试、带电消除缺陷以及等电位作业等,这时就需要用到弧垂绳来辅助作业,弧垂绳是一根非常细、长且轻的绳子,在绳子的一端系有重锤,另一端系有工作用的粗绳,维修时,作业人员把重锤抛过输电线路的导线,然后拉动重锤一端,从而把粗绳拽过导线或把系在粗绳上的工器具拉拽至导线处。In the process of inspection and maintenance of transmission lines, it is always necessary to directly contact the wires, such as live testing, live defect elimination and equipotential work, etc. At this time, it is necessary to use a sag rope to assist the work. The sag rope is a A very thin, long and light rope with a heavy hammer tied to one end of the rope and a thick rope tied to work at the other end. During maintenance, the operator throws the heavy hammer over the wires of the transmission line, and then pulls one end of the heavy hammer, thereby Pull the thick rope through the wire or pull the tools tied to the thick rope to the wire.
现有技术中挂弧垂绳的方式是作业人员直接用手抛掷,由于人工抛掷对于抛掷力度和方向仅凭作业人员的手感,所以很难掌控,进而难以保证工作的效率和其他作业人员的人身安全,并且近年来随着电压等级的不断升高,以及同塔双回路高压输电线路和特种塔型的不断采用,输电线路的呼称高和弧垂距离地面越来越高,依靠作业人员直接用手抛掷弧垂绳工作效率低和安全系数低。In the prior art, the method of hanging the arc sag rope is that the operator throws it directly by hand. Since the force and direction of the manual throwing only depends on the operator's hand feeling, it is difficult to control, and it is difficult to ensure the efficiency of the work and the personal safety of other operators. Safe, and in recent years, with the continuous increase of voltage level, and the continuous adoption of double-circuit high-voltage transmission lines on the same tower and special tower types, the height of the transmission line and the sag from the ground are getting higher and higher, relying on operators to use it directly The hand-throwing arc sag rope has low work efficiency and low safety factor.
发明内容Contents of the invention
为了解决目前直接用手抛掷弧垂绳存在的工作效率低和安全系数低等问题,本发明提供了一种用于向输电线路挂弧垂绳的飞行装置和方法。In order to solve the problems of low work efficiency and low safety factor of throwing the sag rope directly by hand at present, the present invention provides a flying device and method for hanging the sag rope to the power transmission line.
为了解决上述问题,本发明一方面提供了一种用于向输电线路挂弧垂绳的飞行装置,其包括:无人飞行器;悬挂装置,设于所述无人飞行器下方,用于挂载弧垂绳或松开弧垂绳以将所述弧垂绳悬挂在输电线路上;通信装置,设于所述无人飞行器或所述悬挂装置上,并与所述悬挂装置通信连接,向所述悬挂装置输出控制指令;控制终端,与所述通信装置通信连接,向所述通信装置发出所述控制指令,所述悬挂装置在接收到所述通信装置转送来的所述控制指令后,将所述弧垂绳悬挂在输电线路上;和摄像装置,设于所述无人飞行器上,用于实时拍摄所述弧垂绳和所述输电线路的图像,并将所述图像传输至与该摄像装置通信连接的所述通信装置,所述通信装置将所述摄像装置传送来的图像传输至所述控制终端,供地面操作人员参考;所述控制终端上设有用于显示所述图像的显示器。In order to solve the above problems, the present invention provides a flying device for hanging arc sag ropes to power transmission lines on the one hand, which includes: an unmanned aerial vehicle; Hang the sag rope or loosen the sag rope to suspend the sag rope on the transmission line; the communication device is arranged on the unmanned aerial vehicle or the suspension device, and communicates with the suspension device to communicate with the suspension device. The suspension device outputs a control command; the control terminal communicates with the communication device and sends the control command to the communication device. After receiving the control command transmitted by the communication device, the suspension device sends the The sag rope is suspended on the power transmission line; and the camera device is installed on the unmanned aerial vehicle, and is used to capture images of the sag rope and the power transmission line in real time, and transmit the images to the camera The communication device is connected with the communication device, and the communication device transmits the image transmitted by the camera device to the control terminal for reference by ground operators; the control terminal is provided with a display for displaying the image.
在如上所述的飞行装置中,优选所述悬挂装置包括:支架,设置并连接于所述无人飞行器下方;挂钩机构,设于所述支架上,用于挂载或松开所述弧垂绳;电动驱动机构,设于所述支架上,并与所述挂钩机构和所述通信装置连接,根据来自所述通信装置的所述控制指令,驱动所述挂钩机构挂载或松开所述弧垂绳。In the above-mentioned flying device, preferably, the suspension device includes: a bracket, arranged and connected under the UAV; a hook mechanism, arranged on the bracket, for mounting or releasing the sag Rope; an electric drive mechanism, set on the bracket, and connected with the hook mechanism and the communication device, according to the control command from the communication device, drives the hook mechanism to mount or release the Sagging rope.
在如上所述的飞行装置中,优选:所述电动驱动机构包括设置有输出轴的舵机;所述挂钩机构包括摆臂,所述摆臂的固定端套接于所述输出轴。In the above-mentioned flying device, preferably: the electric drive mechanism includes a steering gear provided with an output shaft; the hook mechanism includes a swing arm, and a fixed end of the swing arm is sleeved on the output shaft.
在如上所述的飞行装置中,优选:所述飞行装置还包括限位机构,所述限位机构包括:限位块、弹簧、滑轮和牵引件;在位于所述固定端和所述摆臂的自由端之间的摆臂内部设置有空腔,所述空腔的侧壁包括:上侧壁、下侧壁、前侧壁和后侧壁;所述上侧壁上设置有通孔和穿孔,所述穿孔位于所述通孔和所述固定端之间,所述通孔用于容纳所述限位块;设置于所述空腔内的所述弹簧的下端固定于所述下侧壁,所述弹簧的上端连接于所述限位块的底端;所述下侧壁上设置有第一凹槽和第二凹槽,所述第一凹槽和所述第二凹槽通过长孔连接;所述第一凹槽位于所述弹簧的中部空间下方,所述第二凹槽位于所述第一凹槽和所述固定端之间;所述滑轮设置于所述第一凹槽内;所述牵引件的一端与所述限位块的底端连接,所述牵引件的另一端穿过所述弹簧的中部空间并绕过所述滑轮后,在所述长孔内延伸到所述第二凹槽,然后经所述穿孔伸出到摆臂外部,固定于所述支架上;所述限位块在所述牵引件和所述弹簧的驱动下伸出所述通孔外或退回所述通孔内。In the above-mentioned flying device, preferably: the flying device further includes a limiting mechanism, and the limiting mechanism includes: a limiting block, a spring, a pulley and a traction member; A cavity is provided inside the swing arm between the free ends, and the side walls of the cavity include: an upper side wall, a lower side wall, a front side wall and a rear side wall; the upper side wall is provided with through holes and perforation, the perforation is located between the through hole and the fixed end, the through hole is used to accommodate the limit block; the lower end of the spring arranged in the cavity is fixed on the lower side wall, the upper end of the spring is connected to the bottom end of the limit block; the lower side wall is provided with a first groove and a second groove, and the first groove and the second groove pass through Long hole connection; the first groove is located below the middle space of the spring, and the second groove is located between the first groove and the fixed end; the pulley is arranged in the first groove In the groove; one end of the traction member is connected to the bottom end of the limit block, and the other end of the traction member passes through the middle space of the spring and bypasses the pulley, and then extends in the long hole to the second groove, then protrude to the outside of the swing arm through the through hole, and be fixed on the bracket; the limit block is driven out of the through hole by the traction piece and the spring outside or retracted into the through hole.
在如上所述的飞行装置中,优选:所述飞行装置还包括限位机构,所述限位机构包括:限位块、弹簧、滑轮、牵引件和轴套;在位于所述固定端和所述摆臂的自由端之间的摆臂内部设置有空腔,所述空腔的侧壁包括:上侧壁、下侧壁、前侧壁和后侧壁;所述固定端设置有开口,所述开口与所述空腔连通;所述轴套位于所述开口内且套设于所述输出轴;所述上侧壁设置有通孔;设置于所述空腔内的所述弹簧的下端固定于所述下侧壁,所述弹簧的上端连接于所述限位块的底端;所述下侧壁上设置有第一凹槽和第二凹槽,所述第一凹槽和所述第二凹槽通过长孔连接;所述第一凹槽位于所述弹簧的中部空间下方,所述第二凹槽位于所述第一凹槽和所述固定端之间;所述滑轮设置于所述第一凹槽内;所述牵引件的一端与所述限位块的底端连接,所述牵引件的另一端穿过所述弹簧的中部空间并绕过所述滑轮后,在所述长孔内延伸,并在所述第二凹槽伸出,固定于所述轴套上;所述限位块在所述牵引件和所述弹簧的驱动下伸出所述通孔外或退回所述通孔内。In the flying device as described above, preferably: the flying device further includes a limit mechanism, and the limit mechanism includes: a limit block, a spring, a pulley, a traction piece and a bushing; The inside of the swing arm between the free ends of the swing arm is provided with a cavity, and the side walls of the cavity include: an upper side wall, a lower side wall, a front side wall and a rear side wall; the fixed end is provided with an opening, The opening communicates with the cavity; the sleeve is located in the opening and sleeved on the output shaft; the upper side wall is provided with a through hole; the spring disposed in the cavity The lower end is fixed to the lower side wall, and the upper end of the spring is connected to the bottom end of the limit block; the lower side wall is provided with a first groove and a second groove, and the first groove and the second groove are arranged on the lower side wall. The second groove is connected by a long hole; the first groove is located below the middle space of the spring, and the second groove is located between the first groove and the fixed end; the pulley It is arranged in the first groove; one end of the traction member is connected to the bottom end of the limit block, and the other end of the traction member passes through the middle space of the spring and bypasses the pulley, Extend in the long hole, protrude from the second groove, and be fixed on the bushing; the limiting block protrudes out of the through hole driven by the traction member and the spring outside or retracted into the through hole.
在如上所述的飞行装置中,优选:所述牵引件为细绳。In the above-mentioned flying device, preferably: the traction member is a thin rope.
在如上所述的飞行装置中,优选:所述长孔为设置于所述下侧壁的空腔侧表面上的长槽,将所述第一凹槽和所述第二凹槽相连通。In the above-mentioned flying device, preferably: the long hole is a long groove provided on the side surface of the cavity of the lower side wall, connecting the first groove and the second groove.
在如上所述的飞行装置中,优选还包括:用于控制所述无人飞行器的飞行轨迹的地面控制装置,所述地面控制装置和所述控制终端为一体结构。In the above-mentioned flying device, it is preferable to further include: a ground control device for controlling the flight trajectory of the unmanned aerial vehicle, the ground control device and the control terminal are integrally structured.
在如上所述的飞行装置中,优选:所述无人飞行器为四轴无人飞行器。In the above-mentioned flying device, preferably: the unmanned aerial vehicle is a four-axis unmanned aerial vehicle.
本发明还提供一种用于向输电线路挂弧垂绳的方法,所述方法包括:在飞行装置起飞前,将弧垂绳挂载在所述飞行装置上;在所述飞行装置起飞后,使所述飞行装置实时拍摄所述弧垂绳和输电线路的图像,并在所述图像的中心位置处添加标记且显示所述图像;检测标记的位置,当所述标记位置从所述输电线路的导线一侧移至另一侧时,使所述飞行装置松开弧垂绳以向输电线路挂弧垂绳;其中所述飞行装置为上述的飞行装置。The present invention also provides a method for hanging a sag rope to a power transmission line, the method comprising: before the flight device takes off, hanging the sag rope on the flight device; after the flight device takes off, Make the flying device take the image of the sag rope and the power transmission line in real time, add a mark at the center position of the image and display the image; detect the position of the mark, when the position of the mark is from the power transmission line When one side of the conductor is moved to the other side, the flying device is released from the sag rope to hang the sag rope to the power transmission line; wherein the flying device is the above-mentioned flying device.
本发明通过飞行装置将弧垂绳悬挂在输电线路上,这样在输电线路上挂弧垂绳时,不但可以提高工作效率,以及提高作业人员的安全系数,还可以在任何高度的输电线路上悬挂弧垂绳。The invention hangs the sag rope on the transmission line through the flying device, so that when the sag rope is hung on the transmission line, not only can the work efficiency be improved, but also the safety factor of the operators can be improved, and it can also be hung on the transmission line at any height Sagging rope.
附图说明Description of drawings
图1是本发明提供的一种用于向输电线路挂弧垂绳的飞行装置的结构示意图;Fig. 1 is a kind of structural schematic diagram of the flight device that is used for hanging vertical rope to transmission line provided by the present invention;
图2是图1中A部分的放大示意图;Fig. 2 is the enlarged schematic diagram of part A in Fig. 1;
图3是本发明提供的另一种用于向输电线路挂弧垂绳的飞行装置的结构示意图;Fig. 3 is a schematic structural view of another flying device for hanging a vertical rope to a power transmission line provided by the present invention;
图4是图3中A部分的放大示意图;Fig. 4 is the enlarged schematic diagram of part A in Fig. 3;
图5是图3中限位机构、摆臂和输出轴的的结构示意图;Fig. 5 is a structural schematic diagram of the limit mechanism, the swing arm and the output shaft in Fig. 3;
图6是本发明提供的又一种用于向输电线路挂弧垂绳的飞行装置的限位机构、摆臂和输出轴的结构示意图;Fig. 6 is a structural schematic diagram of the limit mechanism, the swing arm and the output shaft of another flying device for hanging the vertical rope to the power transmission line provided by the present invention;
图7是本发明提供的一种用于向输电线路挂弧垂绳的方法流程示意图;Fig. 7 is a schematic flow chart of a method for hanging a vertical rope to a power transmission line provided by the present invention;
附图标记含义如下:The reference signs have the following meanings:
1四轴无人飞行器;2通信装置;3摄像装置;1 four-axis unmanned aerial vehicle; 2 communication device; 3 camera device;
4弧垂绳;41重锤;42挂环;43细绳;4 arc sag rope; 41 heavy hammer; 42 hanging ring; 43 thin rope;
6悬挂装置;6 suspension devices;
61支架;621舵机;622输出轴;631挂钩;61 bracket; 621 steering gear; 622 output shaft; 631 hook;
632摆臂;6320固定端;6321自由端;633轴套;632 swing arm; 6320 fixed end; 6321 free end; 633 bushing;
6322空腔;6323上侧壁;6324通孔;6325穿孔;6322 cavity; 6323 upper side wall; 6324 through hole; 6325 perforation;
6327下侧壁;6327 lower side wall;
7控制终端;71显示器;7 control terminals; 71 monitors;
8限位机构;81限位块;82弹簧;83牵引件8 limit mechanism; 81 limit block; 82 spring; 83 traction piece
84滑轮。84 pulleys.
具体实施方式detailed description
为使本发明的目的、技术方案和优点更加清楚,下面将结合附图对本发明实施方式作进一步地详细描述。In order to make the object, technical solution and advantages of the present invention clearer, the implementation manner of the present invention will be further described in detail below in conjunction with the accompanying drawings.
为了解决现有技术中存在的弧垂绳4难以准确手工抛过输电线路的问题,本发明提供了一种用于向输电线路挂弧垂绳的飞行装置,下面以无人飞行器为四轴无人飞行器为例进行说明。In order to solve the problem that the sag rope 4 existing in the prior art is difficult to accurately manually throw over the power transmission line, the present invention provides a flying device for hanging the sag rope 4 to the power transmission line. Take the manned aircraft as an example for illustration.
参照图1-图6,该飞行装置包括四轴无人飞行器1、悬挂装置6、通信装置2、控制终端7和摄像装置3。其中,悬挂装置6设于四轴无人飞行器1下方,用于挂载弧垂绳4并将弧垂绳4悬挂在输电线路上。通信装置2设于四轴无人飞行器1上,并与悬挂装置6通信连接,接收地面操作人员通过操作控制终端7而发出的控制命令,并将该控制命令输出至悬挂装置6以控制悬挂装置6的动作,通信装置还可以设于悬挂装置6上。控制终端7与通信装置2通信连接,用于向通信装置2发出控制指令以控制悬挂装置6的动作,将弧垂绳4悬挂在输电线路上或者挂起弧垂绳4。摄像装置3设于四轴无人飞行器1上,用于实时拍摄弧垂绳和输电线路的图像,并将该图像传输至与其所通信连接的通信装置2。通信装置2将摄像装置3传送来的图像传输至控制终端7,控制终端7上设有用于显示图像的显示器71,地面操作人员通过观察显示器71了解弧垂绳和输电线路的相互位置关系,并通过对控制终端的操作发出控制指令,控制悬挂装置6的动作。通信装置2和控制终端7的连接方式优选为无线连接,以使四轴无人飞行器1在挂载弧垂绳4时,不受图像传输线路的干扰。Referring to FIGS. 1-6 , the flying device includes a four-axis unmanned aerial vehicle 1 , a suspension device 6 , a communication device 2 , a control terminal 7 and a camera device 3 . Wherein, the suspension device 6 is arranged under the four-axis unmanned aerial vehicle 1, and is used for mounting the sag rope 4 and suspending the sag rope 4 on the power transmission line. The communication device 2 is arranged on the four-axis unmanned aerial vehicle 1, and communicates with the suspension device 6, receives the control command issued by the ground operator through the operation control terminal 7, and outputs the control command to the suspension device 6 to control the suspension device 6, the communication device can also be located on the suspension device 6. The control terminal 7 is communicatively connected with the communication device 2, and is used to send control instructions to the communication device 2 to control the action of the suspension device 6, to suspend the sag rope 4 on the transmission line or to hang the sag rope 4. The camera device 3 is arranged on the four-axis unmanned aerial vehicle 1, and is used for taking real-time images of the sag rope and the power transmission line, and transmitting the images to the communication device 2 communicated with it. The communication device 2 transmits the image transmitted by the camera device 3 to the control terminal 7, and the control terminal 7 is provided with a display 71 for displaying the image. The ground operator understands the mutual positional relationship between the sag rope and the power transmission line by observing the display 71, and The action of the suspension device 6 is controlled by issuing control instructions to the operation of the control terminal. The connection mode between the communication device 2 and the control terminal 7 is preferably a wireless connection, so that the quadcopter unmanned aerial vehicle 1 will not be disturbed by the image transmission line when the sag rope 4 is mounted.
悬挂装置6包括支架61、挂钩机构63和设置有输出轴622的电动驱动机构。支架61固定连接在四轴无人飞行器1下部的中心位置,挂钩机构63和电动驱动机构均设于支架61上,挂钩机构63与电动驱动机构的输出轴622连接,用于挂载弧垂绳4的重锤41或者将弧垂绳4从挂钩机构上松开并将弧垂绳4悬挂在输电线路上。进一步具体而言,挂钩机构63可活动地设于支架61上,电动驱动机构的输出轴622与挂钩机构63连接。电动驱动机构优选为舵机621。The suspension device 6 includes a bracket 61 , a hook mechanism 63 and an electric drive mechanism provided with an output shaft 622 . The bracket 61 is fixedly connected to the central position of the lower part of the four-axis unmanned aerial vehicle 1. The hook mechanism 63 and the electric drive mechanism are both arranged on the bracket 61. The hook mechanism 63 is connected with the output shaft 622 of the electric drive mechanism for mounting the arc sag rope. 4 or the sag rope 4 is released from the hook mechanism and the sag rope 4 is suspended on the power transmission line. More specifically, the hook mechanism 63 is movably arranged on the bracket 61 , and the output shaft 622 of the electric drive mechanism is connected to the hook mechanism 63 . The electric driving mechanism is preferably a steering gear 621 .
如图1和图2所示,弧垂绳4包括重锤41、挂环42和细绳43,细绳43连接于重锤41上表面的挂环42,挂钩机构具有挂钩631,该挂钩631的一端套设于输出轴622,且在电动驱动机构的驱动下能旋转,挂钩631的另一端穿过挂环42使得弧垂绳4挂在挂钩631上。待四轴无人飞行器1上升至指定位置时,地面操作人员通过控制终端使电动驱动机构的输出轴620旋转,从而驱动挂钩631旋转,由此使得挂环42从挂钩631中抽出,这样,在重力作用下,重锤41将快速下落,进而将细绳43挂在输电线路上,实现弧垂绳4悬挂在输电线路上。As shown in Figures 1 and 2, the sag rope 4 includes a weight 41, a hanging ring 42 and a string 43, the string 43 is connected to the hanging ring 42 on the upper surface of the weight 41, and the hook mechanism has a hook 631, and the hook 631 One end of the hook 631 is sheathed on the output shaft 622 and can rotate under the driving of the electric drive mechanism. The other end of the hook 631 passes through the hanging ring 42 so that the sag rope 4 is hung on the hook 631 . When the four-axis unmanned aerial vehicle 1 rises to the designated position, the ground operator rotates the output shaft 620 of the electric drive mechanism through the control terminal, thereby driving the hook 631 to rotate, thereby causing the hanging ring 42 to be extracted from the hook 631. Under the action of gravity, the weight 41 will fall rapidly, and then the string 43 will be hung on the transmission line, so that the sag rope 4 is suspended on the transmission line.
在另一种实施方式中,如图3-图5所示,挂钩机构包括摆臂632,摆臂632的固定端6320套接于输出轴622,在固定端6320和摆臂632的自由端6321之间挂载弧垂绳的重锤。应用时,摆臂632在舵机621和输出轴622的驱动作用下旋转,旋转角度可以从0度(与地面平行)至90度(与地面垂直,向图中右下角逆时针旋转),当摆臂632在舵机621的驱动下旋转至与地面平行的位置时,将弧垂绳4的挂环42套设于摆臂632上以挂载重锤41,由于重锤41上系有细绳43,摆臂621间接挂载了细绳43。当摆臂632在舵机621的驱动下旋转至与地面垂直时,弧垂绳4的重锤41在重力作用下,脱离摆臂632,向下坠落,重锤41上的细绳43向下延伸,从而将弧垂绳悬挂在输电线路上。In another embodiment, as shown in FIGS. 3-5 , the hook mechanism includes a swing arm 632 , the fixed end 6320 of the swing arm 632 is sleeved on the output shaft 622 , and the fixed end 6320 and the free end 6321 of the swing arm 632 The weight of the sag rope is mounted between them. In application, the swing arm 632 rotates under the drive of the steering gear 621 and the output shaft 622, and the rotation angle can be from 0 degrees (parallel to the ground) to 90 degrees (perpendicular to the ground, rotating counterclockwise to the lower right corner in the figure). When the swing arm 632 rotates to a position parallel to the ground under the driving of the steering gear 621, the hanging ring 42 of the sag rope 4 is sleeved on the swing arm 632 to hang the weight 41. Since the weight 41 is tied with a string 43. The swing arm 621 is indirectly mounted with the string 43. When the swing arm 632 rotates to be perpendicular to the ground under the driving of the steering gear 621, the weight 41 of the sag rope 4 will break away from the swing arm 632 under the action of gravity and fall downwards, and the string 43 on the weight 41 will fall downwards. Extend, thereby suspending the sag rope on the transmission line.
在四轴无人飞行器的飞行过程中,为了避免弧垂绳的挂环42左右移动造成重锤提前从摆臂621上脱落的现象,飞行装置还包括用于限定挂环42位置的限位机构8(如图3-图5所示),其包括限位块81、弹簧82、滑轮84和牵引件83。During the flight of the four-axis unmanned aerial vehicle, in order to avoid the phenomenon that the hanging ring 42 of the sag rope moves left and right to cause the heavy hammer to fall off the swing arm 621 in advance, the flying device also includes a limit mechanism for limiting the position of the hanging ring 42 8 (as shown in FIGS. 3-5 ), which includes a limit block 81 , a spring 82 , a pulley 84 and a traction member 83 .
为了设置限位机构8,在摆臂632的固定端6320和自由端6321之间,在所述摆臂的内部设置有空腔6322,该空腔6322由固定端6320、自由端6321和上侧壁6323、下侧壁6327、前后侧壁(未图示)围成,其中上侧壁6323和下侧壁6327隔着空腔6322上下相对,未图示的前后侧壁隔着空腔6322前后相对。In order to set the limit mechanism 8, between the fixed end 6320 and the free end 6321 of the swing arm 632, a cavity 6322 is provided inside the swing arm, and the cavity 6322 consists of the fixed end 6320, the free end 6321 and the upper side. The wall 6323, the lower side wall 6327, and the front and rear side walls (not shown), wherein the upper side wall 6323 and the lower side wall 6327 face each other up and down across the cavity 6322, and the front and rear side walls not shown in the figure are separated by the cavity 6322. relatively.
上侧壁6323设置有用于容纳限位块81的通孔6324,上侧壁6323上还设置有穿孔6325,以使牵引件83的细绳从其穿出固定于支架61上,通孔6324与穿孔6325之间相隔一定距离,穿孔6325更靠近摆臂的固定端,而且通孔6324与穿孔6325均与空腔6322连通,也即将空腔6322与摆臂的外部连通。The upper side wall 6323 is provided with a through hole 6324 for accommodating the limit block 81, and the upper side wall 6323 is also provided with a perforation 6325, so that the string of the traction member 83 passes through it and is fixed on the bracket 61. The through hole 6324 and There is a certain distance between the through holes 6325, and the through holes 6325 are closer to the fixed end of the swing arm, and both the through holes 6324 and the through holes 6325 communicate with the cavity 6322, that is, the cavity 6322 communicates with the outside of the swing arm.
在空腔内设置有弹簧82,弹簧82的下端固定于下侧壁6327的内表面(空腔侧表面),弹簧82的上端与限位块81的底端接触连接。为了避免限位块81从通孔6324掉出,优选弹簧82的上端与限位块81的底部固定连接。在无人飞行器飞至规定位置之前,弧垂绳4挂载在摆臂上时,限位块81的上端伸出通孔6324外,阻挡弧垂绳4的挂环42从摆臂上滑落。当无人飞行器飞至规定位置之后,在电动驱动机构的驱动下,摆臂621的自由端向下转动,同时限位块81在弹簧82和细绳的带动下退回通孔6324内,此时借助重力的作用,挂环42从摆臂621上滑落,悬挂于输电线路上。A spring 82 is arranged in the cavity, the lower end of the spring 82 is fixed on the inner surface of the lower side wall 6327 (side surface of the cavity), and the upper end of the spring 82 is in contact with the bottom end of the limiting block 81 . In order to prevent the limiting block 81 from falling out of the through hole 6324 , preferably, the upper end of the spring 82 is fixedly connected with the bottom of the limiting block 81 . Before the unmanned aerial vehicle flies to the prescribed position, when the sag rope 4 is mounted on the swing arm, the upper end of the limit block 81 stretches out of the through hole 6324, preventing the hanging ring 42 of the sag rope 4 from sliding off the swing arm. After the unmanned aerial vehicle flies to the specified position, under the drive of the electric drive mechanism, the free end of the swing arm 621 rotates downwards, and simultaneously the limit block 81 returns in the through hole 6324 under the drive of the spring 82 and the string. With the help of gravity, the hanging ring 42 slides off the swing arm 621 and hangs on the power transmission line.
在电动驱动机构的控制下,为了使得弹簧82相应地动作,在空腔内还设置有如下的结构:作为牵引件83的细绳的一端固定于限位块81的底端或者弹簧82的上端,细绳的另一端在弹簧82的中部空间延伸,并绕过设置在所述中部空间内且固定于下侧壁6327的空腔侧表面上的滑轮84,然后在空腔6322内延伸,直至从穿孔6325穿出,并将另一端固定于支架61上。Under the control of the electric drive mechanism, in order to make the spring 82 act accordingly, the following structure is also arranged in the cavity: one end of the string as the traction member 83 is fixed to the bottom end of the stop block 81 or the upper end of the spring 82 , the other end of the string extends in the middle space of the spring 82, and goes around the pulley 84 that is arranged in the middle space and fixed on the cavity side surface of the lower side wall 6327, and then extends in the cavity 6322 until Pass through the hole 6325, and fix the other end on the bracket 61.
为了使得细绳在绕过滑轮84改变方向后在空腔内延伸的过程中,不与弹簧82的底部相互干涉,优选在下侧壁6327的空腔侧面形成两个凹槽----第一凹槽和第二凹槽,第一凹槽和第二凹槽之间通过一位于下侧壁内的直线形长孔相连通,其中,第一凹槽位于弹簧82的中部空间下方(第一凹槽的开口面积比弹簧82的中部空间截面积小),滑轮84固定于第一凹槽内,第二凹槽相比于第一凹槽更靠近摆臂的固定端一侧,细绳通过第一凹槽改变方向后在长孔内延伸至第二凹槽,从第二凹槽内穿出后引申至穿孔6325而将另一端固定于支架61上。由此,避免在运行过程中,绕过滑轮的细绳与弹簧相接触,影响牵引效果。In order to prevent the string from interfering with the bottom of the spring 82 during the process of extending the string around the pulley 84 and changing its direction in the cavity, it is preferable to form two grooves on the side of the cavity of the lower side wall 6327---the first The groove and the second groove are communicated between the first groove and the second groove through a linear elongated hole located in the lower side wall, wherein the first groove is located below the central space of the spring 82 (first The opening area of the groove is smaller than the central space cross-sectional area of the spring 82), the pulley 84 is fixed in the first groove, the second groove is closer to the fixed end side of the swing arm than the first groove, and the string passes through After changing direction, the first groove extends to the second groove in the long hole, passes through the second groove and extends to the through hole 6325 to fix the other end on the bracket 61 . Thus, it is avoided that the thin rope bypassing the pulley is in contact with the spring during operation, which affects the traction effect.
作为另一个优选,可以在第二凹槽内也设置一个滑轮,用于细绳的变向调整。而且,取代上述长孔,可以在下侧壁的空腔侧表面上设置长槽,由长槽将第一凹槽和第二凹槽加以连通,细绳沿着长槽从第一凹槽延伸到第二凹槽。As another preference, a pulley may also be arranged in the second groove for direction change adjustment of the string. Moreover, instead of the above-mentioned long holes, long grooves can be set on the cavity side surface of the lower side wall, the first groove and the second groove are communicated by the long grooves, and the string extends from the first groove to the second groove along the long grooves. second groove.
滑轮优选为定滑轮。应用中,当摆臂632位于与地面平行的位置时,将挂环42套设于固定端6320和通孔6324之间,由于限位块81的上端伸出通孔6324外,会阻挡挂环42从摆臂632上滑落;当摆臂632从与地面平行的位置转至与地面垂直的位置的过程中,牵引件83的细绳会被拉伸以拉动限位块81压缩弹簧82并向通孔6324内运动,当限位块81的上端沉入通孔内时,在重锤41的重力作用下挂环42从摆动壁632上滑落,将弧垂绳的细绳挂载在输电线路上。限位块81的上端形状优选为弧形,通孔6324或者穿孔6325的孔壁与孔底的夹角(倒角)优选为圆角。The pulley is preferably a fixed pulley. In application, when the swing arm 632 is in a position parallel to the ground, the hanging ring 42 is sleeved between the fixed end 6320 and the through hole 6324, since the upper end of the limit block 81 protrudes out of the through hole 6324, it will block the hanging ring 42 slides down from the swing arm 632; when the swing arm 632 turns from a position parallel to the ground to a position perpendicular to the ground, the string of the traction member 83 will be stretched to pull the stop block 81 to compress the spring 82 and move toward Movement in the through hole 6324, when the upper end of the limit block 81 sinks into the through hole, the hanging ring 42 slides down from the swing wall 632 under the gravity of the weight 41, and the thin rope of the sag rope is hung on the power transmission line superior. The shape of the upper end of the limiting block 81 is preferably arc-shaped, and the angle (chamfer) between the hole wall and the hole bottom of the through hole 6324 or the through hole 6325 is preferably rounded.
在又一种实施方式中,如图6所示,为摆臂与输出轴的主视剖面图,其中,第一凹槽、第二凹槽以及连通第一、第二凹槽的长孔与上述实施方式完全相同,不同的是本实施方式中不再在上侧壁上设置穿孔,而是在摆臂内的空腔在固定端形成开口,输出轴依次穿过摆臂的前侧壁、开口、后侧壁后与摆臂固定连接在一起,也即空腔6322与开口连通且连为一体,在位于开口处的输出轴上套设有轴套633,该轴套633在输出轴的转动过程中使得细绳缠绕在其上以拉动弹簧。In yet another embodiment, as shown in FIG. 6 , it is a front sectional view of the swing arm and the output shaft, wherein the first groove, the second groove and the long hole communicating with the first and second grooves are connected with the The above-mentioned embodiments are exactly the same, the difference is that no perforation is provided on the upper side wall in this embodiment, but the cavity in the swing arm forms an opening at the fixed end, and the output shaft passes through the front side wall of the swing arm, The opening, the rear side wall and the swing arm are fixedly connected together, that is, the cavity 6322 communicates with the opening and is connected as a whole. The output shaft at the opening is sleeved with a shaft sleeve 633, and the shaft sleeve 633 is placed on the output shaft. During the rotation, the string is wound around it to pull the spring.
细绳的另一端穿过弹簧的中部空间经位于第一凹槽内的滑轮改向后,依次穿过长孔、第二凹槽(第二凹槽内设置有滑轮时就通过滑轮)后固定在轴套633上,随着输出轴的转动,轴套633也转动,并拉紧细绳,使得细绳拉动弹簧使弹簧压缩或者放松。The other end of the string passes through the middle space of the spring and is redirected by the pulley located in the first groove, then passes through the long hole and the second groove in turn (if there is a pulley in the second groove, it will pass through the pulley) and then fixed On the shaft sleeve 633, as the output shaft rotates, the shaft sleeve 633 also rotates, and tightens the string so that the string pulls the spring to compress or relax the spring.
比如输出轴逆时针转动时,带动摆臂跟着逆时针转动,由于细绳的长度固定,而细绳的另一端固定在轴套上,随着摆臂和轴套的转动,细绳会向轴套上缠绕,由此会带动细绳的另一端向下拉动弹簧,使得弹簧被压缩,使得被弹簧支撑的限位块沉入通孔内,不再阻挡挂环从摆臂上脱落,这样,弧垂绳就会从摆臂上脱离而挂在输电线路上。For example, when the output shaft rotates counterclockwise, it drives the swing arm to rotate counterclockwise. Since the length of the string is fixed, and the other end of the string is fixed on the bushing, as the swing arm and the bushing rotate, the string will move toward the shaft. Putting on the winding will drive the other end of the string to pull the spring downward, so that the spring is compressed, so that the limit block supported by the spring sinks into the through hole, and no longer prevents the hanging ring from falling off the swing arm. In this way, The sag rope will break away from the swing arm and hang on the transmission line.
需要说明的是,在限位块81与通孔6324的配合过程中,会留有缝隙,为了避免缝隙过大导致挂环42划入缝隙中,优选挂环42的直径大于缝隙的直径。It should be noted that during the mating process of the limit block 81 and the through hole 6324, there will be a gap. In order to avoid the gap being too large and causing the hanging ring 42 to be drawn into the gap, the diameter of the hanging ring 42 is preferably larger than the diameter of the gap.
在实际中,牵引件83可以为细绳,还可以为细金属丝,优选为细绳。In practice, the traction member 83 may be a string, or a thin metal wire, preferably a string.
为了能够精确向输电线路挂弧垂绳,摄像装置3优选设于悬挂装置6旁边,换句话说其位于四轴无人飞行器下方且连接悬挂装置6。在实际中,为了识别出挂弧垂绳的位置,对摄像装置3实时拍摄的图像的中心处添加标记,还可以在显示该图像的显示器屏幕的中心处添加标记,地面操作人员通过显示器71观察该标记,当该标记位置从输电线路导线的一侧移至与该一侧相对的另一侧时,表明重锤41已位于输电线路导线的另一侧,地面操作人员通过控制终端7发出控制指令以驱动悬挂装置6松开重锤41以在输电线路挂载弧垂绳4。In order to accurately hang the sag rope to the power transmission line, the camera device 3 is preferably arranged next to the suspension device 6 , in other words, it is located below the quadcopter UAV and connected to the suspension device 6 . In practice, in order to identify the position of the hanging arc slump rope, a mark is added to the center of the image captured by the camera device 3 in real time, and a mark can also be added to the center of the display screen showing the image, and the ground operator observes through the display 71 This mark, when the position of the mark moves from one side of the power transmission line conductor to the other side opposite to the one side, indicates that the weight 41 has been positioned on the other side of the power transmission line conductor, and the ground operator sends out control through the control terminal 7 Command to drive the suspension device 6 to loosen the weight 41 to mount the sag rope 4 on the power transmission line.
为了简化结构,四轴无人飞行器1的用于控制无人飞行器飞行轨迹的地面控制装置与控制终端7为一体结构,地面控制装置用于发出飞行控制指令,该飞行控制指令用于指示飞行状态,从而形成飞行轨迹。控制终端7上设有控制四轴无人飞行器1飞行轨迹的按键或操作杆等。In order to simplify the structure, the ground control device and the control terminal 7 of the four-axis unmanned aerial vehicle 1 for controlling the flight path of the unmanned aerial vehicle are in one structure, and the ground control device is used to issue flight control commands, which are used to indicate the flight status , forming a flight path. The control terminal 7 is provided with buttons or joysticks for controlling the flight path of the four-axis unmanned aerial vehicle 1 .
本优选实施例的应用过程大致如下:The application process of this preferred embodiment is roughly as follows:
地面操作人员(作业人员)在输电线路巡视过程中,发现需要维修的位置时,通过控制终端7,使驱动机构62驱动挂钩机构63开启,将弧垂绳4的挂环42挂上。然后使挂钩机构63闭合,操作控制终端7,使四轴无人飞行器1飞行到输电线路上方,摄像装置3对输电线路、弧垂绳4等进行拍照,显示器71显示该图像。电力工人根据显示的图像判断四轴无人飞行器1是否抵达需要维修的输电线路位置,如果不是,则调整四轴无人飞行器1的飞行状态,直至四轴无人飞行器1抵达到需要维修的输电线路位置,接着使挂钩机构63开启以抛掉重锤41,从而使弧垂绳4挂在需要维修的输电线路位置。When the ground operator (operator) finds a location that needs maintenance during the inspection of the transmission line, the driving mechanism 62 drives the hook mechanism 63 to open through the control terminal 7, and hangs the hanging ring 42 of the sag rope 4. Then the hook mechanism 63 is closed, and the control terminal 7 is operated to make the four-axis unmanned aerial vehicle 1 fly above the power transmission line. The camera 3 takes pictures of the power transmission line, the sag rope 4, etc., and the display 71 displays the image. According to the displayed image, the power worker judges whether the four-axis unmanned aerial vehicle 1 has reached the position of the power transmission line that needs maintenance. Line position, then the hook mechanism 63 is opened to throw away the weight 41, so that the sag rope 4 is hung on the power transmission line position that needs maintenance.
为了解决上述问题,本发明还提供了一种用于向输电线路挂弧垂绳的飞行装置向输电线路挂弧垂绳的方法,参见图7,该方法包括:In order to solve the above-mentioned problems, the present invention also provides a method for hanging a vertical rope to the power transmission line for the flying device, see Figure 7, the method includes:
S10、在飞行装置起飞前,将弧垂绳挂载在飞行装置上;S10, before the flight device takes off, mount the sag rope on the flight device;
挂载弧垂绳的方法可参见上述悬挂装置挂载弧垂绳的相关描述,此处不再一一赘述。For the method of mounting the sag rope, please refer to the related description of the suspension device mounting the sag rope, and details will not be repeated here.
S20、在飞行装置起飞后,使该飞行装置实时拍摄弧垂绳和输电线路的图像,并在图像的中心位置处添加标记且显示该图像;S20. After the flying device takes off, make the flying device take images of the sag rope and the power transmission line in real time, add a mark at the center of the image and display the image;
关于步骤S20的相关描述可参见上述摄像装置和控制终端的相关描述,此处不再一一赘述。For related descriptions of step S20, refer to the related descriptions of the above-mentioned camera device and control terminal, which will not be repeated here.
S30、检测标记的位置,当标记位置从输电线路的导线一侧移至另一侧时,使飞行装置松开弧垂绳以向输电线路挂弧垂绳。S30. Detect the position of the mark. When the position of the mark moves from one side of the wire of the power transmission line to the other side, the flying device is released from the sag rope to hang the sag rope to the power transmission line.
地面操作人员(作业人员)检测标记的位置,在显示的图像中检测到当标记位置从输电线路的导线一侧移至另一侧时,松开弧垂绳以向输电线路挂弧垂绳。The ground operator (operator) detects the position of the mark, and when it is detected in the displayed image that the position of the mark moves from one side of the conductor of the transmission line to the other, releases the sag rope to hang the sag line to the transmission line.
需要说明的是步骤S10、S20和S30所述的飞行装置为前述的飞行装置,当然飞行装置中的无人飞行器可以为四轴无人飞行器,此处不再一一赘述。It should be noted that the flying devices described in steps S10, S20 and S30 are the aforementioned flying devices. Of course, the unmanned aerial vehicle in the flying device may be a four-axis unmanned aerial vehicle, which will not be repeated here.
综上所述,本发明通过在飞行装置上设置悬挂装置,并使悬挂装置挂住弧垂绳或抛掉弧垂绳。借此,实现在挂弧垂绳时,提高工作效率和作业人员的安全系数,还可以在任何高度的输电线路上悬挂弧垂绳。In summary, the present invention sets the suspension device on the flying device, and makes the suspension device hang the sag rope or throw away the sag rope. Thereby, when hanging the sag rope, the work efficiency and the safety factor of the operators can be improved, and the sag rope can also be hung on the transmission line of any height.
以上所述仅为本发明的较佳实施例,并不用以限制本发明,凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention shall be included in the protection of the present invention. within range.
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Families Citing this family (28)
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Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5328133A (en) * | 1993-07-30 | 1994-07-12 | Marc Charest | System for carrying equipment and/or a workman to a high voltage line or installations |
EP0697335B1 (en) * | 1993-02-18 | 1999-07-28 | McLean, Ian | Hydro service system assembly |
CN101707334A (en) * | 2009-11-24 | 2010-05-12 | 龚文基 | Static cable electric laying method and system of unmanned helicopter |
CN101964502A (en) * | 2010-08-24 | 2011-02-02 | 四川电力送变电建设公司 | Method for spreading initial guide rope with remote control fixed wing aircraft |
CN102064493A (en) * | 2010-11-02 | 2011-05-18 | 北京交通大学 | Method for paying off overhead transmission line by unmanned helicopter |
CN202840361U (en) * | 2012-10-11 | 2013-03-27 | 国家电网公司 | Primary guide rope remote control decoupling device |
CN203387114U (en) * | 2013-05-09 | 2014-01-08 | 衡水众翔电子科技有限公司 | Flight device for hanging sag rope on power transmission lines |
-
2013
- 2013-07-15 CN CN201320419022.2U patent/CN203387113U/en not_active Expired - Fee Related
- 2013-07-15 CN CN201320428846.6U patent/CN203387114U/en not_active Expired - Fee Related
- 2013-07-15 CN CN201310294555.7A patent/CN103368103B/en active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0697335B1 (en) * | 1993-02-18 | 1999-07-28 | McLean, Ian | Hydro service system assembly |
US5328133A (en) * | 1993-07-30 | 1994-07-12 | Marc Charest | System for carrying equipment and/or a workman to a high voltage line or installations |
CN101707334A (en) * | 2009-11-24 | 2010-05-12 | 龚文基 | Static cable electric laying method and system of unmanned helicopter |
CN101964502A (en) * | 2010-08-24 | 2011-02-02 | 四川电力送变电建设公司 | Method for spreading initial guide rope with remote control fixed wing aircraft |
CN102064493A (en) * | 2010-11-02 | 2011-05-18 | 北京交通大学 | Method for paying off overhead transmission line by unmanned helicopter |
CN202840361U (en) * | 2012-10-11 | 2013-03-27 | 国家电网公司 | Primary guide rope remote control decoupling device |
CN203387114U (en) * | 2013-05-09 | 2014-01-08 | 衡水众翔电子科技有限公司 | Flight device for hanging sag rope on power transmission lines |
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