CN110611270A - Stringing method and stringing track aircraft thereof - Google Patents
Stringing method and stringing track aircraft thereof Download PDFInfo
- Publication number
- CN110611270A CN110611270A CN201910830942.5A CN201910830942A CN110611270A CN 110611270 A CN110611270 A CN 110611270A CN 201910830942 A CN201910830942 A CN 201910830942A CN 110611270 A CN110611270 A CN 110611270A
- Authority
- CN
- China
- Prior art keywords
- cable
- tower
- overhead line
- aircraft
- branch
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 15
- 239000000835 fiber Substances 0.000 claims abstract description 50
- 238000005096 rolling process Methods 0.000 claims abstract description 8
- 238000004804 winding Methods 0.000 claims description 16
- 238000010521 absorption reaction Methods 0.000 claims description 4
- 238000007665 sagging Methods 0.000 claims description 3
- 238000001179 sorption measurement Methods 0.000 description 27
- 238000010276 construction Methods 0.000 description 7
- 238000006073 displacement reaction Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G1/00—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines
- H02G1/02—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables
- H02G1/04—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables for mounting or stretching
Abstract
The invention provides a stringing method and a stringing rail flying machine thereof, which comprise an aircraft body, wherein the aircraft body is provided with a fiber rope reeling and unreeling device for reeling and unreeling a fiber rope, at least two walking devices for walking on the fiber rope and a cable fixing device for fixing a cable, the walking devices comprise a base arranged on the aircraft body, the upper end of the base is hinged with a support arm, the lower end of the support arm is provided with a roller for rolling on the fiber rope, the support arm inclines to the left side when the roller is contacted with the aircraft body, and the included angle between the support arm and the horizontal direction is more than 45 degrees and less than 90 degrees, so that the technical problem of preventing the stringing rail flying machine from backing up on the fiber rope is solved.
Description
Technical Field
The invention relates to a stringing method and a stringing rail aircraft thereof.
Background
In the construction process of many electric power wiring, often can receive the restriction of topography and environmental characteristics, for example the wiring process must stride across some rivers, lake branch, industry and commerce area, residential area, highway, railway, or hillock, canyon, forestry nursery stock district etc.. These factors lead to a geometric multiplication of construction costs, a delay or even an interruption of the construction progress, and the construction quality is therefore not guaranteed. The stringing operation is carried out by using the stringing rail aircraft, so that crops and nursery stocks can be effectively protected from being felled, the residential building does not need to be moved and dismantled, constructors do not trek and cross obstacles for a long distance any more, economic compensation caused by the construction is greatly saved, the construction progress is greatly accelerated, and the surface damage of the wire is reduced.
When the existing overhead line rail flying machine moves forwards on a fiber rope, if the existing overhead line rail flying machine is influenced by sudden strong wind, the existing overhead line rail flying machine is easily blown back by the strong wind and runs backwards on the fiber rope, so that a cable dragged by the overhead line rail flying machine is rotated and twisted together, and is not easy to be dragged again.
Disclosure of Invention
The invention provides a stringing method and a stringing rail flying machine thereof, which aim to solve the technical problem of preventing the stringing rail flying machine from backing up on a fiber rope.
The technical scheme of the invention is realized as follows: the utility model provides an overhead line track flying machine, includes the aircraft body, the aircraft body is equipped with fine rope winding and unwinding devices, at least two running gear that are used for walking on fine rope, the cable fixing device who is used for fixed cable that are used for receiving and unwinding fine rope, running gear is including the base of locating the aircraft body, the base upper end articulates there is the support arm, the support arm lower extreme is equipped with and is used for rolling gyro wheel on fine rope, the support arm is to the left side slope when gyro wheel and aircraft body contact, and the support arm is for being greater than 45 and being less than 90 with the contained angle of horizontal direction.
Further, be equipped with the elasticity rand release that is used for releasing elasticity rand on the aircraft body, be triangle-shaped behind the elasticity rand buckle, the elasticity rand includes first branch, second branch, third branch, the second branch is equipped with the buckle, the third branch is equipped with the trip, elasticity rand release is located the running gear left side, elasticity rand release includes the bin with aircraft body fixed connection, be equipped with in the bin and store the chamber, it is triangle-shaped to store the chamber along length direction's cross section, triangle-shaped's cross section reduces gradually from a left side to its triangle-shaped's waist length in the right side, the bin left end is equipped with release mechanism, release mechanism includes two relative settings and with bin articulated clamping piece, the inboard that the clamping piece is relative is equipped with and is used for the second branch rand to elasticity rand, The third branch carries out spacing draw-in groove, the upper end of one of them clamping piece is equipped with the electro-magnet, and the upper end of another clamping piece is equipped with the absorption piece that mutually supports with the electro-magnet to make electro-magnet and absorption piece be close to each other when making the electro-magnet circular telegram, cable fixing device is located between elastic collar release and the running gear, the bin bottom is equipped with the clearing hole that is used for passing through fine rope and cable.
Furthermore, the opposite adsorption surfaces of the electromagnet and the adsorption block are symmetrical inclined surfaces, so that the adsorption surfaces of the electromagnet and the adsorption block can be superposed after the electromagnet and the adsorption block are attracted.
Further, fine rope winding and unwinding devices include with aircraft body fixed connection's shell, be equipped with the drum in the shell, the drum winding has fine rope.
Further, the cable fixing device comprises a fixing hole for fixing the cable and a through hole for enabling the fiber rope to pass through, and the fixing hole is provided with a fixing bolt penetrating through the side wall of the fixing hole.
Further, the clamping piece is V-shaped.
Further, the inner side surface of the clamping piece is flush with the inner side surface of the storage cavity so that the elastic clamping ring can smoothly slide to the clamping groove.
The present invention also provides a stringing method including the stringing rail aircraft according to any one of claims 1 to 7, comprising the steps of: (1) the overhead line track flying machine loads the fiber rope to take off, and when the overhead line track flying machine reaches the top end of the first tower, workers positioned at the top end of the first tower tie one end of the fiber rope to the first tower; (2) the overhead line rail aircraft drags the fiber rope to fly to a second tower, and workers at the top end of the second tower press the fiber rope below the roller, sequentially penetrate through the through hole and are tied to the second tower; (3) one end of the cable penetrates through the through hole and then is fixed in the fixing hole; (4) and starting the overhead line track aircraft to drag the cable along the fiber rope so as to drag the cable from the top end of the second tower to the top end of the first tower.
Further, in the step (4), an elastic clamping ring is released at intervals in the process of dragging the cable from the top end of the second tower to the top end of the first tower so as to prevent the cable from sagging and increase the difficulty of dragging the cable to move forwards.
By adopting the technical scheme, the invention has the beneficial effects that: when the rollers of the overhead line track flying machine contact with the aircraft body, the support arm inclines to the left side, namely the inclination direction of the support arm is opposite to the displacement direction of the overhead line track flying machine, the included angle between the support arm and the horizontal direction is more than 45 degrees and less than 90 degrees, if the overhead line track flying machine backs up due to insufficient power or the influence of factors such as headwind and the like, the included angle between the support arm and the horizontal direction tends to increase, namely the rollers tend to approach the base, at the moment, the rollers press the fiber ropes between the rollers and the aircraft body, and the backing-up of the overhead line track flying machine on the fiber ropes is prevented, namely the invention has the function of preventing the overhead line track flying machine from backing up on the fiber ropes.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
FIG. 1 is a position distribution diagram of a first tower and a second tower according to the present invention;
FIG. 2 is a schematic illustration of the construction of the stringing rail aircraft of the present invention;
FIG. 3 is a schematic illustration of the stringing track aircraft with the resilient collar release removed in accordance with the present invention;
FIG. 4 is a schematic view of the structure of the resilient collar release mechanism of the present invention;
FIG. 5 is a front view of the resilient collar release apparatus of the present invention;
FIG. 6 is a schematic view of the elastic collar of the present invention;
FIG. 7 is a cross-sectional view of the cord take-up and pay-off device of the present invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
An embodiment 1 of an overhead line track flying machine is shown in fig. 1-5 and comprises an aircraft body 1, wherein the aircraft body is provided with a fiber rope winding and unwinding device 2 for winding and unwinding fiber ropes, at least two traveling devices 3 for traveling on the fiber ropes and a cable fixing device 4 for fixing cables, the traveling devices comprise bases 5 arranged on the aircraft body, the upper ends of the bases are hinged with support arms 6, the lower ends of the support arms are provided with idler wheels 7 for rolling on the fiber ropes, the support arms incline to the left when the idler wheels are in contact with the aircraft body, and the included angles between the support arms and the horizontal direction are larger than 45 degrees and smaller than 90 degrees. When the rollers of the stringing track flying machine contact with the aircraft body, the supporting arm inclines to the left side, namely the inclination direction of the supporting arm is opposite to the displacement direction of the stringing track flying machine, the included angle between the supporting arm and the horizontal direction is more than 45 degrees and less than 90 degrees, if the stringing track flying machine backs up due to insufficient power or the influence of factors such as headwind and the like, the included angle between the supporting arm and the horizontal direction tends to increase, namely the rollers tend to approach the base, and the rollers press the fiber ropes between the rollers and the aircraft body at the moment, so that the backing up of the stringing track flying machine on the fiber ropes is prevented.
An embodiment 2 of a stringing rail vehicle comprises an aircraft body 1, the aircraft body is provided with a fiber rope winding and unwinding device 2 for winding and unwinding a fiber rope, at least two walking devices 3 for walking on the fiber rope and a cable fixing device 4 for fixing a cable, the walking devices comprise a base 5 arranged on the aircraft body, the upper end of the base is hinged with a support arm 6, the lower end of the support arm is provided with a roller 7 for rolling on the fiber rope, the support arm inclines to the left side when the roller is contacted with the aircraft body, the included angle between the support arm and the horizontal direction is more than 45 degrees and less than 90 degrees, the aircraft body is provided with an elastic clamping ring releasing device 8 for releasing an elastic clamping ring 9, the elastic clamping ring is triangular after being buckled, the elastic clamping ring comprises a first branch 10, a second branch 11 and a third branch 12, the second branch is provided with a buckling ring 13, the third branch is provided with a buckling hook 14, the elastic collar releasing device is positioned on the left side of the walking device and comprises a storage box 15 fixedly connected with the aircraft body, a storage cavity 16 is arranged in the storage box, the cross section of the storage cavity along the length direction is triangular, the triangular cross section is gradually reduced from left to right, the triangular waist length is gradually reduced, a releasing mechanism is arranged at the left end of the storage box and comprises two clamping pieces 17 which are oppositely arranged and hinged with the storage box, a clamping groove 18 used for limiting a second branch and a third branch of the elastic collar is arranged on the opposite inner side of each clamping piece, the upper end of one clamping piece is provided with an electromagnet 19, the upper end of the other clamping piece is provided with an adsorption block 20 matched with the electromagnet, so that the electromagnet and the adsorption block are close to each other when the electromagnet is electrified, the cable fixing device is positioned between the elastic retainer ring releasing device and the walking device, and the bottom of the storage box is provided with a through hole 21 for passing a fiber rope and a cable. When the overhead line track aircraft drags the cable walking on the fine rope, the cable tip is fixed in cable fixing device after passing the clearing hole, and the fine rope passes behind the clearing hole and cooperates with the gyro wheel so that the gyro wheel can roll on the fine rope. The fine rope and the cable all get into from the rand exit of elasticity rand release left end this moment promptly, go out from the clearing hole of bin bottom, and elasticity rand cover is in fine rope and cable this moment promptly, and when elasticity rand popped out from the bin, the elasticity rand cover is in fine rope and cable in order to prevent to overlap in fine rope and cable separation.
An embodiment 3 of a stringing rail vehicle is shown in fig. 1-5, and comprises an aircraft body 1, the aircraft body is provided with a fiber rope winding and unwinding device 2 for winding and unwinding a fiber rope, at least two walking devices 3 for walking on the fiber rope, and a cable fixing device 4 for fixing a cable, the walking devices comprise a base 5 arranged on the aircraft body, the upper end of the base is hinged with a support arm 6, the lower end of the support arm is provided with a roller 7 for rolling on the fiber rope, the support arm inclines to the left side when the roller is contacted with the aircraft body, the included angle between the support arm and the horizontal direction is more than 45 degrees and less than 90 degrees, the aircraft body is provided with an elastic collar releasing device 8 for releasing an elastic collar 9, the elastic collar is triangular after being buckled, the elastic collar comprises a first branch 10, a second branch 11 and a third branch 12, the second branch is provided with a buckle 13, and the third branch is provided, the elastic collar releasing device is positioned on the left side of the walking device and comprises a storage box 15 fixedly connected with the aircraft body, a storage cavity 16 is arranged in the storage box, the cross section of the storage cavity along the length direction is triangular, the triangular cross section is gradually reduced from the left to the right of the waist length of the triangle, a releasing mechanism is arranged at the left end of the storage box and comprises two clamping pieces 17 which are oppositely arranged and hinged with the storage box, a clamping groove 18 for limiting the second branch and the third branch of the elastic collar is arranged on the opposite inner side of each clamping piece, an electromagnet 19 is arranged at the upper end of one clamping piece, an adsorption block 20 matched with the electromagnet is arranged at the upper end of the other clamping piece, so that the electromagnet and the adsorption block are close to each other when the electromagnet is electrified, the cable fixing device is positioned between the elastic collar releasing device and the walking device, and a through hole 21 for, the opposite adsorption surfaces 22 of the electromagnet and the adsorption block are symmetrically inclined surfaces, so that the adsorption surfaces of the electromagnet and the adsorption block can be superposed after the electromagnet and the adsorption block are attracted.
An embodiment 4 of a stringing rail vehicle is shown in fig. 1-5, and comprises an aircraft body 1, the aircraft body is provided with a fiber rope winding and unwinding device 2 for winding and unwinding a fiber rope, at least two walking devices 3 for walking on the fiber rope, and a cable fixing device 4 for fixing a cable, the walking devices comprise a base 5 arranged on the aircraft body, the upper end of the base is hinged with a support arm 6, the lower end of the support arm is provided with a roller 7 for rolling on the fiber rope, the support arm inclines to the left side when the roller is contacted with the aircraft body, the included angle between the support arm and the horizontal direction is more than 45 degrees and less than 90 degrees, the aircraft body is provided with an elastic collar releasing device 8 for releasing an elastic collar 9, the elastic collar is triangular after being buckled, the elastic collar comprises a first branch 10, a second branch 11 and a third branch 12, the second branch is provided with a buckle 13, and the third branch is provided, the elastic collar releasing device is positioned on the left side of the walking device and comprises a storage box 15 fixedly connected with the aircraft body, a storage cavity 16 is arranged in the storage box, the cross section of the storage cavity along the length direction is triangular, the triangular cross section is gradually reduced from the left to the right of the waist length of the triangle, a releasing mechanism is arranged at the left end of the storage box and comprises two clamping pieces 17 which are oppositely arranged and hinged with the storage box, a clamping groove 18 for limiting the second branch and the third branch of the elastic collar is arranged on the opposite inner side of each clamping piece, an electromagnet 19 is arranged at the upper end of one clamping piece, an adsorption block 20 matched with the electromagnet is arranged at the upper end of the other clamping piece, so that the electromagnet and the adsorption block are close to each other when the electromagnet is electrified, the cable fixing device is positioned between the elastic collar releasing device and the walking device, and a through hole 21 for, the two opposite adsorption surfaces 22 of the electromagnet and the adsorption block are symmetrically inclined surfaces so that the adsorption surfaces of the electromagnet and the adsorption block can be superposed after the electromagnet and the adsorption block are attracted, the fine rope winding and unwinding device 2 comprises a shell 23 fixedly connected with the aircraft body, a wire coil 24 is arranged in the shell, a fine rope 25 is wound on the wire coil, and the wire coil 24 rotates around a shaft 26.
An embodiment 5 of a stringing rail vehicle is shown in fig. 1-5, and comprises an aircraft body 1, the aircraft body is provided with a fiber rope winding and unwinding device 2 for winding and unwinding a fiber rope, at least two walking devices 3 for walking on the fiber rope, and a cable fixing device 4 for fixing a cable, the walking devices comprise a base 5 arranged on the aircraft body, the upper end of the base is hinged with a support arm 6, the lower end of the support arm is provided with a roller 7 for rolling on the fiber rope, the support arm inclines to the left side when the roller is contacted with the aircraft body, the included angle between the support arm and the horizontal direction is more than 45 degrees and less than 90 degrees, the aircraft body is provided with an elastic collar releasing device 8 for releasing an elastic collar 9, the elastic collar is triangular after being buckled, the elastic collar comprises a first branch 10, a second branch 11 and a third branch 12, the second branch is provided with a buckle 13, and the third branch is provided, the elastic collar releasing device is positioned on the left side of the walking device and comprises a storage box 15 fixedly connected with the aircraft body, a storage cavity 16 is arranged in the storage box, the cross section of the storage cavity along the length direction is triangular, the triangular cross section is gradually reduced from the left to the right of the waist length of the triangle, a releasing mechanism is arranged at the left end of the storage box and comprises two clamping pieces 17 which are oppositely arranged and hinged with the storage box, a clamping groove 18 for limiting the second branch and the third branch of the elastic collar is arranged on the opposite inner side of each clamping piece, an electromagnet 19 is arranged at the upper end of one clamping piece, an adsorption block 20 matched with the electromagnet is arranged at the upper end of the other clamping piece, so that the electromagnet and the adsorption block are close to each other when the electromagnet is electrified, the cable fixing device is positioned between the elastic collar releasing device and the walking device, and a through hole 21 for, the relative adsorption plane 22 of electro-magnet and adsorption block is the inclined plane of symmetry, so that both adsorption planes can coincide after electro-magnet and adsorption block actuation, fine rope coiling and uncoiling device 2 includes the shell 23 with aircraft body fixed connection, be equipped with drum 24 in the shell, the drum winding has fine rope 25, drum 24 rotates around axle 26, cable fixing device is including the fixed orifices 27 that are used for fixed cable, a perforation 28 for making fine rope pass through, the fixed orifices is equipped with fixing bolt 29 who passes its lateral wall, the clamping piece is the V-arrangement, the inboard surface of clamping piece and the storage intracavity side parallel and level of side so that the smooth slip of elasticity rand to draw-in groove.
An overhead line method embodiment 1, including the overhead line track aircraft of any of embodiments 1-5 above, comprising the steps of: (1) the overhead line track flying machine loads the fiber rope to take off, and when the overhead line track flying machine reaches the top end of the first tower 100, workers positioned at the top end of the first tower tie one end of the fiber rope to the first tower; (2) the overhead line rail aircraft drags the fiber rope to fly to the second tower 200, and workers at the top end of the second tower press the fiber rope below the roller, sequentially penetrate through the through hole and are tied to the second tower; (3) one end of the cable penetrates through the through hole and then is fixed in the fixing hole; (4) and starting the overhead line track aircraft to drag the cable along the fiber rope so as to drag the cable from the top end of the second tower to the top end of the first tower.
An embodiment 2 of the stringing method is different from the embodiment 1 of the stringing method in that in the step (4), an elastic clamping ring is released at intervals in the process of dragging the cable from the top end of the second tower to the top end of the first tower so as to prevent the cable from sagging and increase the difficulty of dragging the cable to move ahead.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.
Claims (9)
1. The utility model provides an overhead line track flying machine, includes the aircraft body, its characterized in that, the aircraft body is equipped with fine rope winding and unwinding devices, two at least running gear that are used for walking on fine rope, the cable fixing device who is used for fixed cable that are used for receiving and unwinding fine rope, running gear is including the base of locating the aircraft body, the base upper end articulates there is the support arm, the support arm lower extreme is equipped with and is used for rolling gyro wheel on fine rope, the support arm is to the left side slope when gyro wheel and aircraft body contact, and the support arm is for being greater than 45 and being less than 90 with the contained angle of horizontal direction.
2. The overhead line track flying machine of claim 1, wherein the aircraft body is provided with an elastic collar release device for releasing the elastic collar, the elastic collar is triangular after being fastened, the elastic collar comprises a first branch, a second branch and a third branch, the second branch is provided with a buckle, the third branch is provided with a hook, the elastic collar release device is located on the left side of the traveling device, the elastic collar release device comprises a storage box fixedly connected with the aircraft body, a storage cavity is arranged in the storage box, the cross section of the storage cavity in the length direction is triangular, the cross section of the triangle is gradually reduced from left to right in the waist length of the triangle, the left end of the storage box is provided with a release mechanism, the release mechanism comprises two clamping pieces which are oppositely arranged and hinged with the storage box, and the opposite inner sides of the clamping pieces are provided with a second branch for the elastic collar, The third branch carries out spacing draw-in groove, the upper end of one of them clamping piece is equipped with the electro-magnet, and the upper end of another clamping piece is equipped with the absorption piece that mutually supports with the electro-magnet to make electro-magnet and absorption piece be close to each other when making the electro-magnet circular telegram, cable fixing device is located between elastic collar release and the running gear, the bin bottom is equipped with the clearing hole that is used for passing through fine rope and cable.
3. The overhead line track flying machine according to claim 2, wherein the opposing attraction surfaces of the electromagnet and the attraction block are inclined surfaces that are symmetrical so that the attraction surfaces of the electromagnet and the attraction block can overlap after they are attracted.
4. The overhead line track aircraft of claim 3, wherein the cord take-up and pay-off device comprises a housing fixedly attached to the aircraft body, wherein a spool is disposed within the housing, and wherein the spool is wrapped with the cord.
5. The overhead line track aircraft according to claim 4, wherein the cable fixing means comprises a fixing hole for fixing the cable, a through hole for passing the cord, the fixing hole being provided with a fixing bolt passing through a side wall thereof.
6. The overhead line rail aircraft of claim 5, wherein the clamp is V-shaped.
7. The overhead line track aircraft of claim 6, wherein the clamp inner side surface is flush with the storage cavity inner side surface so that the resilient collar can slide smoothly into the slot.
8. A stringing method, comprising the stringing rail aircraft according to any one of claims 1-7, comprising the steps of: (1) the overhead line track flying machine loads the fiber rope to take off, and when the overhead line track flying machine reaches the top end of the first tower, workers positioned at the top end of the first tower tie one end of the fiber rope to the first tower; (2) the overhead line rail aircraft drags the fiber rope to fly to a second tower, and workers at the top end of the second tower press the fiber rope below the roller, sequentially penetrate through the through hole and are tied to the second tower; (3) one end of the cable penetrates through the through hole and then is fixed in the fixing hole; (4) and starting the overhead line track aircraft to drag the cable along the fiber rope so as to drag the cable from the top end of the second tower to the top end of the first tower.
9. A stringing method according to claim 8, characterized in that in the step (4) the cable is dragged from the top end of the second tower to the top end of the first tower, and at intervals, an elastic collar is released to prevent the cable from sagging and increase the difficulty of dragging the cable forward.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910830942.5A CN110611270B (en) | 2019-09-04 | Stringing method and stringing orbital aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910830942.5A CN110611270B (en) | 2019-09-04 | Stringing method and stringing orbital aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110611270A true CN110611270A (en) | 2019-12-24 |
| CN110611270B CN110611270B (en) | 2024-04-26 |
Family
ID=
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR617554A (en) * | 1926-04-09 | 1927-02-22 | Launch and landing device for airplanes | |
| JP3167261U (en) * | 2011-01-31 | 2011-04-14 | 山本 寛 | Rope guide device |
| CN202050187U (en) * | 2011-05-20 | 2011-11-23 | 河南送变电建设公司 | Device for preventing traction rope from deviating |
| CN204526870U (en) * | 2015-04-15 | 2015-08-05 | 中铁武汉电气化局集团有限公司 | A kind of wiring railway contact wires car |
| WO2015143923A1 (en) * | 2014-03-24 | 2015-10-01 | 郭强 | Fast aerial cable transit system |
| CA2875552A1 (en) * | 2014-04-08 | 2015-10-08 | Wall Industries Inc. | An apparatus for moving a line cart along a cable |
| CN205675880U (en) * | 2016-06-02 | 2016-11-09 | 国网江西省电力公司南昌供电分公司 | A kind of cable laying frame |
| CN107819296A (en) * | 2017-11-06 | 2018-03-20 | 孙哲涛 | High voltage cable crusing robot walking clipping mechanism |
| CN108248888A (en) * | 2017-12-25 | 2018-07-06 | 成都优力德新能源有限公司 | For being tethered at the automatic deploying and retracting line apparatus of unmanned plane during flying device |
| US20190061976A1 (en) * | 2017-08-24 | 2019-02-28 | Aurora Flight Sciences Corporation | Rail Recovery System For Aircraft |
| CN211126811U (en) * | 2019-09-04 | 2020-07-28 | 国网河南省电力公司三门峡供电公司 | Overhead line track flying machine |
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR617554A (en) * | 1926-04-09 | 1927-02-22 | Launch and landing device for airplanes | |
| JP3167261U (en) * | 2011-01-31 | 2011-04-14 | 山本 寛 | Rope guide device |
| CN202050187U (en) * | 2011-05-20 | 2011-11-23 | 河南送变电建设公司 | Device for preventing traction rope from deviating |
| WO2015143923A1 (en) * | 2014-03-24 | 2015-10-01 | 郭强 | Fast aerial cable transit system |
| CA2875552A1 (en) * | 2014-04-08 | 2015-10-08 | Wall Industries Inc. | An apparatus for moving a line cart along a cable |
| CN204526870U (en) * | 2015-04-15 | 2015-08-05 | 中铁武汉电气化局集团有限公司 | A kind of wiring railway contact wires car |
| CN205675880U (en) * | 2016-06-02 | 2016-11-09 | 国网江西省电力公司南昌供电分公司 | A kind of cable laying frame |
| US20190061976A1 (en) * | 2017-08-24 | 2019-02-28 | Aurora Flight Sciences Corporation | Rail Recovery System For Aircraft |
| CN107819296A (en) * | 2017-11-06 | 2018-03-20 | 孙哲涛 | High voltage cable crusing robot walking clipping mechanism |
| CN108248888A (en) * | 2017-12-25 | 2018-07-06 | 成都优力德新能源有限公司 | For being tethered at the automatic deploying and retracting line apparatus of unmanned plane during flying device |
| CN211126811U (en) * | 2019-09-04 | 2020-07-28 | 国网河南省电力公司三门峡供电公司 | Overhead line track flying machine |
Non-Patent Citations (1)
| Title |
|---|
| 宋颖等: "架空输电线路工程架线施工双滑车设置方法", 科技资讯, no. 8, 31 December 2016 (2016-12-31), pages 26 - 27 * |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE3723393A1 (en) | ARRANGEMENT FOR LAYING SEISMIC CABLES | |
| CN211126811U (en) | Overhead line track flying machine | |
| EP3748123A1 (en) | Tunnel wall-adhering shuttle platform and tunnel monitoring apparatus | |
| US20140151616A1 (en) | Medium traverse | |
| CN110611270A (en) | Stringing method and stringing track aircraft thereof | |
| CN110611270B (en) | Stringing method and stringing orbital aircraft | |
| CN103950835B (en) | Collapsible track drawing device | |
| AU2005202796B2 (en) | Cable Reeler and Cable Retrieval Method | |
| CN202214033U (en) | Uncoiling and paving device for double-coiled adhesive tape of belt type conveyor | |
| CN214421988U (en) | Automatic wire winding and hanging device of trolley | |
| JPH01206809A (en) | Device for removing matter caught by transmission line | |
| CN114314179A (en) | Well cable conductor winding and unwinding devices | |
| JP4562194B2 (en) | Overhead cable laying method | |
| CN217125062U (en) | Pulley device, towing equipment and navigation equipment | |
| CN217920831U (en) | Cable guider applied to external cable of ship | |
| KR20040065431A (en) | The brightness emergency coil prop moving carrier | |
| CN214652765U (en) | Fixed-point operation machine power supply device and operation machine | |
| CN212712246U (en) | Portable wire transmission frame | |
| CN215042235U (en) | Constant-tension wire barrow for contact net | |
| CN217322755U (en) | Cable paying-off device | |
| CN214879076U (en) | Cable coiling device for electric power engineering construction | |
| CN105775901A (en) | Outdoor optical cable winding device | |
| JPS5836121B2 (en) | Construction method for long cables | |
| CN113928344A (en) | Suspension type monorail transportation system suitable for transport agricultural product in steep area | |
| CN115196426A (en) | Cable guider applied to external cable of ship |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant |