WO2020181959A1 - 矿井暗道柔性推进布线方法 - Google Patents

矿井暗道柔性推进布线方法 Download PDF

Info

Publication number
WO2020181959A1
WO2020181959A1 PCT/CN2020/075621 CN2020075621W WO2020181959A1 WO 2020181959 A1 WO2020181959 A1 WO 2020181959A1 CN 2020075621 W CN2020075621 W CN 2020075621W WO 2020181959 A1 WO2020181959 A1 WO 2020181959A1
Authority
WO
WIPO (PCT)
Prior art keywords
cabin
cone
column
conveying
propulsion
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.)
Ceased
Application number
PCT/CN2020/075621
Other languages
English (en)
French (fr)
Inventor
张永亮
路成刚
黄萍
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Qingdao University of Technology
Original Assignee
Qingdao University of Technology
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Qingdao University of Technology filed Critical Qingdao University of Technology
Publication of WO2020181959A1 publication Critical patent/WO2020181959A1/zh
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Images

Classifications

    • 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
    • H02G1/06—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for laying cables, e.g. laying apparatus on vehicle

Definitions

  • This application relates to a flexible advance wiring method for underground tunnels in mines.
  • the technical problem to be solved by this application is generally to provide a device and method for a flexible propulsion wiring machine for underground tunnels in mines; the detailed technical problems to be solved and the beneficial effects obtained are described in detail in the following content and in conjunction with the content in the specific embodiments.
  • a flexible propulsion wiring method for underground tunnels in a mine by means of a wiring machine device, the device includes a conical propulsion cabin device, a cylindrical propulsion cabin device connected to the right end of the conical propulsion cabin device at the left end, and a wire feeding platform;
  • the method includes the following steps:
  • Step 1 First, place the fixed platform at the location of the wiring channel opening where the wiring is designed to be required, and place the conveying hole of the conveyor directly against the wiring opening that is designed to be wired; then, pass the column cabin transmission line through the conveying and transmission line.
  • Wire hole fix the first wire of the column cabin to be laid on the column cabin fixing buckle, and place the conical propulsion cabin device and the cylindrical propulsion cabin device in the wiring channel that needs to be wired;
  • the cone cabin motor drives the cone cabin power circle to rotate through the cone cabin driving wheel and the cone cabin transmission wheel
  • the column cabin motor drives the column cabin power circle to rotate through the column cabin driving wheel and the column cabin transmission wheel.
  • the cone cabin rubber pattern on the outer side of the cone cabin power circle and the column cabin power circle is driven and starts to rotate, and the conveying motor drives the conveying wheel to rotate through the conveying motor shaft, so that the conical propulsion cabin device and the cylindrical propulsion cabin device start to operate;
  • Step two under the action of the base of the fixed platform and the transmission of the column cabin transmission line, the conical propulsion cabin device and the cylindrical propulsion cabin device advance relative to the fixed platform to realize the propulsion action; at the same time, the rubber pattern in the cone cabin Under the action of friction with the inner wall of the wiring channel, forward power is generated; at the same time, under the action of friction between the transmission wheel and the column cabin transmission line, forward power is generated; finally, under the advancement of all forward power, the wiring machine device pulls the column The first wire of the cabin passes through the wiring channel that needs wiring work to complete the wiring work.
  • Figure 1 is a schematic diagram of the main structure of the present application.
  • Fig. 2 is a cross-sectional view of A-A in Fig. 1 of the present application.
  • Figure 3 is a B-B cross-sectional view of Figure 1 of the present application.
  • Fig. 4 is a schematic diagram of the main structure of the conveyor of the present application.
  • Fig. 5 is a side view of the main structure of the conveyor of the present application.
  • Fig. 6 is a sectional view of the transmission line of the present application.
  • cone cabin propulsion wheel 1 cone cabin rubber pattern 2, cone cabin power ring 3, cone cabin gap 4, column cabin drive ring 5, column cabin tooth pattern 6, column cabin transmission wheel 7, cone cabin bearing shaft 8, column Cabin driving wheel 9, column cabin transmission wheel 10, column cabin main shell 11, column cabin middle rubber ring 12, cone cabin large end shell 13, cone cabin adjustment belt 14, cone cabin tooth pattern 15, cone cabin opening 16, Cone cabin transmission wheel 17, cone cabin transmission shaft 18, cone cabin driving wheel 19, cone cabin motor 20, cone cabin small end shell 21, column cabin motor 22, column cabin rear cover 23, column cabin fixing buckle 24, column Cabin first wire 25, column cabin transmission line 26, conveyor 27, fixed platform 28, conveying motor shaft 29, column cabin rubber layer 30, column cabin wire bundle 31, conveying fixing frame 32, conveying wheel 33, conveying shaft 34 , Conveying motor 35, conveying line hole 36, column cabin control line 37, cone cabin connecting ring 38, cone cabin bracket 39, column cabin power ring 40, column cabin propulsion wheel 41, column cabin bearing shaft 42, column cabin opening 43 , Column cabin bracket 44, conveying bearing 45, column cabin second wire 46, platform bolt 47, platform
  • the cone propulsion cabin device includes a cone cabin large end shell 13, a cone cabin small end shell 21 coaxially arranged on the left side of the cone cabin large end shell 13 and connected to the left of the cone cabin large end shell 13.
  • the cone cabin connecting ring 38 between the port and the right port of the cone cabin small end shell 21, the cone cabin power ring coaxially sleeved on the outer wall of the cone cabin large end shell 13 and the cone cabin small end shell 21 3.
  • a cone adjustment belt 14 arranged at the cavity between the inner side wall of the cone cabin power ring 3 and the outer side wall of the cone cabin connecting ring 38 and the cross-section is a right triangle.
  • the conical cabin adjustment belt 14 is coaxially fixed on the outer side wall of the cone cabin power ring 3
  • Cone cabin propulsion wheel 1 conical cabin rubber pattern coaxially arranged on the outer side wall of the conical cabin propulsion wheel 1, cone cabin openings 16 distributed on the cone cabin connecting ring 38, and cone cabin bearings arranged at the cone cabin opening 16
  • cone bracket 39 arranged in the inner cavity of the small end shell 21 of the cone cabin, cone cabin axially arranged at the center of the cone cabin bracket 39
  • a motor 20, and a cone driving wheel 19 arranged on the output shaft of the cone motor 20 and meshing with the tooth pattern of the cone driving wheel 17;
  • the cone angle of the inner wall of the large end shell 13 of the cone cabin is greater than the cone angle of the inner wall of the small end shell 21 of the cone cabin, the inner wall side generatrix of the cone cabin power ring 3, the outer wall side generatrix of the cone cabin large end shell 13, and the cone
  • the outer wall side generatrix of the small end shell 21 of the cabin is collinear; the large end face of the cone cabin power ring 3 is coplanar with the large end face of the cone cabin large end shell 13; the hypotenuse of the cone cabin adjustment belt 14 and the inner wall of the cone cabin power ring 3 Fitted and fixedly connected, the inner side wall of the horizontal right-angle side of the cone adjustment belt 14 parallel to the axis line of the cone connection ring 38 is provided with cone gear 15 meshing with the gear of the cone transmission wheel 17.
  • the rubber pattern 2 of the cone cabin is arranged in a spiral shape
  • the large end shell 13 of the cone cabin is a steel cone-cylinder shell with a bottom diameter of 10 cm, a top diameter of 6, a height of 5 cm, and a thickness of 0.1 cm.
  • the small end shell 21 of the cone cabin is a diameter of 6 cm, a height of 3 cm, and a thickness of 0.1 cm steel cone-cylindrical shell
  • the cone cabin connecting ring 38 is a steel ring with a diameter of 6 cm, a height of 1.5 cm, and a thickness of 0.1 cm.
  • the large end shell 13 and the small end shell 21 of the cone cabin pass through the cone.
  • the cabin connecting ring 38 is rigidly connected to form a "cliff-shaped" cone.
  • Cone cabin power ring 3 is a conical steel power ring with a diameter of 13 cm, a height of 10 cm, and a thickness of 1 cm.
  • the cone power ring 3 covers the large end shell 13 and the small end shell 21 of the cone cabin.
  • the bottom surface of the cone cabin power ring 3 and the bottom surface of the cone cabin large end shell 13 are on the same plane.
  • a ring of cone adjustment belt 14 is set at the position where the inner wall of the cone cabin power ring 3 is opposite to the cone cabin connecting ring 38.
  • the cross section of the cone cabin adjustment belt 14 is a right triangle.
  • the bottom of the cone cabin adjustment belt 14 is 1cm and the height is 2cm.
  • the oblique side of the cone cabin adjusting belt 14 is fixed to the inner wall of the cone cabin power ring 3, and the relatively long right-angle side of the cone cabin adjusting belt 14 is parallel to the cone cabin connecting ring 38.
  • Cone cabin tooth lines 15 are provided on the right-angled surface of the cone cabin adjusting belt 14 with a relatively long section.
  • a layer of 3 cm thick cone propulsion wheel 1 is fixedly installed on the outer side of the cone power circle 3, and the cone power circle 3 and the cone propulsion wheel 1 are a whole.
  • a series of spiral cone rubber patterns 2 with a depth of 2 cm and a width of 1 cm and a spacing of 2 cm are arranged on the outer side of the cone driving wheel 1.
  • Three cone compartment openings 16 with a length of 4 cm and a width of 1.5 cm are provided on the cone compartment connecting ring 38, and the included angle between two adjacent cone compartment openings 16 is 120°.
  • a cone bearing shaft 8 with an outer diameter of 0.5 cm is installed at the center of each cone opening 16, and a steel cone transmission wheel 17 with a diameter of 3.5 cm and a height of 1 cm is installed outside the cone shaft bearing shaft 8.
  • Cone cabin tooth pattern 15 is provided on the outside of the cone cabin transmission wheel 17.
  • the cone cabin tooth pattern 15 on the cone cabin transmission wheel 17 and the cone cabin tooth pattern 15 on the cone cabin adjustment belt 14 are exactly the same, when the cone cabin transmission wheel 17 rotates
  • the cone adjustment belt 14 can be driven to rotate.
  • a cone motor 20 with a length of 4 cm, a width of 4 cm, and a height of 3 cm is fixed in the small end shell 21 of the cone cabin through four cone cabin brackets 39.
  • a cone motor 20 with a diameter of 3 cm is rigidly installed on the cone cabin drive shaft 18 of the cone cabin motor 20.
  • the cone drive wheel 19 made of steel with a height of 1cm
  • the cone gear 15 is set on the outside of the cone drive wheel 19, the cone gear 15 on the cone drive wheel 19 and the cone gear on the cone drive wheel 17
  • the pattern 15 is exactly the same, when the cone drive wheel 19 rotates, the cone drive wheel 17 can be driven to rotate.
  • the cylindrical propulsion cabin device includes a column cabin main shell 11, a column cabin power ring 40 coaxially sleeved outside the column cabin main shell 11 and whose right end surface is coplanar with the right end surface of the column cabin main shell 11, and a column cabin power ring 40 fixedly arranged in the column cabin
  • Column cabin propelling wheel 41 fixedly sleeved on the outside of the column cabin power ring 40 and arranged in an axial array, and column cabin slot provided between adjacent column cabin propelling wheels 41 4.
  • the column cabin motor 22 axially arranged at the center of the column cabin bracket 44 in the column cabin main shell 11, the column cabin transmission shaft 10 arranged at the axial ends of the column cabin motor 22, and the column cabin transmission shaft 10 and
  • the column cabin driving wheel 9 meshed with the column cabin transmission wheel 7 tooth pattern, the column cabin rear cover 23 which is sealed and arranged at the right end of the column cabin main shell 11, the column cabin transmission line 26 arranged at the center of the column cabin rear cover 23, is arranged in The column cabin control line 37 at the center of the column cabin transmission line 26, the column cabin rubber layer 30 wrapped on the column cabin transmission line 26, the column cabin fixing buckle 24 arranged on the outside of the column cabin rear cover 23, and clamped on the column The column cabin first wire 25 on the cabin fixing buckle 24;
  • a cone cabin rubber pattern 2 is provided on the column cabin propelling wheel 41.
  • the column cabin transmission line 26 is formed by spirally weaving a plurality of column cabin wire bundles 31.
  • the column cabin control line 37 is connected to the cone cabin through the column cabin second wire 46.
  • the motor 20 and the column cabin motor 22 are electrically connected;
  • An intermediate rubber ring 12 is provided between the large end shell 13 of the cone cabin and the sealed end surface of the main shell 11 of the cylindrical propulsion cabin device column cabin;
  • the main shell 11 of the column cabin is a steel shell with a diameter of 10cm, a length of 30cm and a thickness of 0.1cm.
  • the column cabin power ring 40 is a steel cylinder with a diameter of 13cm, a height of 35cm and a thickness of 1cm.
  • the column cabin power ring 40 is used to hold the column.
  • the cabin main shell 11 is covered inside, and the bottom surface of the column cabin power ring 40 and the bottom surface of the column cabin main shell 11 are on the same plane.
  • Two steel column cabin drive rings 5 with a diameter of 13 cm and a width of 3 cm and a thickness of 1 cm are arranged on the inner wall of the column cabin power ring 40.
  • the column cabin drive ring 5 and the inner wall of the column cabin power ring 40 are fixed and integral with each other.
  • a column cabin tooth pattern 6 is arranged inside the column cabin driving ring 5.
  • Three column cabin openings 43 with a length of 4 cm and a width of 1.5 cm are provided on each column cabin driving ring 5 corresponding to the column cabin main shell 11, and the included angle between two adjacent column cabin openings 43 is 120°.
  • a column cabin bearing shaft 42 with an outer diameter of 0.5 cm is set at the center of each column cabin opening 43, and a steel column cabin transmission wheel 7 with a diameter of 3.5 cm and a height of 1 cm is installed outside the column cabin bearing shaft 42 ,
  • the column cabin tooth pattern 6 is arranged on the outside of the column cabin transmission wheel 7.
  • the column cabin tooth pattern 6 on the column cabin transmission wheel 7 and the column cabin tooth pattern 6 on the column cabin driving ring 5 exactly coincide, when the column cabin transmission wheel 7 rotates It can drive the column compartment driving ring 5 to rotate.
  • On the outer side of the column cabin power circle 40 three rings of column cabin propulsion wheels 41 with a width of 10 cm and a thickness of 3 cm are fixedly installed.
  • the column cabin power circle 40 and the column cabin propulsion wheels 41 are a whole, between the two adjacent sections of column cabin propulsion wheels 41 The distance between the two is 2cm, and a circle of column hatches 4 with a width of 2cm and a depth of 2cm is formed.
  • a series of spiral cone rubber patterns 2 with a depth of 2 cm, a width of 1 cm, and a spacing of 2 cm are arranged on the outside of the cylinder propulsion wheel 41.
  • a column cabin motor 22 with a length of 5 cm, a width of 5 cm and a height of 8 cm is fixed in the column cabin main shell 11 through four column cabin brackets 44, and a column cabin motor 22 with a diameter of 7 cm and a height is rigidly installed on the column cabin drive shafts 10 at both ends of the column cabin motor 22.
  • the rear end of the cylindrical propulsion cabin device is sealed and fixed by a steel pillar cabin rear cover 23 with a diameter of 10cm and a thickness of 1cm, and a pillar cabin transmission with a diameter of 5cm is fixedly installed at the center of the outside of the pillar cabin rear cover 23 Line 26, the column cabin transmission line 26 is formed by spirally weaving a number of column cabin wire bundles 31, a 0.3 cm diameter column cabin control line 37 is laid at the center of the column cabin transmission line 26, the column cabin transmission line 26 The outermost layer is tightly wrapped by a column cabin rubber layer 30 with a thickness of 0.5 cm, which can freely twist the column cabin transmission line 26 without changing the strength of the structure and state of the column cabin transmission line 26.
  • the column cabin control line 37 controls the switching, forward and reverse rotation and power supply of the cone cabin motor 20 and the column cabin motor 22 through the column cabin second wire 46.
  • a post compartment fixing buckle 24 is fixedly installed on the outside of the post compartment rear cover 23. The post compartment fixing buckle 24 can clamp the post compartment first wire 25 and drag the post compartment first wire 25 forward for wiring work.
  • the cone large end shell 13 of the cone propulsion cabin device and the column cabin main shell 11 of the cylindrical propulsion cabin device are rigidly sealed, so that the small end shell 21 of the cone cabin, the large end shell 13 of the cone cabin,
  • the main shell 11 of the column cabin becomes an integral structure.
  • a middle rubber ring 12 with an inner diameter of 10 cm and an outer diameter of 13 cm and a thickness of 0.5 cm is fixedly installed at the junction of the large end shell 13 of the cone cabin and the main shell 11 of the column cabin.
  • the middle rubber ring 12 is fixed on the main shell 11 of the column cabin because The elasticity of the rubber, the middle rubber ring 12 can relatively close the gap between the cone cabin power ring 3 and the cylinder cabin power ring 40, but does not affect the cone cabin power ring 3 and the cylinder cabin power ring 40 relative to the small end shell of the cone cabin
  • the body 21, the large-end shell 13 of the cone cabin and the main shell 11 of the column cabin rotate freely.
  • the wire feeding platform includes a fixed platform 28, and a conveyor 27 arranged on the fixed platform 28: the fixed platform 28 is preset with platform bolts 47,
  • the fixed platform 28 is a reinforced concrete cube with a length of 50 cm, a width of 50 cm, and a height of 50 cm.
  • the conveyor 27 is fixed on the fixed platform 28 by platform bolts 47 and nuts 48.
  • the conveyor 27 includes a conveying housing 49, a conveying line hole 36 arranged on the front and rear side walls of the conveying housing 49, six and three pairs of conveying fixing frames 32 distributed on the two inner side walls of the conveying line hole 36,
  • the conveying bearing 45 arranged on the conveying fixed frame 32, the conveying shaft 34 of the two conveying bearings 45 installed on the same axis line, the rubber conveying wheel 33 installed on the conveying shaft 34, and the conveying motor shaft 29
  • the conveying motor 35 is connected to the corresponding conveying shaft 34 in transmission.
  • the two ends of the conveying fixing frame 32 are fixedly connected to the two side walls of the conveying housing 49 provided with the conveying line holes 36, and the angle between the axis lines of every two conveying fixing frames 32 is sixty degrees; the three conveying fixing frames
  • the diameter of the triangle inscribed circle enclosed by the conveying wheel 33 on the frame 32 is the same as the outer diameter of the column cabin transmission line 26 and the outer column cabin rubber layer 30; the conveying motor 35 rotates synchronously;
  • the conveying shell 49 is 30 cm in length, 30 cm in width, and 30 cm in height and made of steel.
  • a conveying line hole 36 with a diameter of 6 cm is opened, and the two conveying line holes 36 correspond to each other.
  • On the two wall surfaces of the conveying housing 49 with the conveying line holes 36 are installed six steel conveying fixing frames 32 with a length of 30 cm, a width of 5 cm and a thickness of 1.5 cm.
  • the two ends of the conveying fixing frames 32 are fixed to the conveying housing 49.
  • Two wall surfaces are provided with conveying holes 36.
  • Six transport fixing frames 32 are set in pairs.
  • a conveying bearing 45 is installed in the middle of each conveying fixing frame 32, and a conveying shaft 34 is installed in the conveying bearing 45 of each group of conveying fixing frames 32.
  • the conveying shaft 34 can rotate freely in the conveying bearing 45.
  • the angle between two adjacent conveying shafts 34 is 60°.
  • a rubber conveying wheel 33 with a diameter of 4 cm and a height of 8 cm is fixedly installed on each conveying shaft 34.
  • the distance between the conveying fixing frame 32 and the conveying wheel 33 is 0.5 cm.
  • the diameter of the circumscribed circle between the three rubber wheels 33 is 5.5 cm, which is the same as the outer diameter of the column cabin transmission line 26 and the outer column cabin rubber layer 30.
  • the center of the circumscribed circle between the three rubber wheels 33 coincides with the center of the conveying hole 36.
  • a conveying motor 35 with a length of 3 cm, a width of 3 cm and a height of 3 cm is installed at the end of each conveying shaft 34.
  • the conveying motor shaft 29 of the conveying motor 35 is rigidly connected to the corresponding conveying rotating shaft 34.
  • the conveying motor shaft 29 drives the rotating shaft to rotate, and then drives the conveying wheel 33 to rotate.
  • the three conveying motors 35 rotate synchronously, so the three conveying wheels 33 also rotate synchronously.
  • a flexible advance wiring method for underground tunnels in a mine includes the following steps:
  • Step 1 First, place the fixed platform 28 at the position of the wiring channel opening where the wiring work is designed, and the transmission line hole 36 of the conveyor 27 is facing the wiring port where the wiring work is designed; then, the column compartment transmission line 26 Pass through the conveying hole 36, fix the column cabin first wire 25 that needs to be laid on the column cabin fixing buckle 24, and place the conical propulsion cabin device and the cylindrical propulsion cabin device in the wiring channel designed to require wiring work; Secondly, start the cone motor 20, the column motor 22 and the conveying motor 35 at the same time.
  • the cone motor 20 drives the cone power circle 3 to rotate through the cone drive wheel 19 and the cone drive wheel 17, and the column motor 22 passes the column
  • the cabin driving wheel 9 and the column cabin transmission wheel 7 drive the column cabin power ring 40 to rotate, the cone cabin power ring 3 and the cone cabin rubber pattern 2 outside the column cabin power ring 40 are driven and start to rotate, and the conveying motor 35 passes through the conveying motor shaft 29
  • the conveyor wheel 33 is driven to rotate, so that the conical propulsion cabin device and the cylindrical propulsion cabin device start to operate.
  • Step two under the action of the base of the fixed platform 28 and the transmission of the column cabin transmission line 26, the conical propulsion cabin device and the cylindrical propulsion cabin device advance relative to the fixed platform 28, thereby realizing the propulsion action; at the same time, in the cone
  • the friction between the rubber pattern 2 of the cabin and the inner wall of the wiring channel generates forward power; at the same time, the friction between the transmission wheel 33 and the column cabin transmission line 26 generates forward power; finally, under the advancement of all forward power,
  • the wiring machine device pulls the column compartment first wire 25 through the wiring channel that requires wiring work to complete the wiring work.
  • Cone cabin propulsion wheel 1 is pushed forward by the taper.
  • Cone cabin rubber pattern 2 has strong soil gripping ability, high efficiency, good wear resistance, and reasonable power output.
  • Cone cabin power ring 3 realizes power output, and the cone cabin gap 4 is convenient for installation.
  • the application realizes self-advancement in the underpass, self-coordinated wire feeding, convenient operation, good flexibility, and strong adaptability to the geological environment.
  • the application does not damage the wires, has reasonable design, low cost, strong and durable, safe and reliable, simple operation, time-saving and labor-saving, capital-saving, compact structure and convenient use.

Landscapes

  • Filling Or Emptying Of Bunkers, Hoppers, And Tanks (AREA)
  • Earth Drilling (AREA)
  • Lining And Supports For Tunnels (AREA)

Abstract

本申请涉及矿井暗道柔性推进布线方法，借助于，矿井暗道柔性推进布线机装置，其包括锥形推进舱装置、左端与锥形推进舱装置右端连接的柱形推进舱装置、以及送线平台。锥形推进舱装置包括锥舱大端部壳体、同轴设置在锥舱大端部壳体左侧的锥舱小端部壳体、连接在锥舱大端部壳体左端口与锥舱小端部壳体右端口之间的锥舱连接圈、同轴套装在锥舱大端部壳体与锥舱小端部壳体外侧壁上的锥舱动力圈、设置在锥舱动力圈内侧壁与锥舱连接圈外侧壁之间空腔处且截面为直角三角形的锥舱调节带、同轴固定设置在锥舱动力圈外侧壁上的锥舱推进轮、同轴设置在锥舱推进轮外侧壁上的锥舱橡胶纹；本申请设计合理、结构紧凑且使用方便。

Description

矿井暗道柔性推进布线方法 技术领域
本申请涉及矿井暗道柔性推进布线方法。
背景技术
目前，在矿井进行布线，现有的方案要不采用人工布线，要不布线机结构简单不合理，使用不方便，在矿井无法实现自动布线，对矿井适应性差，无法实现自动调节，经常出现，将线拉断，或线散落，对复杂地质环境适应能力差，输送线不方便，影响了布线工作。
发明内容
本申请所要解决的技术问题总的来说是提供一种矿井暗道柔性推进布线机装置及方法；详细解决的技术问题以及取得有益效果在后述内容以及结合具体实施方式中内容具体描述。
为解决上述问题，本申请所采取的技术方案是：
一种矿井暗道柔性推进布线方法，借助于布线机装置，该装置包括锥形推进舱装置、左端与锥形推进舱装置右端连接的柱形推进舱装置、以及送线平台；
该方法包括以下步骤：
步骤一，首先，将固定平台放置在设计需要布线工作的布线通道口位置，将输送器的输送输线孔正对着设计需要布线工作的布线口；然后，将柱舱传动线穿过输送输线孔，将需要布设的柱舱第一导线固定在柱舱固定扣上，将锥形推进舱装置与柱形推进舱装置置于设计需要布线工作的布线通道内；其次，同时启动锥舱电机、柱舱电机和输送电机，其中，锥舱电机通过锥舱主动轮、锥舱传动轮带动锥舱动力圈旋转，柱舱电机通过柱舱主动轮、柱舱传动轮带动柱舱动力圈旋转，锥舱动力圈和柱舱动力圈外侧的锥舱橡胶纹被带动并开始转动，输送电机通过输送电机轴带动输送输动轮转动，从而锥形推进舱装置与柱形推进舱装置开始运转；
步骤二，在固定平台的基座作用和柱舱传动线传动作用下，锥形推进舱装置与柱形推进舱装置相对于固定平台向前推进，从而实现推进动作；同时，在锥舱橡胶纹与布线通道内壁之间摩擦作用下，产生前进动力；同时在输送输动轮与柱舱传动线之间摩擦作用下，产生前进动力；最后，在所有前进动力的推进下，布线机装置拉着柱舱第一导线穿过需要布线工作的布线通道，完成布线工作。
本申请的有益效果不限于此描述，为了更好的便于理解，在具体实施方式部分进行了更加详细的描述。
附图说明
附图1是本申请的主体结构示意图。
附图2是本申请图1的A-A剖视图。
附图3是本申请图1的B-B剖视图。
附图4是本申请的输送器主体结构示意图。
附图5是本申请的输送器主体结构侧视图。
附图6是本申请的传动线剖面图。
其中：锥舱推进轮1、锥舱橡胶纹2、锥舱动力圈3、锥舱缺口4、柱舱驱动环5、柱舱齿纹6、柱舱传动轮7、锥舱轴承转轴8、柱舱主动轮9、柱舱传动轮10、柱舱主外壳11、柱舱中间橡胶圈12、锥舱大端部壳体13、锥舱调节带14、锥舱齿纹15、锥舱开口16、锥舱传动轮17、锥舱传动轴18、锥舱主动轮19、锥舱电机20、锥舱小端部壳体21、柱舱电机22、柱舱后盖23、柱舱固定扣24、柱舱第一导线25、柱舱传动线26、输送器27、固定平台28、输送电机轴29、柱舱橡胶层30、柱舱钢丝束31、输送固定架32、输送输动轮33、输送转轴34、输送电机35、输送输线孔36、柱舱控制线37、锥舱连接圈38、锥舱支架39、柱舱动力圈40、柱舱推进轮41、柱舱轴承转轴42、柱舱开口43、柱舱支架44、输送轴承45、柱舱第二导线46、平台螺栓47、平台螺母48。
具体实施方式
实施例：如图1-6本申请包括锥形推进舱装置、左端与锥形推进舱装置右端连接的柱形推进舱装置、以及送线平台。
锥形推进舱装置包括锥舱大端部壳体13、同轴设置在锥舱大端部壳体13左侧的锥舱小端部壳体21、连接在锥舱大端部壳体13左端口与锥舱小端部壳体21右端口之间的锥舱连接圈38、同轴套装在锥舱大端部壳体13与锥舱小端部壳体21外侧壁上的锥舱动力圈3、设置在锥舱动力圈3内侧壁与锥舱连接圈38外侧壁之间空腔处且截面为直角三角形的锥舱调节带14、同轴固定设置在锥舱动力圈3外侧壁上的锥舱推进轮1、同轴设置在锥舱推进轮1外侧壁上的锥舱橡胶纹2、分布在锥舱连接圈38上的锥舱开口16、设置在锥舱开口16处的锥舱轴承转轴8、安装在锥舱轴承转轴8上的锥舱传动轮17、设置在锥舱小端部壳体21内 腔中的锥舱支架39、轴向设置在锥舱支架39中心处的锥舱电机20、以及设置在锥舱电机20的输出轴上且与锥舱传动轮17齿纹啮合的锥舱主动轮19；
锥舱大端部壳体13的内壁锥度角大于锥舱小端部壳体21的内壁锥度角，锥舱动力圈3内壁侧母线、锥舱大端部壳体13的外壁侧母线、以及锥舱小端部壳体21的外壁侧母线共线；锥舱动力圈3大端面与锥舱大端部壳体13大端面共面；锥舱调节带14的斜边与锥舱动力圈3内壁贴合并固定连接，相对于锥舱连接圈38轴心线平行的锥舱调节带14的水平直角边内侧壁上设置有与锥舱传动轮17齿轮啮合的锥舱齿纹15，
锥舱橡胶纹2为螺旋状设置；
锥舱大端部壳体13为一个底径10cm、顶径6、高5cm、厚0.1cm的钢制锥柱形壳，锥舱小端部壳体21为一个直径6cm、高3cm、厚0.1cm的钢制锥柱形壳，锥舱连接圈38为一个直径6cm、高1.5cm、厚0.1cm的钢制圈，锥舱大端部壳体13和锥舱小端部壳体21通过锥舱连接圈38刚性连接，形成一个“断崖形”的圆锥体。锥舱动力圈3，为一个直径13cm、高10cm、厚1cm的圆锥形钢制动力圈，锥舱动力圈3将锥舱大端部壳体13和锥舱小端部壳体21罩在里面，锥舱动力圈3的底面和锥舱大端部壳体13的底面在同一个平面上。
在锥舱动力圈3内壁与锥舱连接圈38相对的位置处设置一圈锥舱调节带14，锥舱调节带14的截面呈直角三角形，锥舱调节带14截面的底1cm、高2cm，锥舱调节带14的斜边与锥舱动力圈3内壁相固定，锥舱调节带14截面相对较长的直角边与锥舱连接圈38平行。在锥舱调节带14截面相对较长的直角面上设置锥舱齿纹15。
在锥舱动力圈3的外侧固定安装一层厚3cm的锥舱推进轮1，锥舱动力圈3和锥舱推进轮1是一个整体。在锥舱推进轮1的外侧设置一系列深2cm宽1cm间距2cm的螺旋状锥舱橡胶纹2。在锥舱连接圈38上设置三个长4cm、宽1.5cm的锥舱开口16，相邻两个锥舱开口16之间的夹角为120°。在每一个锥舱开口16的中心位置处都设置一根外径0.5cm的锥舱轴承转轴8，在锥舱轴承转轴8外安装一个直径3.5cm高1cm的钢制的锥舱传动轮17，在锥舱传动轮17外侧设置锥舱齿纹15，锥舱传动轮17上的锥舱齿纹15与锥舱调节带14上的锥舱齿纹15恰好吻合，当锥舱传动轮17转动时可以带动锥舱调节带14转动。通过四根锥舱支架39在锥舱小端部壳体21内固定一个长4cm、宽4cm、高3cm的锥舱电 机20，在锥舱电机20的锥舱传动轴18刚性安装一个直径3cm、高1cm的钢制的锥舱主动轮19，在锥舱主动轮19的外侧设置锥舱齿纹15，锥舱主动轮19上的锥舱齿纹15与锥舱传动轮17上的锥舱齿纹15恰好吻合，当锥舱主动轮19转动时可以带动锥舱传动轮17转动。
柱形推进舱装置包括柱舱主外壳11、同轴套装在柱舱主外壳11外侧且右端面与柱舱主外壳11右端面共面的柱舱动力圈40、固定设置在柱舱动力圈40内侧壁上的钢制的柱舱驱动环5、同轴设置在柱舱驱动环5内侧壁上的柱舱齿纹6、分布在柱舱主外壳11上且与柱舱驱动环5对应的柱舱开口43、设置在柱舱开口43中心位置处的柱舱轴承转轴42、安装在柱舱轴承转轴42上的柱舱传动轮7、设置在柱舱传动轮7外侧壁且与柱舱传动轮7齿纹啮合的柱舱齿纹6、固定套装在柱舱动力圈40的外侧且轴心阵列设置的柱舱推进轮41、设置在相邻的柱舱推进轮41之间的柱舱槽口4、轴向设置在柱舱主外壳11内的柱舱支架44中心处的柱舱电机22、设置在柱舱电机22轴向两端的柱舱传动轴10、设置在柱舱传动轴10上且与柱舱传动轮7齿纹啮合的柱舱主动轮9、密封设置在柱舱主外壳11右端的柱舱后盖23、设置在柱舱后盖23中心处的柱舱传动线26、布设在柱舱传动线26中心位置处的柱舱控制线37、包裹在柱舱传动线26上的柱舱橡胶层30、设置在柱舱后盖23外侧的柱舱固定扣24、以及卡接在柱舱固定扣24上的柱舱第一导线25；
在柱舱推进轮41上设置有锥舱橡胶纹2，柱舱传动线26由若干根柱舱钢丝束31螺旋交叉编织而成，柱舱控制线37通过柱舱第二导线46分别与锥舱电机20和柱舱电机22电连接；
在锥舱大端部壳体13与柱形推进舱装置柱舱主外壳11密封端面之间设置有中间橡胶圈12；
柱舱主外壳11为一个直径10cm、长30cm、厚0.1cm的钢制外壳，柱舱动力圈40为一个直径13cm、高35cm、厚1cm的钢制圆柱形，用柱舱动力圈40将柱舱主外壳11罩在里面，柱舱动力圈40的底面和柱舱主外壳11的底面在同一个平面上。在柱舱动力圈40内壁上设置两圈直径13cm宽3cm厚1cm的钢制柱舱驱动环5，柱舱驱动环5与柱舱动力圈40内壁相固定而互为整体。在柱舱驱动环5内侧设置柱舱齿纹6。在每一个柱舱驱动环5对应柱舱主外壳11上都设置三个长4cm、宽1.5cm的柱舱开口43，相邻两个柱舱开口43之间的夹角为120°。 在每一个柱舱开口43的中心位置处都设置一根外径0.5cm的柱舱轴承转轴42，在柱舱轴承转轴42外安装一个直径3.5cm、高1cm的钢制的柱舱传动轮7，在柱舱传动轮7外侧设置柱舱齿纹6，柱舱传动轮7上的柱舱齿纹6与柱舱驱动环5上的柱舱齿纹6恰好吻合，当柱舱传动轮7转动时可以带动柱舱驱动环5转动。在柱舱动力圈40的外侧固定安装三圈宽10cm、厚3cm的柱舱推进轮41，柱舱动力圈40和柱舱推进轮41是一个整体，相邻两段柱舱推进轮41之间的间距为2cm，并形成一圈宽2cm、深2cm的柱舱槽口4。在柱舱推进轮41的外侧设置一系列深2cm、宽1cm、间距2cm的螺旋状锥舱橡胶纹2。通过四根柱舱支架44在柱舱主外壳11内固定一个长5cm、宽5cm高8cm的柱舱电机22，在柱舱电机22两端的柱舱传动轴10上都刚性安装一个直径7cm、高1cm的钢制的柱舱主动轮9，在每一个柱舱主动轮9的外侧都设置柱舱齿纹6，柱舱主动轮9上的柱舱齿纹6与柱舱传动轮7上的柱舱齿纹6恰好吻合，当柱舱主动轮9转动时可以带动柱舱传动轮7转动。通过直径10cm、厚1cm的钢制的柱舱后盖23将柱形推进舱装置的后端进行密封并固定，在柱舱后盖23外侧的圆心位置处固定安装一根直径5cm的柱舱传动线26，柱舱传动线26由若干根柱舱钢丝束31螺旋交叉编织而成，在柱舱传动线26中心位置处布设一根直径0.3cm的柱舱控制线37，柱舱传动线26的最外层由厚度为0.5cm的柱舱橡胶层30紧密包裹，能达到自由拧动柱舱传动线26而不会改变柱舱传动线26结构和状态的强度。柱舱控制线37通过柱舱第二导线46控制锥舱电机20和柱舱电机22的开关、正反转及供电工作。在柱舱后盖23外侧固定安装一个柱舱固定扣24，柱舱固定扣24可以将柱舱第一导线25卡住并拖动柱舱第一导线25前进，进行布线工作。
将锥形推进舱装置的锥舱大端部壳体13和柱形推进舱装置柱舱主外壳11进行刚性密封连接，使得锥舱小端部壳体21、锥舱大端部壳体13、柱舱主外壳11成为一个整体结构。在锥舱大端部壳体13、柱舱主外壳11的连接处固定安装一圈内径10cm外径13cm厚0.5cm的中间橡胶圈12，中间橡胶圈12固定在柱舱主外壳11上，因为橡胶的自身弹性，中间橡胶圈12能够相对封闭锥舱动力圈3和柱舱动力圈40之间的缝隙，但不影响锥舱动力圈3和柱舱动力圈40相对于锥舱小端部壳体21、锥舱大端部壳体13和柱舱主外壳11自由转动。
送线平台包括固定平台28、以及设置在固定平台28上的输送器27：在固定平台28预设有平台螺栓47，
固定平台28为一个长50cm、宽50cm、高50cm的钢筋混凝土立方体。通过平台螺栓47和螺母48将输送器27固定在固定平台28上。
输送器27包括输送外壳49、设置在输送外壳49前后两侧壁上的输送输线孔36、六个且呈三对分布在输送输线孔36的两个内侧壁上的输送固定架32、设置在输送固定架32上的输送轴承45、安装在同一轴心线上的两个输送轴承45中的输送转轴34、安装在输送转轴34上的橡胶输送输动轮33、以及通过输送电机轴29与对应输送转轴34传动连接的输送电机35。
输送固定架32的两端与输送外壳49的设置有输送输线孔36的两侧壁固定连接，每两个输送固定架32的轴心线夹角为六十度；该三个的输送固定架32上的输送输动轮33围成的三角形的内接圆直径与柱舱传动线26、以及外柱舱橡胶层30的外径相同；输送电机35同步转动；
输送外壳49为长30cm、宽30cm、高30cm且钢制，在输送外壳49的前后壁面上都开设一个直径6cm的输送输线孔36，两个输送输线孔36相对应。在输送外壳49开设有输送输线孔36的两个壁面上安装六个长30cm、宽5cm、厚1.5cm的钢制的输送固定架32，输送固定架32的两端被固定在输送外壳49开设有输送输线孔36的两个壁面上。六个输送固定架32两两一组。在每一个输送固定架32的中间位置都安装一个输送轴承45，在每一组输送固定架32的输送轴承45中都安装一根输送转轴34，输送转轴34可以在输送轴承45内自由转动。相邻两根输送转轴34之间的夹角为60°。在每一根输送转轴34上都固定安装一个直径4cm、高8cm的橡胶输送输动轮33。输送固定架32与输送输动轮33之间的距离为0.5cm。三个橡胶轮33之间的外切圆直径为5.5cm，与柱舱传动线26、外柱舱橡胶层30的外径相同。三个橡胶轮33之间的外切圆的圆心与输送输线孔36的圆心重合。在每一根输送转轴34的末端都安装一个长3cm、宽3cm、高3cm的输送电机35。输送电机35的输送电机轴29与对应的输送转轴34刚性连接。当输送电机35转动时，通过输送电机轴29带动转轴转动，进而带动输送输动轮33转动。三个输送电机35同步转动，因此三个输送输动轮33也是同步转动。
一种矿井暗道柔性推进布线方法，借助于布线机装置，该方法包括以下步骤：
步骤一，首先，将固定平台28放置在设计需要布线工作的布线通道口位置，将输送器27的输送输线孔36正对着设计需要布线工作的布线口；然后，将柱舱传动线26穿过输送输线孔36，将需要布设的柱舱第一导线25固定在柱舱固定 扣24上，将锥形推进舱装置与柱形推进舱装置置于设计需要布线工作的布线通道内；其次，同时启动锥舱电机20、柱舱电机22和输送电机35，其中，锥舱电机20通过锥舱主动轮19、锥舱传动轮17带动锥舱动力圈3旋转，柱舱电机22通过柱舱主动轮9、柱舱传动轮7带动柱舱动力圈40旋转，锥舱动力圈3和柱舱动力圈40外侧的锥舱橡胶纹2被带动并开始转动，输送电机35通过输送电机轴29带动输送输动轮33转动，从而锥形推进舱装置与柱形推进舱装置开始运转。
步骤二，在固定平台28的基座作用和柱舱传动线26传动作用下，锥形推进舱装置与柱形推进舱装置相对于固定平台28向前推进，从而实现推进动作；同时，在锥舱橡胶纹2与布线通道内壁之间摩擦作用下，产生前进动力；同时在输送输动轮33与柱舱传动线26之间摩擦作用下，产生前进动力；最后，在所有前进动力的推进下，布线机装置拉着柱舱第一导线25穿过需要布线工作的布线通道，完成布线工作。
锥舱推进轮1通过锥度推动前行，锥舱橡胶纹2抓土能力强，效率高，耐磨性好，动力输出合理，锥舱动力圈3实现动力输出，锥舱缺口4方便安装，本申请实现在暗道中自行前行，自行配合送线，操作方便，柔性好，对地质环境适应能力强。
本申请不损伤导线，设计合理、成本低廉、结实耐用、安全可靠、操作简单、省时省力、节约资金、结构紧凑且使用方便。
本申请充分描述是为了更加清楚的公开，而对于现有技术就不再一一例举。
最后应说明的是：以上实施例仅用以说明本申请的技术方案，而非对其限制；尽管参照前述实施例对本申请进行了详细的说明，本领域的普通技术人员应当理解：其依然可以对前述实施例所记载的技术方案进行修改，或者对其中部分技术特征进行等同替换；作为本领域技术人员对本申请的多个技术方案进行组合是显而易见的。而这些修改或者替换，并不使相应技术方案的本质脱离本申请实施例技术方案的精神和范围。

Claims (6)

  1. 一种矿井暗道柔性推进布线方法，其特征在于:借助于布线机装置，该装置包括锥形推进舱装置、左端与锥形推进舱装置右端连接的柱形推进舱装置、以及送线平台；
    该方法包括以下步骤：
    步骤一，首先，将固定平台放置在设计需要布线工作的布线通道口位置，将输送器的输送输线孔正对着设计需要布线工作的布线口；然后，将柱舱传动线穿过输送输线孔，将需要布设的柱舱第一导线固定在柱舱固定扣上，将锥形推进舱装置与柱形推进舱装置置于设计需要布线工作的布线通道内；其次，同时启动锥舱电机、柱舱电机和输送电机，其中，锥舱电机通过锥舱主动轮、锥舱传动轮带动锥舱动力圈旋转，柱舱电机通过柱舱主动轮、柱舱传动轮带动柱舱动力圈旋转，锥舱动力圈和柱舱动力圈外侧的锥舱橡胶纹被带动并开始转动，输送电机通过输送电机轴带动输送输动轮转动，从而锥形推进舱装置与柱形推进舱装置开始运转；
    步骤二，在固定平台的基座作用和柱舱传动线传动作用下，锥形推进舱装置与柱形推进舱装置相对于固定平台向前推进，从而实现推进动作；同时，在锥舱橡胶纹与布线通道内壁之间摩擦作用下，产生前进动力；同时在输送输动轮与柱舱传动线之间摩擦作用下，产生前进动力；最后，在所有前进动力的推进下，布线机装置拉着柱舱第一导线穿过需要布线工作的布线通道，完成布线工作；
    其中，柱舱传动线由若干根柱舱钢丝束螺旋交叉编织而成。
  2. 根据权利要求1所述的矿井暗道柔性推进布线方法，其特征在于:锥形推进舱装置包括锥舱大端部壳体、同轴设置在锥舱大端部壳体左侧的锥舱小端部壳体、连接在锥舱大端部壳体左端口与锥舱小端部壳体右端口之间的锥舱连接圈、同轴套装在锥舱大端部壳体与锥舱小端部壳体外侧壁上的锥舱动力圈、设置在锥舱动力圈内侧壁与锥舱连接圈外侧壁之间空腔处且截面为直角三角形的锥舱调节带、同轴固定设置在锥舱动力圈外侧壁上的锥舱推进轮、同轴设置在锥舱推进轮外侧壁上的锥舱橡胶纹、分布在锥舱连接圈上的锥舱开口、设置在锥舱开口处的锥舱轴承转轴、安装在锥舱轴承转轴上的锥舱传动轮、设置在锥舱小端部壳体内腔中的锥舱支架、轴向设置在锥舱支架中心处的锥舱电机、以及设置在锥舱电机的输出轴上且与锥舱传动轮齿纹啮合的锥舱主动轮；
    锥舱大端部壳体的内壁锥度角大于锥舱小端部壳体的内壁锥度角，锥舱动力圈内壁侧母线、锥舱大端部壳体的外壁侧母线、以及锥舱小端部壳体的外壁侧母线共线；锥舱动力圈大端面与锥舱大端部壳体大端面共面；锥舱调节带的斜边与锥舱动力圈内壁贴合并固定连接，相对于锥舱连接圈轴心线平行的锥舱调节带的水平直角边内侧壁上设置有与锥舱传动轮齿轮 啮合的锥舱齿纹；
    锥舱橡胶纹为螺旋状设置。
  3. 根据权利要求2所述的矿井暗道柔性推进布线方法，其特征在于:柱形推进舱装置包括柱舱主外壳、同轴套装在柱舱主外壳外侧且右端面与柱舱主外壳右端面共面的柱舱动力圈、固定设置在柱舱动力圈内侧壁上的钢制的柱舱驱动环、同轴设置在柱舱驱动环内侧壁上的柱舱齿纹、分布在柱舱主外壳上且与柱舱驱动环对应的柱舱开口、设置在柱舱开口中心位置处的柱舱轴承转轴、安装在柱舱轴承转轴上的柱舱传动轮、设置在柱舱传动轮外侧壁且与柱舱传动轮齿纹啮合的柱舱齿纹、固定套装在柱舱动力圈的外侧且轴心阵列设置的柱舱推进轮、设置在相邻的柱舱推进轮之间的柱舱槽口、轴向设置在柱舱主外壳内的柱舱支架中心处的柱舱电机、设置在柱舱电机轴向两端的柱舱传动轴、设置在柱舱传动轴上且与柱舱传动轮齿纹啮合的柱舱主动轮、密封设置在柱舱主外壳右端的柱舱后盖、设置在柱舱后盖中心处的柱舱传动线、布设在柱舱传动线中心位置处的柱舱控制线、包裹在柱舱传动线上的柱舱橡胶层、设置在柱舱后盖外侧的柱舱固定扣、以及卡接在柱舱固定扣上的柱舱第一导线；
    在柱舱推进轮上设置有锥舱橡胶纹，柱舱控制线通过柱舱第二导线分别与锥舱电机和柱舱电机电连接；
    在锥舱大端部壳体与柱形推进舱装置柱舱主外壳密封端面之间设置有中间橡胶圈。
  4. 根据权利要求3所述的矿井暗道柔性推进布线方法，其特征在于:送线平台包括固定平台、以及设置在固定平台上的输送器：在固定平台预设有与输送器连接的平台螺栓。
  5. 根据权利要求4所述的矿井暗道柔性推进布线方法，其特征在于:输送器包括输送外壳、设置在输送外壳前后两侧壁上的输送输线孔、六个且呈三对分布在输送输线孔的两个内侧壁上的输送固定架、设置在输送固定架上的输送轴承、安装在同一轴心线上的两个输送轴承中的输送转轴、安装在输送转轴上的橡胶输送输动轮、以及通过输送电机轴与对应输送转轴传动连接的输送电机。
  6. 根据权利要求5所述的矿井暗道柔性推进布线方法，其特征在于:输送固定架的两端与输送外壳的设置有输送输线孔的两侧壁固定连接，每两个输送固定架的轴心线夹角为六十度；该三个的输送固定架上的输送输动轮围成的三角形的内接圆直径与柱舱传动线、以及外柱舱橡胶层的外径相同；输送电机同步转动。
PCT/CN2020/075621 2019-03-14 2020-02-18 矿井暗道柔性推进布线方法 Ceased WO2020181959A1 (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201910195304.0 2019-03-14
CN201910195304.0A CN109980577B (zh) 2019-03-14 2019-03-14 矿井暗道柔性推进布线方法

Publications (1)

Publication Number Publication Date
WO2020181959A1 true WO2020181959A1 (zh) 2020-09-17

Family

ID=67078972

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2020/075621 Ceased WO2020181959A1 (zh) 2019-03-14 2020-02-18 矿井暗道柔性推进布线方法

Country Status (2)

Country Link
CN (1) CN109980577B (zh)
WO (1) WO2020181959A1 (zh)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109980577B (zh) * 2019-03-14 2020-05-05 青岛理工大学 矿井暗道柔性推进布线方法
CN112938612A (zh) * 2021-01-27 2021-06-11 包仁钦 一种井下省力布线装置

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11341634A (ja) * 1998-05-27 1999-12-10 Sumitomo Electric Ind Ltd モーターローラ
CN206498142U (zh) * 2017-02-21 2017-09-15 山东亿立信息工程技术有限公司 一种通信电缆牵引结构
CN206685809U (zh) * 2017-04-26 2017-11-28 华创电子股份有限公司 智能穿线装置
CN109950835A (zh) * 2019-03-14 2019-06-28 青岛理工大学 矿井暗道柔性推进布线机装置
CN109980577A (zh) * 2019-03-14 2019-07-05 青岛理工大学 矿井暗道柔性推进布线方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105429059B (zh) * 2015-10-30 2017-07-14 国网山东省电力公司东营供电公司 翻滚式电缆穿引装置
CN106972420B (zh) * 2017-05-31 2018-06-08 广州供电局有限公司 电缆敷设设备
CN109193472A (zh) * 2018-09-28 2019-01-11 周玲玲 一种地下电缆电线电线铺设机器人
DE202018107405U1 (de) * 2018-12-21 2019-01-23 Jürgen Stehr Vorrichtung zum Verlegen von Kabeln und/oder Leitungen

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11341634A (ja) * 1998-05-27 1999-12-10 Sumitomo Electric Ind Ltd モーターローラ
CN206498142U (zh) * 2017-02-21 2017-09-15 山东亿立信息工程技术有限公司 一种通信电缆牵引结构
CN206685809U (zh) * 2017-04-26 2017-11-28 华创电子股份有限公司 智能穿线装置
CN109950835A (zh) * 2019-03-14 2019-06-28 青岛理工大学 矿井暗道柔性推进布线机装置
CN109980577A (zh) * 2019-03-14 2019-07-05 青岛理工大学 矿井暗道柔性推进布线方法

Also Published As

Publication number Publication date
CN109980577B (zh) 2020-05-05
CN109980577A (zh) 2019-07-05

Similar Documents

Publication Publication Date Title
US2630906A (en) Silage distributor
WO2020181959A1 (zh) 矿井暗道柔性推进布线方法
EP0681669B1 (en) Pipe tractor
CN102132682B (zh) 增氧机
CN206142395U (zh) 一种滚筒输送装置
CN109950835A (zh) 矿井暗道柔性推进布线机装置
US3508619A (en) Hose guide for rock drills
CN101958520B (zh) 野外电缆布线机
CN209472299U (zh) 矿井暗道柔性推进布线机装置
AU615593B2 (en) A hose and cable reel arrangement for a rock drilling equipment
US2897779A (en) Pipe lining apparatus
CN110948011B (zh) 一种用于圆管件排孔的自动钻孔装置
CN210914271U (zh) 一种建筑用钢筋传输装置
CN216720786U (zh) 一种电缆布线用绕卷装置
CN214429109U (zh) 一种电线电缆牵引装置
CN215527337U (zh) 一种节能式电缆制造设备
CN109921337B (zh) 矿井暗道或地下管廊布线器装置、布线装置
CN209756016U (zh) 一种节约制作成本的管材牵引机
CN211522685U (zh) 一种港口施工轨道铺设装置
JPS5830862B2 (ja) 長尺物送出装置
CN200945666Y (zh) 一种组合钻机
US2802653A (en) Tunneling machine having rotating cutting bars
JPH084011A (ja) 多軸掘削機
CN103660820B (zh) 履带式多功能水下无人驾驶多用直升飞行机
US3071199A (en) Portable earth boring machine

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 20770278

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 20770278

Country of ref document: EP

Kind code of ref document: A1

32PN Ep: public notification in the ep bulletin as address of the adressee cannot be established

Free format text: NOTING OF LOSS OF RIGHTS PURSUANT TO RULE 112(1) EPC (EPO FORM 1205A DATED 14/02/2022)

122 Ep: pct application non-entry in european phase

Ref document number: 20770278

Country of ref document: EP

Kind code of ref document: A1