CN201670522U - Intelligent misaligned belt adjusting conveyer - Google Patents
Intelligent misaligned belt adjusting conveyer Download PDFInfo
- Publication number
- CN201670522U CN201670522U CN2010201709756U CN201020170975U CN201670522U CN 201670522 U CN201670522 U CN 201670522U CN 2010201709756 U CN2010201709756 U CN 2010201709756U CN 201020170975 U CN201020170975 U CN 201020170975U CN 201670522 U CN201670522 U CN 201670522U
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- frame
- tail
- axle bed
- head
- belt
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- Expired - Fee Related
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Abstract
The utility model relates to an intelligent misaligned belt adjusting conveyer, which comprises an elongated frame rack, a head cylinder and a tail cylinder are drum-shaped cylinder. Two sides of the conveyer belts at the head and the tail are respectively provided with displacement sensors, and electro-hydraulic push rods are respectively connected between an axle seat at the head and a frame and between an axle seat at the tail and the frame. The two sides of the upper part of the conveyor belt of a misalignment adjusting roller are provided with a left roller displacement sensor and a right roller displacement sensor. The left roller electro-hydraulic push rod and the right roller electro-hydraulic push rod are connected between the trough edges of the two sides of a misalignment adjusting roller trapezoid trough support and the frame. A buffering hydraulic cylinder is provided with a pressure sensor, a scraper conveyor is arranged under the conveyor belt under the tail of the belt conveyor, and the frame at the conveyor tail is provided with a scraper of the tail cylinder. The intelligent misaligned belt adjusting conveyer can clean granular material scattered under the conveyor tail in time. The two sides of the conveyer belt of the intelligent misalignment belt conveyer are provided with displacement sensors connected with the corresponding electro-hydraulic push rods. When the conveyor belt is misaligned, the misaligned conveyor belt can trigger the corresponding displacement sensors, and the corresponding displacement sensors drive the corresponding electro-hydraulic push rods to adjust the misaligned conveyor belt in time, which saves time and labor.
Description
Technical field
The utility model relates to the deviation correcting device of a kind of belt conveyer, particularly a kind of belt conveyer.
Background technology
Belt conveyer is used to carry powder class material.Under coal mine, be with belt conveyer raw coal to be transported to main shaft from the exploitation driving surface to transport.Distance between exploitation driving surface and the main shaft is bigger, carries the belt conveyer of raw coal quite long.Belt conveyer has rectangular shaped as frame frame, be evenly equipped with carrying roller along its length on the rectangular shaped as frame frame, one end of frame has head, the other end has tail, left side on the head place frame, the right side has a left side respectively, right head axle bed slideway, left side on the tail place frame, the right side has a left side respectively, right tail axle bed slideway, a left side, on the right head axle bed slideway left side is arranged respectively, right head axle bed, a left side, between the right head axle bed axis head drum vertical with the length direction of frame arranged, a left side, on the right tail axle bed slideway left side is arranged respectively, right tail axle bed, a left side, the aircraft tail cylinder that the parallel axes of axis and head drum is arranged between the right tail axle bed, be connected with rubber conveyer belt between head drum and the aircraft tail cylinder, the actuating device of rubber conveyer belt and the tightening device of rubber conveyer belt are arranged on the frame, the rubber conveyer belt tightening device has tensioning winch and buffering hydraulic actuating cylinder, a left side, be connected with the tuningout screw rod respectively between right head axle bed and the frame, a left side, be connected with the tuningout screw rod respectively between right tail axle bed and the frame, on the frame in the uniform along its length carrying roller, the compartment of terrain is distributed with deviation regulating idler, deviation regulating idler has troffer, in the middle of the bottom land below of troffer pivot shaft is arranged, there is the support axis hole centre of the frame of troffer below, pivot shaft is inserted in and supports in the axis hole, and carrying roller is arranged on the troffer.
For the quite long raw coal belt conveyer of the length under the coal mine, easier generation rubber conveyer belt sideslip and lax phenomenon in operational process.
Above-mentioned belt conveyer of the prior art has following deficiency:
1. head drum and aircraft tail cylinder all are rotatingcylindrical drums, and in the use, cylinder can not be regulated the rubber conveyer belt sideslip voluntarily when the rubber conveyer belt sideslip;
2. in the use, the length direction of the axis of head drum and the axis runout of aircraft tail cylinder and frame is vertical when the whole sideslip of rubber conveyer belt takes place, be to remove to regulate the axle bed of head drum and the axle bed of aircraft tail cylinder with the method for manual regulation tuningout screw rod, allow the axis of head drum and the axis of aircraft tail cylinder recover vertical with the length direction of frame, adjust the whole sideslip of rubber conveyer belt with manual methods, take a lot of work, effort, tuningout be untimely, can not guarantee the normal operation of belt conveyer;
3. in the use, place inhomogeneous when rubber conveyer belt stage casing sideslip takes place in the rubber conveyer belt stage casing because of powder class material, be to adjust rubber conveyer belt stage casing sideslip with the hand rotation deviation regulating idler, equally also be take a lot of work, effort, tuningout be untimely, can not guarantee the normal operation of belt conveyer;
4. when rubber conveyer belt is lax, can strain rubber conveyer belt with tensioning winch, buffering hydraulic cylinder can play buffer action during tensioning winch tension rubber conveyer belt, the tensioning winch pulling force is big, can solve and have big lax rubber conveyer belt, produce lessly when lax at rubber conveyer belt, be difficult to solve with tensioning winch;
5. belt conveyer in use; when powder class material is loaded on the tail of belt conveyer; powder class material regular meeting falls on the ground of tail below; waste material, influence environment; need in time to remove; otherwise influence the running of rubber conveyer belt machine,, remove very difficult because the tail below is short, narrow.
Summary of the invention
The purpose of this utility model is in order to overcome above-mentioned deficiency, to propose a kind of saving of labor, laborsaving, the intelligent timely tuningout belt conveyer of tuningout.
The utility model is realized with the following method.
Intelligence tuningout belt conveyer has rectangular shaped as frame frame, be evenly equipped with carrying roller along its length on the rectangular shaped as frame frame, one end of frame has head, the other end has tail, left side on the head place frame, the right side has a left side respectively, right head axle bed slideway, left side on the tail place frame, the right side has a left side respectively, right tail axle bed slideway, a left side, on the right head axle bed slideway left side is arranged respectively, right head axle bed, a left side, between the right head axle bed axis head drum vertical with the length direction of frame arranged, a left side, on the right tail axle bed slideway left side is arranged respectively, right tail axle bed, a left side, the aircraft tail cylinder that the parallel axes of axis and head drum is arranged between the right tail axle bed, be connected with rubber conveyer belt between head drum and the aircraft tail cylinder, the actuating device of rubber conveyer belt and the tightening device of rubber conveyer belt are arranged on the frame, the tightening device of rubber conveyer belt has tensioning winch and buffering hydraulic actuating cylinder, a left side, be connected with deviation correcting device respectively between right head axle bed and the frame, a left side, be connected with deviation correcting device respectively between right tail axle bed and the frame, on the frame in the uniform along its length carrying roller, the compartment of terrain is distributed with deviation regulating idler, deviation regulating idler has troffer, there is pivot shaft the below of troffer, the support axis hole is arranged on the frame of the below of troffer, pivot shaft is inserted in and supports in the axis hole, carrying roller is arranged on the troffer, head drum and aircraft tail cylinder are drum, both sides above the rubber conveyer belt at head place have a left side respectively, right head displacement pickup, both sides below the rubber conveyer belt at tail place have a left side respectively, right tail displacement pickup, a left side, deviation correcting device between right head axle bed and the frame is an Electrohydraulic push rod, a left side, deviation correcting device between right tail axle bed and the frame is an Electrohydraulic push rod, both sides above the rubber conveyer belt at deviation regulating idler place have a left side respectively, right carrying roller displacement pickup, one side of troffer bottom land below has pivot shaft, one side of the following methods, rack of troffer has the support axis hole, pivot shaft is inserted in and supports in the axis hole, the opposite side of troffer bottom land below has slide block, the opposite side of the following methods, rack of troffer has the cambered way that matches with above-mentioned slide block, slide block is in cambered way, be connected with the carrying roller Electrohydraulic push rod between slide block and the frame, between the both sides of the below of troffer and the frame spring is arranged, 1～6 group of carrying roller carrying roller is arranged on the troffer, pressure sensor is arranged on buffering hydraulic cylinder, below the belt conveyer tail, below the load-transfer device slat conveyer is arranged, the scraper plate of aircraft tail cylinder is arranged on the frame at tail place.
During installation, corresponding displacement sensor is linked to each other with Electrohydraulic push rod by control setup, the pressure sensor on the buffering hydraulic cylinder is linked to each other with the Hydraulic Station of buffering hydraulic cylinder by control setup.
During use, with the actuating device points driving for belt conveyor operation of rubber conveyer belt.Because head drum and aircraft tail cylinder are drum, when a spot of sideslip took place rubber conveyer belt, drum can be regulated rubber conveyer belt voluntarily and be recovered normal in certain scope; When belt conveyer because of the reason of head and aircraft tail cylinder axle bigger sideslip took place, the rubber conveyer belt of sideslip can trigger corresponding displacement pickup, drives corresponding Electrohydraulic push rod by corresponding control setup the rubber conveyer belt of sideslip is adjusted; When belt deflection takes place because the powder class material on the rubber conveyer belt stage casing places inhomogeneous in belt conveyer, the load-transfer device of sideslip can trigger corresponding carrying roller displacement pickup, drives the carrying roller Electrohydraulic push rod by corresponding control setup the rubber conveyer belt stage casing of sideslip is adjusted; When the rubber conveyer belt of belt conveyer produces less when lax, pressure on the buffering hydraulic cylinder can reduce, because the sensor that links to each other with Hydraulic Station with control setup is arranged on the buffering hydraulic cylinder, buffering hydraulic cylinder can be less lax the returning to normally of rubber conveyer belt.
Head drum of the present utility model and aircraft tail cylinder are drum, the respective point of rubber conveyer belt both sides has displacement pickup, displacement pickup links to each other with corresponding Electrohydraulic push rod, when belt deflection, the load-transfer device of sideslip can trigger corresponding displacement pickup, and then drive corresponding Electrohydraulic push rod and can adjust the load-transfer device of sideslip, not only timely, also saving of labor, laborsaving; The sensor that links to each other with Hydraulic Station with control setup is arranged on the buffering hydraulic cylinder of tightening device, can be less lax the returning to normally of rubber conveyer belt; There is slat conveyer the following load-transfer device below of tail, can clean out the powder class material that is scattered below of tail in time.
Below in conjunction with accompanying drawing, the utility model is further described.
Description of drawings
Fig. 1 is that the master of a kind of intelligent tuningout belt conveyer that proposes according to invention scheme of the present utility model looks scheme drawing;
Fig. 2 is that the master of head drum and aircraft tail cylinder looks scheme drawing;
Fig. 3 is the I place enlarged diagram of Fig. 1;
Fig. 4 is the II place enlarged diagram of Fig. 1;
Fig. 5 is the III place enlarged diagram of Fig. 1;
Fig. 6 is the IV place enlarged diagram of Fig. 1;
Fig. 7 is that the A of Fig. 5 is to scheme drawing;
Fig. 8 is the schematic side view of Fig. 7.
The specific embodiment
Among Fig. 1～Fig. 8, intelligence tuningout belt conveyer has rectangular shaped as frame frame 1, be evenly equipped with carrying roller 2 along its length on the rectangular shaped as frame frame, one end of frame has head 3, the other end has tail 4, left side on the head place frame, the right side has a left side respectively, right head axle bed slideway 5, left side on the tail place frame, the right side has a left side respectively, right tail axle bed slideway 6, a left side, on the right head axle bed slideway left side is arranged respectively, right head axle bed 7, a left side, between the right head axle bed axis head drum vertical with the length direction of frame 8 arranged, a left side, on the right tail axle bed slideway left side is arranged respectively, right tail axle bed 9, a left side, the aircraft tail cylinder 10 that the parallel axes of axis and head drum is arranged between the right tail axle bed, be connected with rubber conveyer belt 11 between head drum and the aircraft tail cylinder, the actuating device 12 of rubber conveyer belt and the tightening device of rubber conveyer belt are arranged on the frame, the tightening device of rubber conveyer belt has tensioning winch 13 and buffering hydraulic actuating cylinder 14, a left side, be connected with deviation correcting device respectively between right head axle bed and the frame, a left side, be connected with deviation correcting device respectively between right tail axle bed and the frame, on the frame in the uniform along its length carrying roller, the compartment of terrain is distributed with deviation regulating idler 15, deviation regulating idler has troffer 16, there is pivot shaft the below of troffer, the support axis hole is arranged on the frame of the below of troffer, pivot shaft is inserted in and supports in the axis hole, carrying roller 17 is arranged on the troffer, head drum and aircraft tail cylinder are drum 18, both sides above the rubber conveyer belt at head place have a left side respectively, right head displacement pickup 19, both sides below the rubber conveyer belt at tail place have a left side respectively, right tail displacement pickup 20, a left side, deviation correcting device between right head axle bed and the frame is an Electrohydraulic push rod 21, a left side, deviation correcting device between right tail axle bed and the frame is an Electrohydraulic push rod 22, both sides above the rubber conveyer belt at deviation regulating idler place have a left side respectively, right carrying roller displacement pickup 23, one side of troffer bottom land below has pivot shaft 24, one side of the following methods, rack of troffer has the axis hole 25 of support, pivot shaft is inserted in and supports in the axis hole, the opposite side of troffer bottom land below has slide block 26, the opposite side of the following methods, rack of troffer has the cambered way 27 that matches with above-mentioned slide block, slide block is in cambered way, be connected with carrying roller Electrohydraulic push rod 28 between slide block and the frame, be connected with spring 29 between the both sides of troffer below and the frame, 1～6 group of carrying roller carrying roller is arranged on the troffer, pressure sensor 30 is arranged on buffering hydraulic cylinder, slat conveyer 31 is arranged below the load-transfer device below the belt conveyer tail, the scraper plate 32 of aircraft tail cylinder is arranged on the frame at tail place.
Claims (1)
1. intelligent tuningout belt conveyer, rectangular shaped as frame frame is arranged, be evenly equipped with carrying roller along its length on the rectangular shaped as frame frame, one end of frame has head, the other end has tail, left side on the head place frame, the right side has a left side respectively, right head axle bed slideway, left side on the tail place frame, the right side has a left side respectively, right tail axle bed slideway, a left side, on the right head axle bed slideway left side is arranged respectively, right head axle bed, a left side, between the right head axle bed axis head drum vertical with the length direction of frame arranged, a left side, on the right tail axle bed slideway left side is arranged respectively, right tail axle bed, a left side, the aircraft tail cylinder that the parallel axes of axis and head drum is arranged between the right tail axle bed, be connected with rubber conveyer belt between head drum and the aircraft tail cylinder, the actuating device of rubber conveyer belt and the tightening device of rubber conveyer belt are arranged on the frame, the tightening device of rubber conveyer belt has tensioning winch and buffering hydraulic actuating cylinder, a left side, be connected with deviation correcting device respectively between right head axle bed and the frame, a left side, be connected with deviation correcting device respectively between right tail axle bed and the frame, on the frame in the uniform along its length carrying roller, the compartment of terrain is distributed with deviation regulating idler, deviation regulating idler has troffer, there is pivot shaft the below of troffer, the support axis hole is arranged on the frame of the below of troffer, pivot shaft is inserted in and supports in the axis hole, carrying roller is arranged on the troffer, it is characterized in that: head drum and aircraft tail cylinder are drum, both sides above the rubber conveyer belt at head place have a left side respectively, right head displacement pickup, both sides below the rubber conveyer belt at tail place have a left side respectively, right tail displacement pickup, a left side, deviation correcting device between right head axle bed and the frame is an Electrohydraulic push rod, a left side, deviation correcting device between right tail axle bed and the frame is an Electrohydraulic push rod, both sides above the rubber conveyer belt at deviation regulating idler place have a left side respectively, right carrying roller displacement pickup, one side of troffer bottom land below has pivot shaft, one side of the following methods, rack of troffer has the support axis hole, pivot shaft is inserted in and supports in the axis hole, the opposite side of troffer bottom land below has slide block, the opposite side of the following methods, rack of troffer has the cambered way that matches with above-mentioned slide block, slide block is in cambered way, be connected with the carrying roller Electrohydraulic push rod between slide block and the frame, between the both sides of the below of troffer and the frame spring is arranged, 1～6 group of carrying roller carrying roller is arranged on the troffer, pressure sensor is arranged on buffering hydraulic cylinder, below the belt conveyer tail, below the load-transfer device slat conveyer is arranged, the scraper plate of aircraft tail cylinder is arranged on the frame at tail place.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201709756U CN201670522U (en) | 2010-04-27 | 2010-04-27 | Intelligent misaligned belt adjusting conveyer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201709756U CN201670522U (en) | 2010-04-27 | 2010-04-27 | Intelligent misaligned belt adjusting conveyer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201670522U true CN201670522U (en) | 2010-12-15 |
Family
ID=43327934
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010201709756U Expired - Fee Related CN201670522U (en) | 2010-04-27 | 2010-04-27 | Intelligent misaligned belt adjusting conveyer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201670522U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102424242A (en) * | 2011-08-11 | 2012-04-25 | 中联重科股份有限公司 | Belt conveyor and asphalt stirring equipment with same |
| CN106697762A (en) * | 2017-01-08 | 2017-05-24 | 车新宁 | Scraping-plate conveying belt type elevator for delivering residue soil out in subway tunnel construction |
| CN112027496A (en) * | 2020-09-01 | 2020-12-04 | 安徽星辉工业科技有限公司 | Novel pinch roller device of belt conveyor |
-
2010
- 2010-04-27 CN CN2010201709756U patent/CN201670522U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102424242A (en) * | 2011-08-11 | 2012-04-25 | 中联重科股份有限公司 | Belt conveyor and asphalt stirring equipment with same |
| CN106697762A (en) * | 2017-01-08 | 2017-05-24 | 车新宁 | Scraping-plate conveying belt type elevator for delivering residue soil out in subway tunnel construction |
| CN112027496A (en) * | 2020-09-01 | 2020-12-04 | 安徽星辉工业科技有限公司 | Novel pinch roller device of belt conveyor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20101215 Termination date: 20140427 |