CN205221770U - Belting is pressed to zone face about pipe support fuselage - Google Patents

Belting is pressed to zone face about pipe support fuselage Download PDF

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Publication number
CN205221770U
CN205221770U CN201520847385.5U CN201520847385U CN205221770U CN 205221770 U CN205221770 U CN 205221770U CN 201520847385 U CN201520847385 U CN 201520847385U CN 205221770 U CN205221770 U CN 205221770U
Authority
CN
China
Prior art keywords
roll
zone face
belting
area
conveyer belt
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.)
Expired - Fee Related
Application number
CN201520847385.5U
Other languages
Chinese (zh)
Inventor
杨淑荣
武骏
杨春林
李晓东
杨彬
杨泽彬
曹亚丽
李旭东
张跃华
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.)
SHANXI HAOYE GENERAL EQUIPMENT CO Ltd
Original Assignee
SHANXI HAOYE GENERAL EQUIPMENT CO Ltd
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 SHANXI HAOYE GENERAL EQUIPMENT CO Ltd filed Critical SHANXI HAOYE GENERAL EQUIPMENT CO Ltd
Priority to CN201520847385.5U priority Critical patent/CN205221770U/en
Application granted granted Critical
Publication of CN205221770U publication Critical patent/CN205221770U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model relates to a press the belting, concretely relates to belting is pressed to zone face about pipe support fuselage. The utility model provides a can only compress tightly the zone face in order to solve original pressure belting, result in probably influence the problem that the conveyer belt used because of the lower zone face winding of conveyer belt, and then provide a belting is pressed to zone face about pipe support fuselage, the lambda type console mode support body that sets up including the bilateral symmetry, between the two console mode support bodys through the axle unit mount have a plurality of go up to press to take roll, still install the area that pushes down of a plurality of parallels between the two console mode support bodys and roll, push down the area and roll to locate and press the area and roll the below, and push down to take and roll that to roll the antarafacial perpendicular with last pressure area. The utility model discloses the device rolls through last pressure area to press the edge of last conveyer belt to the last roll surface of notch carrier roller group, push down the area roll the restriction down the movable track of conveyer belt come the cooperation to compress tightly the restriction conveyer belt, the zone face friction harms the sticky tape about effectively preventing, prevent that the ribbon from causing spill the material, the incident appears.

Description

Lower belt surface belt pressing device on pipe support fuselage
Technical field
The utility model relates to a kind of belt pressing device, is specifically related to lower belt surface belt pressing device on a kind of pipe support fuselage.
Background technology
In order to prevent, load-transfer device emerged in operation from wearing and tearing, ribbon causes the spreading even problem of safety misadventure, needs to compress load-transfer device.But can only limit the upper zone face of load-transfer device for the belt pressing device as described in 201310605553.5, and load-transfer device is annular back and forth operational mode, when loosening appears in its lower belt surface, still there will be zone face be wound around or depart from the problems such as conveying track, spreading can be caused, ribbon affects conveying products quality, even cause safety misadventure.
Summary of the invention
This practicality newly can only compress upper zone face to solve original belt pressing device, causes to be wound around because of the lower belt surface of load-transfer device the problem affecting load-transfer device and use, and then provides lower belt surface belt pressing device on a kind of pipe support fuselage.
The utility model adopts following technical scheme:
Lower belt surface belt pressing device on a kind of pipe support fuselage, comprise the Λ type floor type support body that bilateral symmetry is arranged, by Shaft assembly, some upper pressure zones are installed between two floor type support bodys to roll, some parallel lower pressure zones are also installed between described two floor type support bodys roll, lower pressure zone rolls is located at the pressure zone side of rolling down, and lower pressure zone rolls, and to roll antarafacial with upper pressure zone vertical.
Described lower pressure zone rolls two ends and is provided with vertical carriage.
Described carriage is the channel-section steel having bar hole, and the two ends that lower pressure zone rolls are placed in the bar hole of channel-section steel.
The diameter that described upper pressure zone rolls is φ 700-φ 900mm.
The utility model device rolls by upper pressure zone the upper roll surface edge of upper conveyor belt being depressed into groove profile carrier roller group, the event trace that lower pressure zone rolls the lower load-transfer device of restriction coordinates compression limit transport band, effectively can prevent lower belt surface frictionally damage adhesive tape, the spreading preventing ribbon from causing, occur safety misadventure; The height simultaneously utilizing carriage effectively to descend pressure zone to roll, can be applicable to the load-transfer device compressing different radius of turn.
Accompanying drawing explanation
Fig. 1 is structural front view of the present utility model;
Fig. 2 is structure side view of the present utility model;
In figure: 1-floor type support body, the upper pressure zone of 2-roll, under 3-idler machining, 4-pressure zone roll, load-transfer device, 7-carriage under 5-upper conveyor belt, 6-.
Detailed description of the invention
Lower belt surface belt pressing device on pipe support fuselage as shown in Figure 1, 2, comprise the Λ type floor type support body 1 that bilateral symmetry is arranged, by Shaft assembly, some upper pressure zones are installed between two floor type support bodys 1 and roll 2, some parallel lower pressure zones are also installed between described two floor type support bodys 1 and roll 4, lower pressure zone rolls 4 and is located at pressure zone and rolls below 2, and lower pressure zone rolls 4, and to roll 2 antarafacials vertical with upper pressure zone.
It is adopt the belt pressing device upper pressure wheel device on modular conveyor that upper pressure zone rolls 2, unique difference is exactly that the diameter of traditional pinch roller is somewhat little according to the long-time empirical discovery diameter used, when the coal cinder that granularity in the coal carried is larger, will be stuck on belt wheel, result in blockage.To on same colliery, the ascending pinch roller doing different-diameter has several times done design plans different several times from minimum φ 500-φ 700-φ 900, learn that between φ 700-φ 900, result of use is the best in the feedback according to client, reality used afterwards, and because wheel structure itself is comparatively simple, even if it is almost constant to become larger wheels diameter cost, but solves the too little problem of traditional pinch roller diameter.
Λ type floor type support body 1 is made up of zinc-plated channel-section steel, zinc-plated pipe, steel plate, bolt of rear end plate, adjusting bolt etc., compare with traditional pinch roller support body, the utility model has several feature: the first, floor type, this measure solves because during No Load Start, load-transfer device moment tension force becomes the problem causing greatly ribbon even to drive pinch roller support body floating, because when mounted, need ground, tunnel to utilize ground bolt or anchor pole to fix this device.Just because of be floor type, with the support body of conveyer fuselage without any associating, can when designing and producing, the intensity of suitable increase pinch roller, without the need to worrying the weight of pinch roller; The second, Height Adjustable, connect the place of support body in belt wheel bearing, specially on support body, make elongated hole, so just can pass through top bolt below bearing seat according to the center height of on-site actual situations adjustment pinch roller; Three, this device compares all right right and left mutually changing with traditional belt pressing device, especially on acclive tunnel, installs this device, can reach large-scale lift action by right and left mutually changing pinch roller, low to the requirement of field ground ground.A pressure roller device only configures pinch roller, and the other end steel pipe manufacturing do not used a horizontal drawing device, can make this device more stable.
Described lower pressure zone rolls 4 two ends and is provided with vertical carriage 7, adjust lower pressure zone by carriage 7 and roll the height and position of 4 to carry zone face under compressing, lower pressure zone rolls 4 and moves up and down the object that can reach adjustment height along channel-section steel bar hole, thus without the need to the position of support body.
This device rolls by upper pressure zone the upper roll surface that the edge of upper conveyor belt 5 to be depressed into groove profile carrier roller group 3 by 2, rolled the event trace of load-transfer device 6 under 4 restrictions simultaneously by lower pressure zone, prevent lower belt surface frictionally damage adhesive tape, the spreading preventing ribbon from causing, occur safety misadventure.

Claims (4)

1. lower belt surface belt pressing device on a pipe support fuselage, comprise Λ type floor type support body (1) that bilateral symmetry is arranged, by Shaft assembly, some upper pressure zones are installed between two floor type support bodys (1) to roll (2), it is characterized in that: between described two floor type support bodys (1), some parallel lower pressure zones are also installed and roll (4), lower pressure zone rolls (4) and is located at pressure zone and rolls (2) below, and lower pressure zone rolls (4), and roll (2) antarafacial with upper pressure zone vertical.
2. lower belt surface belt pressing device on pipe support fuselage according to claim 1, is characterized in that: described lower pressure zone rolls (4) two ends and is provided with vertical carriage (7).
3. lower belt surface belt pressing device on pipe support fuselage according to claim 2, is characterized in that: described carriage (7) is for having the channel-section steel of bar hole, and the two ends that lower pressure zone rolls (4) are placed in the bar hole of channel-section steel.
4. lower belt surface belt pressing device on pipe support fuselage according to claim 1, is characterized in that: the diameter that described upper pressure zone rolls (2) is φ 700-φ 900mm.
CN201520847385.5U 2015-10-29 2015-10-29 Belting is pressed to zone face about pipe support fuselage Expired - Fee Related CN205221770U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520847385.5U CN205221770U (en) 2015-10-29 2015-10-29 Belting is pressed to zone face about pipe support fuselage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520847385.5U CN205221770U (en) 2015-10-29 2015-10-29 Belting is pressed to zone face about pipe support fuselage

Publications (1)

Publication Number Publication Date
CN205221770U true CN205221770U (en) 2016-05-11

Family

ID=55896847

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520847385.5U Expired - Fee Related CN205221770U (en) 2015-10-29 2015-10-29 Belting is pressed to zone face about pipe support fuselage

Country Status (1)

Country Link
CN (1) CN205221770U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110088015A (en) * 2016-10-24 2019-08-02 Lhb 采矿解决方案有限公司 Conveyer system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110088015A (en) * 2016-10-24 2019-08-02 Lhb 采矿解决方案有限公司 Conveyer system

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160511

Termination date: 20191029