CN214076986U

CN214076986U - Hammer mill with hoop structure

Info

Publication number: CN214076986U
Application number: CN202022901604.7U
Authority: CN
Inventors: 吴家和; 吴家俊
Original assignee: Shanghai Minwang Machinery Technology Co ltd
Current assignee: Shanghai Minwang Machinery Technology Co ltd
Priority date: 2020-12-03
Filing date: 2020-12-03
Publication date: 2021-08-31
Anticipated expiration: 2030-12-03

Abstract

The utility model discloses a hammer mill with clamp structure, including main part and clamp dismouting structure, the main part lower extreme is provided with the spacing subassembly of slip, and slides the spacing subassembly lower extreme and be provided with the universal wheel, clamp dismouting structure sets up in main part one side, and clamp dismouting structure includes fuselage, first clamp ring, second clamp ring, block groove, connecting bolt and aircraft nose, the block groove has been seted up in the fuselage outside, and the block groove outside is provided with first clamp ring. This hammer mill with clamp structure, fuselage and aircraft nose pass through block groove and first clamp ring and second clamp ring block, run through connecting bolt inside first clamp ring and second clamp ring again, can realize the installation of fuselage and aircraft nose fixed, and through this structure, can realize the separation of fuselage and aircraft nose, the off-line sterilization of being convenient for can carry out simple and convenient washing and maintenance to the fuselage, reduces the cost of operation, and the practicality is higher.

Description

Hammer mill with hoop structure

Technical Field

The utility model relates to a hammer mill technical field specifically is a hammer mill with clamp structure.

Background

The hammer crusher mainly crushes materials by means of impact, the materials enter the hammer crusher and are crushed by the impact of the hammer head rotating at a high speed, the crushed materials obtain kinetic energy from the hammer head of the hammer crusher and impact towards the inner baffle plate of the frame body from the high speed, the screen bars and the materials impact with each other at the same time and are crushed for multiple times, the materials smaller than the gap of the screen bars are discharged from the gap, and the individual larger materials are crushed by the hammer head on the screen bars again, ground, extruded and crushed, and the materials are extruded from the gap by the hammer head of the hammer crusher, so that the products with required granularity are obtained.

Hammer mill on market, the separation is dismantled to aircraft nose and the fuselage inconvenience, is not convenient for carry out sterilization process to the rubbing crusher, inconvenient inside washing and the maintenance that carries on portably of rubbing crusher, and the cost of operation is higher, and hammer mill collects full back at the material, needs carry the material, the problem of comparatively wasting time and energy, for this reason, we propose a hammer mill with clamp structure.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a hammer mill with clamp structure to solve the hammer mill on the market that proposes in the above-mentioned background art, the separation is dismantled with the fuselage inconvenience to the aircraft nose, is not convenient for carry out sterilization treatment to the rubbing crusher, inconvenient carrying out simple and convenient washing and maintenance to rubbing crusher inside, the cost of operation is higher, and hammer mill is collected full back at the material, need carry the material, comparatively problem that wastes time and energy.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a hammer mill with clamp structure, includes main part and clamp dismouting structure, the main part lower extreme is provided with the spacing subassembly of slip, and slides spacing subassembly lower extreme and be provided with the universal wheel, clamp dismouting structure sets up in main part one side, and clamp dismouting structure includes fuselage, first clamp ring, second clamp ring, block groove, connecting bolt and aircraft nose, the block groove has been seted up in the fuselage outside, and the block groove outside is provided with first clamp ring, first clamp ring one side is provided with the second clamp ring, and the inside running through of second clamp ring is provided with connecting bolt, second clamp ring upper end is provided with the aircraft nose.

Preferably, the sliding limiting assembly comprises a bottom plate, a guide plate, a sliding groove, a sliding plate and a storage box, the guide plate is welded and fixed on one side of the bottom plate, the sliding groove is formed in the guide plate, the sliding plate is arranged on the inner side of the guide plate, and the storage box is fixedly bonded on the upper end of the sliding plate.

Preferably, the sliding plate and the bottom plate form a sliding structure through the sliding groove, and one side of the bottom plate is tightly attached to one side of the guide plate.

Preferably, the machine body and the first clamp ring form a clamping structure through the clamping groove, and the inner side of the first clamp ring is tightly attached to the outer sides of the machine body and the machine head.

Preferably, the connecting bolt penetrates through the inside of the first clamp ring and the second clamp ring, and the first clamp ring and the second clamp ring form a dismounting structure through the connecting bolt.

Preferably, the lower end of the machine head is tightly attached to the upper end of the machine body, and the transverse center line of the machine body is completely overlapped with the transverse center line of the machine head.

Compared with the prior art, the beneficial effects of the utility model are as follows:

1. the storage box is used for connecing the material after being processed greatly, when storage box splendid attire material, the slide of storage box lower extreme passes through sliding tray and bottom plate block, can avoid the storage box to rock phenomenons such as empting appear, and when the storage box was filled with the material, can slide the slide of storage box lower extreme left along the inboard sliding tray of bottom plate, support through the deflector, can avoid the storage box directly to drop the phenomenon appearance that powder material looses in the ground derivation storage box, can be with the storage box by promoting on the bottom plate and take off, very labour saving and time saving, and through this structure, can improve this hammer crusher's reliability in utilization.

2. Fuselage and aircraft nose pass through block groove and first clamp ring and second clamp ring block, run through connecting bolt inside first clamp ring and second clamp ring again, can realize the installation of fuselage and aircraft nose fixed, and through this structure, can realize the separation of fuselage and aircraft nose, the off-line sterilization of being convenient for can carry out simple and convenient washing and maintenance to the fuselage, reduces the cost of operation, and the practicality is higher.

Drawings

FIG. 1 is a schematic side view of the present invention;

FIG. 2 is a schematic view of the structure of the local clamp of the present invention;

FIG. 3 is an enlarged schematic view of the structure at A of FIG. 1 according to the present invention;

fig. 4 is a schematic structural view of the sliding position limiting assembly of the present invention.

In the figure: 1. a main body; 2. a sliding limit component; 201. a base plate; 202. a guide plate; 203. a sliding groove; 204. a slide plate; 205. a storage box; 3. a universal wheel; 4. a clamp dismounting structure; 401. a body; 402. a first clamp ring; 403. a second clamp ring; 404. a clamping groove; 405. a connecting bolt; 406. a handpiece.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides a hammer mill with clamp structure, including main part 1 and

clamp dismouting structure

4, 1 lower extreme of main part is provided with the spacing subassembly 2 that slides, and slide spacing subassembly 2 lower extreme and be provided with universal wheel 3, clamp dismouting structure 4 sets up in 1 one side of main part, and clamp dismouting structure 4 includes fuselage 401, first clamp ring 402, second clamp ring 403, block groove 404, connecting bolt 405 and aircraft nose 406, block groove 404 has been seted up in the fuselage 401 outside, and the block groove 404 outside is provided with first clamp ring 402, first clamp ring 402 one side is provided with second clamp ring 403, and the inside through connection bolt 405 that is provided with of second clamp ring 403, second clamp ring 403 upper end is provided with aircraft nose 406.

The utility model discloses in: the sliding limiting assembly 2 comprises a bottom plate 201, a guide plate 202, a sliding groove 203, a sliding plate 204 and a storage box 205, wherein the guide plate 202 is fixed on one side of the bottom plate 201 in a welding mode, the sliding groove 203 is formed in the guide plate 202, the sliding plate 204 is arranged on the inner side of the guide plate 202, and the storage box 205 is fixedly bonded on the upper end of the sliding plate 204.

The utility model discloses in: the sliding plate 204 and the bottom plate 201 form a sliding structure through the sliding groove 203, and one side of the bottom plate 201 is tightly attached to one side of the guide plate 202, the storage box 205 is used for containing the processed materials, when the storage box 205 contains the materials, the sliding plate 204 at the lower end of the storage box 205 is clamped with the bottom plate 201 through the sliding groove 203, the phenomenon that the storage box 205 shakes to dump can be avoided, and when the storage box 205 is filled with the materials, the sliding plate 204 at the lower end of the storage box 205 can slide leftwards along the sliding groove 203 on the inner side of the bottom plate 201, the support of the guide plate 202 can be used for avoiding the phenomenon that the storage box 205 directly falls off and the powder materials in the storage box 205 are scattered, the storage box 205 can be pushed down from the bottom plate 201, time and labor are saved, and the use reliability of the hammer mill can be improved through the structure.

The utility model discloses in: the body 401 and the first clamp ring 402 form a clamping structure through the clamping groove 404, and the inner side of the first clamp ring 402 is tightly attached to the outer sides of the body 401 and the nose 406.

The utility model discloses in: the connecting bolt 405 penetrates through the first clamp ring 402 and the second clamp ring 403, and the first clamp ring 402 and the second clamp ring 403 form a detachable structure through the connecting bolt 405.

The utility model discloses in: the lower extreme of aircraft nose 406 closely laminates with the upper end of fuselage 401, and the horizontal central line of fuselage 401 and the horizontal central line of aircraft nose 406 coincide completely, fuselage 401 and aircraft nose 406 pass through block groove 404 and first clamp ring 402 and second clamp ring 403 block, run through connecting bolt 405 inside first clamp ring 402 and second clamp ring 403 again, can realize fuselage 401 and aircraft nose 406's installation fixed, and through this structure, can realize fuselage 401 and aircraft nose 406's separation, be convenient for off-line sterilization, can carry out simple and convenient washing and maintenance to fuselage 401, the cost of operation is reduced, and the practicality is higher.

The working principle is as follows: for the hammer mill with the hoop structure, firstly, the lower end of the main body 1 is provided with the sliding limiting component 2, the storage box 205 is used for containing processed materials, when the storage box 205 contains materials, the sliding plate 204 at the lower end of the storage box 205 is clamped with the bottom plate 201 through the sliding groove 203, the phenomena of shaking and dumping of the storage box 205 and the like can be avoided, when the storage box 205 is filled with materials, the sliding plate 204 at the lower end of the storage box 205 can slide leftwards along the sliding groove 203 at the inner side of the bottom plate 201 and can avoid the phenomenon that the storage box 205 directly falls down to the ground and leads powder materials in the storage box 205 to be scattered through the support of the guide plate 202, the storage box 205 can be pushed to be taken down from the bottom plate 201, time and labor are saved, and the use reliability of the hammer mill can be improved through the structure, the lower end of the sliding limiting component 2 is provided with the universal wheel 3, the hoop dismounting structure 4 is arranged at one side of the main body 1, fuselage 401 and aircraft nose 406 pass through block groove 404 and first clamp ring 402 and the block of second clamp ring 403, run through connecting bolt 405 inside first clamp ring 402 and second clamp ring 403 again, can realize fuselage 401 and the installation of aircraft nose 406 is fixed, and through this structure, can realize the separation of fuselage 401 and aircraft nose 406, the off-line sterilization of being convenient for, can carry out simple and convenient washing and maintenance to fuselage 401, reduce the cost of operation, the practicality is higher, just so accomplish the whole use of hammer mill that has the clamp structure.

In summary, the following steps: in the utility model, the universal wheel 3 is arranged at the lower end of the sliding limiting component 2, the hoop dismounting structure 4 is arranged at one side of the main body 1, the machine body 401 and the machine head 406 are clamped with the first clamp ring 402 and the second clamp ring 403 through the clamping groove 404, and then the connecting bolt 405 is penetrated in the first clamp ring 402 and the second clamp ring 403, so that the installation and fixation of the machine body 401 and the machine head 406 can be realized, and through the structure, the separation of the machine body 401 and the machine head 406 can be realized, the off-line sterilization is convenient, the machine body 401 can be cleaned and maintained simply, the operation cost is reduced, the practicability is higher, the sliding limiting component 2 is arranged at the lower end of the main body 1, the storage box 205 is used for containing the processed material, when the storage box 205 contains the material, the sliding plate 204 at the lower end of the storage box 205 is clamped with the bottom plate 201 through the sliding groove 203, the phenomena of shaking and dumping of the storage box 205 can be avoided, and when the storage box 205 is filled with the material, can slide the slide 204 of storage box 205 lower extreme along the inboard sliding tray 203 of bottom plate 201 left, through the support of deflector 202, can avoid storage box 205 directly to drop ground and derive the phenomenon that the powder material scatters about in the storage box 205 and appear, can push storage box 205 by bottom plate 201 and take off, ten minutes labour saving and time saving, and through this structure, can improve this hammer mill's use reliability.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a hammer mill with clamp structure, includes main part (1) and clamp dismouting structure (4), its characterized in that: main part (1) lower extreme is provided with slip spacing subassembly (2), and slides spacing subassembly (2) lower extreme and be provided with universal wheel (3), clamp dismouting structure (4) set up in main part (1) one side, and clamp dismouting structure (4) include fuselage (401), first clamp ring (402), second clamp ring (403), block groove (404), connecting bolt (405) and aircraft nose (406), block groove (404) have been seted up in fuselage (401) outside, and block groove (404) outside is provided with first clamp ring (402), first clamp ring (402) one side is provided with second clamp ring (403), and second clamp ring (403) inside through being provided with connecting bolt (405), second clamp ring (403) upper end is provided with aircraft nose (406).

2. The hammer mill with the hoop structure of claim 1, wherein: the sliding limiting assembly (2) comprises a bottom plate (201), a guide plate (202), a sliding groove (203), a sliding plate (204) and a storage box (205), wherein the guide plate (202) is welded and fixed on one side of the bottom plate (201), the sliding groove (203) is formed in the guide plate (202), the sliding plate (204) is arranged on the inner side of the guide plate (202), and the storage box (205) is fixedly bonded on the upper end of the sliding plate (204).

3. The hammer mill with the hoop structure of claim 2, wherein: the sliding plate (204) and the bottom plate (201) form a sliding structure through the sliding groove (203), and one side of the bottom plate (201) is tightly attached to one side of the guide plate (202).

4. The hammer mill with the hoop structure of claim 1, wherein: the machine body (401) and the first clamp ring (402) form a clamping structure through the clamping groove (404), and the inner side of the first clamp ring (402) is tightly attached to the outer sides of the machine body (401) and the machine head (406).

5. The hammer mill with the hoop structure of claim 1, wherein: the connecting bolt (405) penetrates through the first clamp ring (402) and the second clamp ring (403), and the first clamp ring (402) and the second clamp ring (403) form a dismounting structure through the connecting bolt (405).

6. The hammer mill with the hoop structure of claim 1, wherein: the lower end of the machine head (406) is tightly attached to the upper end of the machine body (401), and the transverse center line of the machine body (401) is completely overlapped with the transverse center line of the machine head (406).