CN209865830U

CN209865830U - Processing equipment for organosilicon adhesive sealant

Info

Publication number: CN209865830U
Application number: CN201821983103.4U
Authority: CN
Inventors: 刘育建
Original assignee: Nanjing Tianshuangchen New Materials Co Ltd
Current assignee: Nanjing Tianshuangchen New Materials Co Ltd
Priority date: 2018-11-29
Filing date: 2018-11-29
Publication date: 2019-12-31
Anticipated expiration: 2028-11-29

Abstract

The utility model discloses a processing equipment of organosilicon bonding sealant, including the aircraft nose, the bottom of aircraft nose is provided with the processing axle, the top surface of processing axle is the circumferencial formula and has seted up a plurality of connecting hole through holes, the top of connecting hole through hole is fixed with the connection bayonet lock, the inside of connecting the bayonet lock has seted up the shrinkage pool, the shrinkage pool is in same vertical line with the center of connecting hole through hole, and the connecting hole through hole equals with the diameter of shrinkage pool; through the connection bayonet lock of design, can be when installation processing axle and aircraft nose, the time that the screw consumes is look for in great reduction, the effectual work efficiency that has improved, avoid the long-time lift processing axle of user and the tired sense that causes simultaneously to and design the stopper and can carry out the secondary on current bolted connection's basis and fix, alleviateed the load of connecting stud, make the stability of connecting obtain guaranteeing.

Description

Processing equipment for organosilicon adhesive sealant

Technical Field

The utility model belongs to the technical field of the processing equipment, concretely relates to sealed processing equipment who glues of organosilicon bonding.

Background

The organic silicon adhesive sealant is a deketoxime type sealant prepared on the basis of imported special silica gel raw materials, has the characteristics of no metal corrosion and excellent yellowing resistance, has a very wide application range, is also applied to the industries of vehicle lamps and electronic appliances, such as wire harnesses, controllers and the like, and needs to be produced by using special tools in the early production.

The existing processing equipment still has some defects when in use: the sealed processing equipment that glues now is in the installation of earlier stage, need pass through the bolt with the processing axle and install the bottom face at the aircraft nose, process with this, nevertheless in the installation, need align the screw of aircraft nose bottom with the screw on processing axle surface, it is comparatively inconvenient to operate, in the period of aligning the screw, because lift up the processing axle for a long time, can cause certain tired sense for operating personnel, and simultaneously because the processing axle is in the bottom of aircraft nose and unsettled, both's connection only depends on bolted connection, long-time use, can cause great load for the bolt, thereby influence bolted connection's stability.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a sealed processing equipment that glues of organosilicon bonding, in the current sealed processing equipment that glues that proposes in solving above-mentioned background art in the installation of phase ahead, need to process the axle and pass through the bolt and install the bottom face at the aircraft nose, process with this, nevertheless in the installation, need align the screw of aircraft nose bottom with the screw on processing axle surface, it is comparatively inconvenient to operate, in the period of aligning the screw, because lift up the processing axle for a long time, can cause certain tired sense for operating personnel, and simultaneously because the processing axle is in the bottom of aircraft nose and unsettled, both connections only lean on bolted connection, long-time use, can cause great load for the bolt, thereby influence the problem of bolted connection's stability.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a sealed processing equipment that glues of organosilicon bonding, includes the aircraft nose, the bottom of aircraft nose is provided with the processing axle, a plurality of connecting hole through holes have been seted up to the top surface of processing axle for the circumference formula, the top of connecting hole through hole is fixed with the connection bayonet lock, the shrinkage pool has been seted up to the inside of connecting the bayonet lock, the shrinkage pool is in same vertical on-line with the center of connecting hole through hole, and the diameter of connecting hole through hole and shrinkage pool equals, the connecting hole has been seted up to the bottom face of aircraft nose, the side channel has been seted up to the inner wall symmetry of connecting hole, the bayonet lock is connected to the processing.

Preferably, the through-hole has been seted up on the top of shrinkage pool, the side opening has been seted up to the inner wall both sides of through-hole, the inboard of side opening is provided with the stopper, the both sides of stopper and the inner wall junction of side opening are provided with expanding spring, the side channel has been seted up to the inner wall bilateral symmetry of connecting hole, connecting stud has been placed to the inboard of shrinkage pool, connecting stud is through the top threaded connection who runs through-hole and connecting hole, connecting stud accessible extrusion stopper is fixed with its inboard and the connecting hole of card income to the side channel.

Preferably, a vertical column is fixed to one side, opposite to the processing shaft, of the bottom end of the machine head, an operation box is arranged on the outer side of the vertical column, a T-shaped connecting block is fixed to the rear end face of the operation box, a T-shaped placing groove is fixed to the surface of the vertical column, and the operation box is inserted into the T-shaped placing groove through the T-shaped connecting block and fixed to the vertical column.

Preferably, a base is fixed at the bottom end of the upright column, a block-shaped body is arranged on the side edge of the base, and the base can be fixed with external equipment through the block-shaped body.

Preferably, the bottom end surface of the processing shaft is provided with a stirrer, and the stirrer is in a cross shape.

Preferably, a material barrel is placed at the bottom end of the inner side of the base, which is opposite to the stirrer, and the bottom end of the material barrel is provided with a roller.

Preferably, the end face of the machine head is provided with an alarm lamp, and the alarm lamp and the operation box are both electrically connected with external equipment.

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

1. by the designed connecting clamping pin, the time consumed for searching a screw hole can be greatly reduced when the processing shaft and the machine head are installed, the working efficiency is effectively improved, meanwhile, the fatigue feeling caused by long-time lifting of the processing shaft by a user is avoided, and the design limiting block can carry out secondary fixing on the basis of the existing bolt connection, so that the load of a connecting stud is reduced, and the stability of connection is ensured;

2. through the T type standing groove and the T type connecting block of design, can carry out simple effectual being connected with control box and stand to great having made things convenient for the dismantlement in later stage, in use also can carry out stable the placing to the control box simultaneously.

Drawings

Fig. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic view of the connection between the machine head and the processing shaft of the present invention;

fig. 3 is an enlarged schematic view of the area a of the present invention;

FIG. 4 is a schematic view of the connection between the limiting block and the connecting pin of the present invention;

fig. 5 is an enlarged schematic view of the region B of the present invention;

fig. 6 is a schematic view of the connection between the T-shaped placing groove and the T-shaped connecting block of the present invention.

In the figure: 1. a machine head; 2. processing a shaft; 3. a stirrer; 4. a charging barrel; 5. a base; 6. a column; 7. an operation box; 8. a through hole; 9. a side hole; 10. concave holes; 11. connecting a bayonet lock; 12. a limiting block; 13. a through hole; 14. a side groove; 15. connecting a stud; 16. a tension spring; 17. a T-shaped placing groove; 18. t-shaped connecting blocks.

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.

Example 1

Referring to fig. 1 to 5, the present invention provides a technical solution: a processing device for organosilicon adhesive sealant comprises a machine head 1, a processing shaft 2 is arranged at the bottom of the machine head 1, a plurality of connecting hole through holes 8 are circumferentially arranged on the top surface of the processing shaft 2, connecting clamping pins 11 are fixed at the top ends of the connecting hole through holes 8, concave holes 10 are arranged inside the connecting clamping pins 11, the centers of the concave holes 10 and the connecting hole through holes 8 are positioned on the same vertical line, the diameter of the through hole 8 of the connecting hole is equal to that of the concave hole 10, the bottom end face of the machine head 1 is provided with the connecting hole, the inner wall of the connecting hole is symmetrically provided with side grooves 14, the processing shaft 2 can be inserted into the connecting hole through the connecting bayonet lock 11 to be connected with the machine head 1, through the designed connecting bayonet lock 11, can be when installation processing axle 2 and aircraft nose 1, the time that the screw was consumeed is look for in great reduction, the effectual work efficiency that has improved, avoid the user to lift processing axle 2 for a long time and the tired sense that causes simultaneously.

In this embodiment, it is preferred, through-hole 13 has been seted up on the top of shrinkage pool 10, side hole 9 has been seted up to the inner wall both sides of through-hole 13, the inboard of side hole 9 is provided with stopper 12, the both sides of stopper 12 are provided with expanding spring 16 with the inner wall junction of side hole 9, side channel 14 has been seted up to the inner wall bilateral symmetry of connecting hole, connecting stud 15 has been placed to the inboard of shrinkage pool 10, connecting stud 15 is through the top threaded connection who runs through-hole 13 and connecting hole, connecting stud 15 accessible extrusion stopper 12 is fixed with its inboard of card income to side channel 14 with the connecting hole, design stopper 12 can carry out the secondary fixation on current bolted connection's basis, the load of connecting stud 15 has been alleviateed.

Example 2

Referring to fig. 1 to 6, the present invention provides a technical solution: a processing device for organosilicon adhesive sealant comprises a machine head 1, a processing shaft 2 is arranged at the bottom of the machine head 1, a plurality of connecting hole through holes 8 are circumferentially arranged on the top surface of the processing shaft 2, connecting clamping pins 11 are fixed at the top ends of the connecting hole through holes 8, concave holes 10 are arranged inside the connecting clamping pins 11, the centers of the concave holes 10 and the connecting hole through holes 8 are positioned on the same vertical line, the diameter of the through hole 8 of the connecting hole is equal to that of the concave hole 10, the bottom end face of the machine head 1 is provided with the connecting hole, the inner wall of the connecting hole is symmetrically provided with side grooves 14, the processing shaft 2 can be inserted into the connecting hole through the connecting bayonet lock 11 to be connected with the machine head 1, through the designed connecting bayonet lock 11, can be when installation processing axle 2 and aircraft nose 1, the time that the screw was consumeed is look for in great reduction, the effectual work efficiency that has improved, avoid the user to lift processing axle 2 for a long time and the tired sense that causes simultaneously.

In this embodiment, it is preferred, the bottom of aircraft nose 1 is fixed with stand 6 for one side of processing axle 2, the outside of stand 6 is provided with control box 7, the rear end face of control box 7 is fixed with T type connecting block 18, the fixed surface of stand 6 has T type standing groove 17, control box 7 inserts in T type standing groove 17 through T type connecting block 18 and is fixed with stand 6, T type standing groove 17 and T type connecting block 18 through the design, can carry out simple effectual being connected with control box 7 and stand 6, thereby great convenience is given to the dismantlement in later stage, in use also can carry out stable placing to control box 7 simultaneously.

The utility model discloses a theory of operation and use flow: when the utility model is used, the sealant to be processed is placed in the charging barrel 4, then the operation box 7 is started, the operation box 7 drives the stirrer 3 at the bottom end of the processing shaft 2 to rotate, and the sealant in the charging barrel 4 is stirred and processed by the stirrer 3;

when the processing shaft 2 is connected with the machine head 1, the processing shaft 2 is firstly inserted into a connecting hole at the bottom end of the machine head 1 through a connecting bayonet lock 11 at the top end, then a connecting stud 15 is inserted into a through hole 8 of the connecting hole and reaches a concave hole 10 formed in the connecting bayonet lock 11 through the through hole 8 of the connecting hole, at the moment, the connecting stud 15 is continuously inserted into an insertion through hole 13 towards the top end of the connecting bayonet lock 11, the end part of the connecting stud 15 extrudes a limiting block 12, the limiting block 12 is extruded by the end part of the connecting stud 15 and moves towards the outer side of the connecting bayonet lock 11 and is inserted into a side groove 14 formed in the inner wall of the connecting hole, the limiting block 12 pulls a telescopic spring 16 in movement, at the moment, the connecting stud 15 reaches the top end part of the connecting hole, is connected with the position provided with threads on, then the limiting block 12 is restored to the original position under the rebound of the extension spring 16, the machine head 1 and the processing shaft 2 can be separated at the moment, and when the operation box 7 is installed, the T-shaped connecting block 18 on the rear surface of the operation box 7 is clamped into the T-shaped placing groove 17 to complete installation.

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 sealed processing equipment that glues of organosilicon bonding, includes aircraft nose (1), the bottom of aircraft nose (1) is provided with processing axle (2), its characterized in that: the top surface of processing axle (2) is the circumference formula and has seted up a plurality of connecting hole through holes (8), the top of connecting hole through hole (8) is fixed with connects bayonet lock (11), shrinkage pool (10) have been seted up to the inside of connecting bayonet lock (11), shrinkage pool (10) are in same vertical on-line with the center of connecting hole through hole (8), and connecting hole through hole (8) are equal with the diameter of shrinkage pool (10), the connecting hole has been seted up to the bottom face of aircraft nose (1), side channel (14) have been seted up to the inner wall symmetry of connecting hole, processing axle (2) accessible is connected bayonet lock (11) and is inserted in the connecting hole and is connected with aircraft nose (1).

2. The processing equipment of the organosilicon adhesive sealant according to claim 1, characterized in that: through-hole (13) have been seted up on the top of shrinkage pool (10), side hole (9) have been seted up to the inner wall both sides of through-hole (13), the inboard of side hole (9) is provided with stopper (12), the both sides of stopper (12) are provided with expanding spring (16) with the inner wall junction of side hole (9), side channel (14) have been seted up to the inner wall bilateral symmetry of connecting hole, connecting stud (15) have been placed to the inboard of shrinkage pool (10), connecting stud (15) are through the top threaded connection who runs through-hole (13) and connecting hole, connecting stud (15) accessible extrusion stopper (12) are fixed with the inboard and the connecting hole of its card income to side channel (14).

3. The processing equipment of the organosilicon adhesive sealant according to claim 1, characterized in that: the bottom of aircraft nose (1) is fixed with stand (6) for one side of processing axle (2), the outside of stand (6) is provided with control box (7), the rear end face of control box (7) is fixed with T type connecting block (18), the fixed surface of stand (6) has T type standing groove (17), control box (7) are fixed with stand (6) in inserting T type standing groove (17) through T type connecting block (18).

4. The apparatus for processing silicone adhesive sealant according to claim 3, wherein: the bottom end of the upright post (6) is fixed with a base (5), the side edge of the base (5) is provided with a block-shaped body, and the base (5) can be fixed with external equipment through the block-shaped body.

5. The apparatus for processing silicone adhesive sealant according to claim 3, wherein: the bottom surface of processing axle (2) is provided with agitator (3), agitator (3) are the fork form.

6. The apparatus for processing silicone adhesive sealant according to claim 4, wherein: a charging barrel (4) is placed on the inner side of the base (5) relative to the bottom end of the stirrer (3), and rollers are arranged at the bottom end of the charging barrel (4).

7. The processing equipment of the organosilicon adhesive sealant according to claim 1, characterized in that: the terminal surface of aircraft nose (1) is provided with the warning light, warning light and control box (7) all are connected with external equipment electricity.