CN217147073U

CN217147073U - Anti-deformation device for machining cutting fluid for aerospace

Info

Publication number: CN217147073U
Application number: CN202220637910.0U
Authority: CN
Inventors: 黄文飞; 杨同勇; 李文瀚; 王剑; 吕栓锁; 卢建明; 朱国玉
Original assignee: Dalian Sandaaoke Chemistry Co Ltd
Current assignee: Dalian Sandaaoke Chemistry Co Ltd
Priority date: 2022-03-23
Filing date: 2022-03-23
Publication date: 2022-08-09
Anticipated expiration: 2032-03-23

Abstract

The utility model discloses a cutting fluid processing is with preventing that it is poor to matter device for aerospace, including base and bin, the inside rabbling mechanism that is provided with of bin, the rabbling mechanism is including well core rod, bevel gear one, bevel gear two and bevel gear three, well core rod upper end fixed connection is in the inside upper surface center of bin, bevel gear one is rotatory cup joints in well core rod surface upside, bevel gear one is rotatory cup joints in well core rod surface downside, bevel gear three transversely is close well core rod one side center fixedly connected with connecting rod, connecting rod other end swivelling joint is on central pole surface, bevel gear three about both sides face respectively with bevel gear one, bevel gear two meshes the connection. The utility model discloses in, open the motor and make stir board one and stir the board and stir two pairs of cutting fluids and make each part of cutting fluid be in the ventilation state, avoid rotten, stir board one and stir two reverse stirring of board, efficiency is higher.

Description

Anti-deformation device for machining cutting fluid for aerospace

Technical Field

The utility model relates to the technical field, especially, relate to a cutting fluid processing is with preventing transformer for aerospace.

Background

The cutting fluid is an industrial fluid used for cooling and lubricating tools and workpieces in the metal cutting and polishing process, has good cooling, lubricating, antirust, anticorrosion and other properties, and is usually stored in a storage device after being used.

At present, the existing anti-deterioration device for machining the cutting fluid for aerospace still has the defects, and most of the existing cutting fluid is kept still after being placed in a storage device, so that a large amount of bacteria are bred at the non-ventilated part inside the cutting fluid.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide a: in order to solve the problems, the anti-deformation device for machining the cutting fluid is provided for aerospace.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

an anti-deformation device for machining cutting fluid for aerospace comprises a base and a storage box, wherein an agitating mechanism is arranged inside the storage box, the agitating mechanism comprises a first central rod, a second bevel gear and a third bevel gear, the upper end of the central rod is fixedly connected to the center of the upper surface inside the storage box, the first bevel gear is rotatably sleeved on the upper side of the surface of the central rod, the second bevel gear is rotatably sleeved on the lower side of the surface of the central rod, the third bevel gear is transversely close to the center of one surface of the central rod, the other end of the connecting rod is rotatably connected to the surface of the central rod, the upper side surface and the lower side surface of the third bevel gear are respectively connected with the first bevel gear and the second bevel gear in a meshed manner, the upper side and the lower side of the surface of the central rod are respectively sleeved with a first sleeve pipe and a second sleeve pipe, the first sleeve pipe is fixedly connected to the upper surface of the first bevel gear, the second sleeve pipe is fixedly connected to the bottom surface of the second bevel gear, the horizontal both sides fixedly connected with puddler one of sleeve pipe, the vertical both sides fixedly connected with puddler two of sleeve pipe two.

Preferably, the bottom end of the first stirring rod is fixedly connected with a first stirring plate, and the bottom end of the second stirring rod is fixedly connected with a second stirring plate.

Preferably, a driven gear is fixedly connected to the upper surface of the first sleeve, the driven gear is rotatably sleeved at the upper end of the central rod, and a driving gear is meshed and connected to one transverse side of the driven gear.

Preferably, the horizontal one side fixedly connected with motor of bin upper surface, the transmission shaft of motor extends to the bin inside and fixed connection in driving gear upper surface center.

Preferably, a feed inlet is fixedly connected to one lateral side of the upper surface of the storage box.

Preferably, a plurality of ventilation openings are uniformly formed in the top of the side surface of the storage box.

To sum up, owing to adopted above-mentioned technical scheme, the beneficial effects of the utility model are that:

this application is through inside the feed inlet with the cutting fluid injection bin, open the motor, thereby the driving gear begins to rotate and makes driven gear rotate, fixed surface is connected with driven gear on the sleeve pipe one, sleeve pipe one fixed connection is in bevel gear one upper surface, so bevel gear first begins to rotate, bevel gear three upper and lower both sides face respectively with bevel gear one, bevel gear two meshes the connection, so bevel gear two antiport, sleeve pipe two fixed connection is in bevel gear two bottom surfaces, sleeve pipe two begins antiport, sleeve pipe one horizontal both sides fixedly connected with puddler one, sleeve pipe two vertical both sides fixedly connected with puddler two, puddler one bottom fixedly connected with stirs board one, puddler two bottom fixedly connected with stirs board two, so stir board one and stir board two and begin to stir the cutting fluid, a plurality of vents have evenly been seted up at bin side surface top, do benefit to inside ventilation, open the motor and make stir board one and stir board two pairs of cutting fluid and make each part of cutting fluid in the ventilation of cutting fluid stir And in a state, deterioration is avoided, and the stirring plate I and the stirring plate II are reversely stirred, so that the efficiency is higher.

Drawings

Fig. 1 is a schematic view illustrating an overall structure of an anti-deterioration device according to an embodiment of the present invention;

fig. 2 is a schematic diagram illustrating an explosion structure of a deterioration prevention device according to an embodiment of the present invention;

fig. 3 shows an overall structural schematic diagram of an agitation mechanism provided by the embodiment of the present invention.

Illustration of the drawings:

1. a base; 2. a storage tank; 3. a center pole; 4. a first bevel gear; 5. a second bevel gear; 6. a third bevel gear; 7. a connecting rod; 8. a first sleeve; 9. a second sleeve; 10. a first stirring rod; 11. a second stirring rod; 12. a first stirring plate; 13. a second stirring plate; 14. a driven gear; 15. a driving gear; 16. a motor; 17. a feed inlet; 18. And a vent.

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 of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.

Referring to fig. 1-3, the present invention provides a technical solution:

an anti-deterioration device for machining cutting fluid for aerospace comprises a base 1 and a storage box 2, wherein an agitating mechanism is arranged inside the storage box 2, the agitating mechanism comprises a central rod 3, a first bevel gear 4, a second bevel gear 5 and a third bevel gear 6, the upper end of the central rod 3 is fixedly connected to the center of the upper surface inside the storage box 2, the first bevel gear 4 is rotatably sleeved on the upper side of the surface of the central rod 3, the second bevel gear 5 is rotatably sleeved on the lower side of the surface of the central rod 3, the third bevel gear 6 is transversely close to the center of one surface of the central rod 3 and is fixedly connected with a connecting rod 7, the other end of the connecting rod 7 is rotatably connected to the surface of the central rod 3, the upper side surface and the lower side surface of the third bevel gear 6 are respectively meshed with the first bevel gear 4, the upper side and the lower side of the surface of the central rod 3 are respectively sleeved with a first sleeve 8 and a second sleeve 9, and the first sleeve 8 is fixedly connected to the upper surface of the first bevel gear 4, the second sleeve 9 is fixedly connected to the bottom surface of the second bevel gear 5, the first stirring rod 10 is fixedly connected to the two transverse sides of the first sleeve 8, and the second stirring rod 11 is fixedly connected to the two longitudinal sides of the second sleeve 9.

Specifically, as shown in fig. 3, the bottom end of the first stirring rod 10 is fixedly connected with a first stirring plate 12, and the bottom end of the second stirring rod 11 is fixedly connected with a second stirring plate 13.

Specifically, as shown in fig. 3, the upper surface of the first sleeve 8 is fixedly connected with a driven gear 14, the driven gear 14 is rotatably sleeved at the upper end of the central rod 3, and one lateral side of the driven gear 14 is engaged with a driving gear 15.

Specifically, as shown in fig. 2, a motor 16 is fixedly connected to one lateral side of the upper surface of the storage box 2, and a transmission shaft of the motor 16 extends into the storage box 2 and is fixedly connected to the center of the upper surface of the driving gear 15.

Specifically, as shown in fig. 2, a feed port 17 is fixedly connected to one lateral side of the upper surface of the storage box 2.

Specifically, as shown in fig. 2, a plurality of ventilation openings 18 are uniformly formed at the top of the side surface of the storage box 2.

In summary, in the anti-deterioration device for machining cutting fluid for aerospace provided by this embodiment, a feed inlet 17 is fixedly connected to one lateral side of the upper surface of the storage box 2, the cutting fluid is injected into the storage box 2 through the feed inlet 17, the motor 16 is turned on, a transmission shaft of the motor 16 extends into the storage box 2 and is fixedly connected to the center of the upper surface of the driving gear 15, so that the driving gear 15 starts to rotate, so that the driven gear 14 rotates, the driven gear 14 is fixedly connected to the upper surface of the first sleeve 8, the first sleeve 8 is fixedly connected to the upper surface of the first bevel gear 4, so that the first bevel gear 4 starts to rotate, the upper and lower side surfaces of the third bevel gear 6 are respectively engaged with the first bevel gear 4 and the second bevel gear 5, so that the second bevel gear 5 rotates in reverse direction, the second sleeve 9 is fixedly connected to the bottom surface of the second bevel gear 5, the second sleeve 9 starts to rotate in reverse direction, and the first stirring rods 10 are fixedly connected to two lateral sides of the first sleeve 8, the vertical both sides fixedly connected with puddler two 11 of sleeve pipe two 9, puddler one 10 bottom fixedly connected with stir board one 12, and puddler two 11 bottom fixedly connected with stir board two 13, so stir board one 12 and stir board two 13 and begin to stir the cutting fluid, and 2 side surface tops of bin have evenly seted up a plurality of vents 18, do benefit to inside ventilation.

The previous description of the embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.

Claims

1. The utility model provides a cutting fluid processing is with preapring for an unfavorable turn of events matter device for aerospace, includes base (1) and bin (2), its characterized in that, the inside rabbling mechanism that is provided with of bin (2), rabbling mechanism is including well core rod (3), bevel gear (4), bevel gear two (5) and bevel gear three (6), well core rod (3) upper end fixed connection is in the inside upper surface center of bin (2), bevel gear one (4) rotatory cup joint in well core rod (3) surface upside, bevel gear two (5) rotatory cup joint in well core rod (3) surface downside, bevel gear three (6) transversely are close well core rod (3) one side center fixed connection have connecting rod (7), connecting rod (7) other end swivelling joint in well core rod (3) surface, bevel gear three (6) upper and lower both sides face respectively with bevel gear one (4), bevel gear two (5) meshing connection, sleeve pipe one (8) and sleeve pipe two (9) have been cup jointed respectively to well core rod (3) both sides about the surface, sleeve pipe one (8) fixed connection is in bevel gear one (4) upper surface, sleeve pipe two (9) fixed connection is in bevel gear two (5) bottom surface, sleeve pipe one (8) horizontal both sides fixedly connected with puddler one (10), sleeve pipe two (9) vertical both sides fixedly connected with puddler two (11).

2. The anti-deterioration device for machining the cutting fluid for aerospace, according to claim 1, wherein a first stirring plate (12) is fixedly connected to the bottom end of the first stirring rod (10), and a second stirring plate (13) is fixedly connected to the bottom end of the second stirring rod (11).

3. The device for preventing the cutting fluid from being degraded in the aerospace machining process according to claim 1, wherein a driven gear (14) is fixedly connected to the upper surface of the first sleeve (8), the driven gear (14) is rotatably sleeved on the upper end of the central rod (3), and a driving gear (15) is meshed and connected to one lateral side of the driven gear (14).

4. The device for preventing the machining of the cutting fluid for aerospace according to claim 1, wherein a motor (16) is fixedly connected to one side of the upper surface of the storage tank (2) in the transverse direction, and a transmission shaft of the motor (16) extends into the storage tank (2) and is fixedly connected to the center of the upper surface of the driving gear (15).

5. The device for preventing the machining of the cutting fluid for the aerospace according to claim 1, wherein a feed port (17) is fixedly connected to one side of the transverse direction of the upper surface of the storage tank (2).

6. The device for preventing the machining of the cutting fluid for the aerospace as claimed in claim 1, wherein a plurality of ventilation openings (18) are uniformly formed in the top of the side surface of the storage tank (2).