CN217483095U

CN217483095U - Cooling device for machining of aircraft parts

Info

Publication number: CN217483095U
Application number: CN202221181256.3U
Authority: CN
Inventors: 李国立
Original assignee: Chengdu Haoyiqiang Aviation Equipment Manufacturing Co ltd
Current assignee: Chengdu Haoyiqiang Aviation Equipment Manufacturing Co ltd
Priority date: 2022-05-17
Filing date: 2022-05-17
Publication date: 2022-09-23
Anticipated expiration: 2032-05-17

Abstract

The utility model discloses a heat sink is used in aircraft parts processing belongs to aircraft parts processing technology field. A cooling device for processing aircraft parts comprises a machine body and a refrigerator body, wherein a supporting plate is fixedly connected in the machine body, a placing plate is fixedly connected on the supporting plate, a square plate is fixedly connected to the top of the supporting plate, a plurality of spray heads are fixedly connected to the square plate, a liquid collecting box is fixedly connected to the bottom in the machine body, a box cover is connected to the liquid collecting box, a first water pump is fixedly connected in the liquid collecting box, a first water pipe is fixedly connected to the first water pump, a water tank is fixedly connected to the left side of the machine body, a second water pump is fixedly connected in the water tank, a second water pipe is fixedly connected to the second water pump, an air extractor is fixedly connected to the inner wall of the top of the machine body, and an air exhaust pipe and an air outlet pipe are fixedly connected to the air extractor; the utility model discloses can realize the cyclic utilization to the water resource at the cooling in-process, the steam contact that spare part produced when can reducing the human body and cool off, protection personal safety.

Description

Cooling device for machining of aircraft parts

Technical Field

The utility model relates to an aircraft parts processing technology field especially relates to a heat sink is used in aircraft parts processing.

Background

The aircraft need carry out the processing to very many parts in the manufacturing process, nevertheless is going on to the spare part in-process, needs to carry out the cooling treatment through the heat sink to the spare part of processing, and at present, common heat sink adopts the fan to lead to cold wind usually and cools down, perhaps adopts the cooling water to cool down.

However, the existing cooling device for machining aircraft parts cannot recycle water resources when being used, cooled water is discharged, a large amount of water resources are wasted, and a large amount of hot air can be generated in the cooling process and discharged indoors to influence human bodies.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the problem that the existing cooling device in the prior art can not recycle water resource and produce a large amount of steam in the course of working when carrying out the use, and the cooling device is used in the processing of aircraft spare part that provides.

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

a cooling device for processing airplane parts comprises a machine body and a refrigerator body, wherein a supporting plate is fixedly connected in the machine body, a placing plate is fixedly connected to the supporting plate, a square plate is fixedly connected to the top of the supporting plate, the square plate is fixedly connected with a plurality of spray heads, the bottom in the machine body is fixedly connected with a liquid collecting box, the liquid collecting box is connected with a box cover, a first water pump is fixedly connected in the liquid collecting box, the refrigerator body is fixedly connected in the liquid collecting box, the first water pump is fixedly connected with a first water pipe, the left side of the machine body is fixedly connected with a water tank, the first water pipe is arranged in the water tank, a second water pump is fixedly connected in the water tank, a second water pipe is fixedly connected on the second water pump, the second water pipe is communicated with the spray head, the inner wall of the top of the machine body is fixedly connected with an air pump, and an air pumping pipe and an air outlet pipe are fixedly connected to the air pump.

Preferably, the case cover is detachably connected to the liquid collecting tank, the liquid accumulating tank is formed in the top surface of the case cover, a water inlet hole is formed in the case cover, and the liquid accumulating tank is communicated with the liquid collecting tank through the water inlet hole.

Preferably, a filter plate is fixedly connected in the liquid collection tank, the water pumping end of the first water pump is arranged in the liquid collection tank, the first water pipe is fixedly connected at the water outlet end of the first water pump, and one end, far away from the liquid collection tank, of the first water pipe is fixedly connected in the water tank.

Preferably, the through-hole has been seted up to the left side outer wall of organism, water tank fixed connection is on the through-hole, the left side outer wall fixedly connected with water injection pipe of water tank, be equipped with the stopcock on the water injection pipe.

Preferably, the water pumping end of the second water pump is arranged in the water tank, the second water pipe is fixedly connected to the water outlet end of the second water pump, and one end of the second water pipe, which is arranged in the machine body, is fixedly connected to the support plate.

Preferably, a liquid inlet cavity is formed in the square plate, the second water pipe is communicated with the liquid inlet cavity, and the spray head is communicated with the liquid inlet cavity.

Preferably, the inner wall of the top of the machine body is fixedly connected with a mounting frame, the air pump is fixedly connected on the mounting frame, the air exhaust pipe is fixedly connected at the air inlet end of the air pump, the air outlet pipe is fixedly connected at the air outlet end of the air pump,

preferably, one end of the exhaust pipe, which is far away from the air pump, is fixedly connected with an exhaust head, and one end of the exhaust pipe, which is far away from the air pump, penetrates through the outer wall of the right side of the machine body and extends outwards.

Preferably, the placing plate is obliquely placed, a baffle is fixedly connected to the bottom of the placing plate, and a plurality of round holes are formed in the baffle.

Preferably, a sliding groove is formed in the machine body, a sealing door is connected to the sliding groove in a sliding mode, an observation window is formed in the sealing door, and a door handle is fixedly mounted on the sealing door.

Compared with the prior art, the utility model provides a heat sink is used in aircraft parts processing possesses following beneficial effect:

1. this heat sink is used in aircraft parts processing, the cooling water in the water tank cools off placing the spare part on the board through the shower nozzle, absorbs the heat back cooling water of spare part and is heated, flows into the collection liquid case through the filter screen in, the filter filters impurity such as piece in the water, then starts the refrigerator body and cools off the water of retrieving, carries through first water pump after the cooling is accomplished in meeting the water tank, reaches the purpose that water resource circulation used.

2. This heat sink is used in aircraft parts processing can produce a large amount of steam after cooling water and the contact of high temperature spare part, starts the air extractor this moment, and the air extractor passes through the exhaust tube and extracts steam, then through the outlet duct outside steam discharge, can reduce the contact of human body and steam, prevents to be burnt by steam.

The part that does not relate to in the device all is the same with prior art or can adopt prior art to realize, the utility model discloses can realize the cyclic utilization to the water resource at the cooling in-process, the water economy resource can reduce the steam contact that human and spare part produced when cooling, prevents to be burnt by steam, protection staff health safety.

Drawings

Fig. 1 is a schematic view of a front view structure of a cooling device for processing aircraft parts provided by the present invention;

fig. 2 is a schematic front sectional structural view of a cooling device for processing aircraft parts according to the present invention;

fig. 3 is a schematic side view of a placement plate of a cooling device for processing aircraft parts according to the present invention;

fig. 4 is an enlarged schematic structural view of a portion a in fig. 2 of the cooling device for processing aircraft parts according to the present invention;

fig. 5 is an enlarged schematic structural view of a portion B in fig. 2 of a cooling device for processing aircraft parts according to the present invention.

In the figure: 1. a body; 2. a support plate; 3. placing the plate; 4. a square plate; 5. a liquid collection tank; 6. a box cover; 7. a liquid accumulation tank; 8. a filter plate; 9. a refrigerator body; 10. a first water pump; 11. a first water pipe; 12. a water tank; 13. a second water pump; 14. a second water pipe; 15. a water injection pipe; 16. a pipe plug; 17. an air extractor; 18. a mounting frame; 19. an air exhaust pipe; 20. an air pumping head; 21. an air outlet pipe; 22. a spray head; 23. a liquid inlet cavity; 24. a water inlet hole; 25. a baffle plate; 26. a circular hole; 27. a sliding groove; 28. a sealing door; 29. an observation window; 30. a door handle; 31. and a through hole.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the 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.

In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

The embodiment is as follows:

referring to fig. 1-5, a cooling device for processing aircraft parts comprises a machine body 1 and a refrigerator body 9, a support plate 2 is fixedly connected in the machine body 1, a placing plate 3 is fixedly connected on the support plate 2, a square plate 4 is fixedly connected on the top of the support plate 2, a plurality of spray heads 22 are fixedly connected on the square plate 4, a liquid collecting tank 5 is fixedly connected on the bottom in the machine body 1, a tank cover 6 is connected on the liquid collecting tank 5, a first water pump 10 is fixedly connected in the liquid collecting tank 5, the refrigerator body 9 is fixedly connected in the liquid collecting tank 5, a first water pipe 11 is fixedly connected on the first water pump 10, a water tank 12 is fixedly connected on the left side of the machine body 1, the first water pipe 11 is arranged in the water tank 12, a second water pump 13 is fixedly connected in the water tank 12, a second water pipe 14 is fixedly connected on the second water pump 13, the second water pipe 14 is communicated with the spray heads 22, and an air extractor 17 is fixedly connected on the inner wall of the top of the machine body 1, the air pump 17 is fixedly connected with an air pumping pipe 19 and an air outlet pipe 21, the refrigerator body 9 is the most commonly used semiconductor refrigerator, has the characteristics of no noise, no vibration, no need of refrigerant, small volume, light weight and the like, and is reliable in operation, simple and convenient to operate and easy to regulate cold quantity.

The connection can be dismantled on liquid collecting box 5 to case lid 6, and hydrops groove 7 has been seted up on 6 top surfaces of case lid, has seted up inlet opening 24 in case lid 6, and hydrops groove 7 is linked together with liquid collecting box 5 through inlet opening 24, and hydrops groove 7 can prevent that the cooling water of retrieving from overflowing to organism 1 in, flows into liquid collecting box 5 through inlet opening 24.

Fixedly connected with filter 8 in collection liquid box 5, the end of drawing water of first water pump 10 is placed in

collection liquid box

5, 11 fixed connection of first water pipe are at the play water end of first water pump 10, the one end fixed connection that collection liquid box 5 was kept away from to first water pipe 11 is in water tank 12, filter 8 divide into two-layerly, the first layer is the quartz sand filter layer, the second floor is the active carbon filter layer, can reach and carry out filtration purification's purpose to the water after carrying out cooling treatment, and then reach water cyclic utilization's purpose.

Through-hole 31 has been seted up to the left side outer wall of organism 1, and water tank 12 fixed connection is on through-hole 31, and water tank 12's left side outer wall fixedly connected with water injection pipe 15 is equipped with stopcock 16 on the water injection pipe 15, uses up the back when the cooling water, carries out the interpolation of cooling water to water tank 12 through water injection pipe 15.

The water pumping end of the second water pump 13 is arranged in the water tank 12, the second water pipe 14 is fixedly connected to the water outlet end of the second water pump 13, one end of the second water pipe 14, which is arranged in the machine body 1, is fixedly connected in the supporting plate 2, and the second water pump 13 pumps cooling water in the water tank 12 and conveys the cooling water to the square plate 4 through the second water pipe 14.

The square plate 4 is internally provided with the liquid inlet cavity 23, the second water pipe 14 is communicated with the liquid inlet cavity 23, the spray head 22 is provided with a plurality of spray heads, the contact area of cooling water and parts can be increased, and the cooling effect is better.

Organism 1's top inner wall fixedly connected with mounting bracket 18, air extractor 17 fixed connection is on mounting

bracket

18, 19 fixed connection of exhaust tube is at the inlet end of

air extractor

17, 21 fixed connection of outlet duct are at the end of giving vent to anger of air extractor 17, the one end fixedly connected with head of bleeding 20 of air extractor 17 is kept away from to exhaust tube 19, the one end that air extractor 17 was kept away from to outlet duct 21 runs through in 1 right side outer wall of organism and outwards extends, the steam that produces is extracted through exhaust tube 19, it is outdoor through the discharge of outlet duct 21, prevent that steam from burning the staff.

Place board 3 and be the slope and place, place the bottom fixedly connected with baffle 25 of board 3, seted up a plurality of round holes 26 on the baffle 25, baffle 25 can prevent that spare part from droing from placing board 3 when the cooling, and the water that has cooled down flows out through round hole 26.

The sliding groove 27 is formed in the machine body 1, the sealing door 28 is connected to the sliding groove 27 in a sliding mode, the observation window 29 is formed in the sealing door 28, the door handle 30 is fixedly mounted on the sealing door 28, the sealing door 28 is arranged, and damage to workers due to hot air generated when the parts are cooled is prevented.

The utility model discloses in, at first the staff puts the spare part that needs the cooling on placing board 3, then open stopcock 16, add the cooling water through water injection pipe 15 in water tank 12, then start second water pump 13, the cooling water in the extraction water tank 12 is carried in the feed liquor chamber 23 in square plate 4 through second water pipe 14, cool down the spare part on placing board 3 through shower nozzle 22, the water that has cooled down flows to hydrops groove 7 of case lid 6 through round hole 26 of baffle 25, flow into header tank 5 through inlet opening 24, filter 8 filters impurity such as piece in the water, then start refrigerator body 9 and refrigerate the water of retrieving, start first water pump 10 after the refrigeration is accomplished, extract the water of refreezing in header tank 5, carry in water tank 12 through first water pipe 11, realize the cyclic utilization of water, and save water resources; when the cooling water cools down the spare part, close sealing door 28, observe through observation window 29, prevent by the hot gas burn that the cooling produced, when the cooling produced a large amount of hot gas, start air extractor 17, through the hot gas of exhaust tube 19 extraction production, discharge outdoors through outlet duct 21.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. The cooling device for processing the aircraft parts comprises a machine body (1) and a refrigerator body (9), and is characterized in that a supporting plate (2) is fixedly connected in the machine body (1), a placing plate (3) is fixedly connected on the supporting plate (2), a square plate (4) is fixedly connected at the top of the supporting plate (2), a plurality of spray heads (22) are fixedly connected on the square plate (4), a liquid collecting tank (5) is fixedly connected at the bottom in the machine body (1), a tank cover (6) is connected on the liquid collecting tank (5), a first water pump (10) is fixedly connected in the liquid collecting tank (5), the refrigerator body (9) is fixedly connected in the liquid collecting tank (5), a first water pipe (11) is fixedly connected on the first water pump (10), a water tank (12) is fixedly connected at the left side of the machine body (1), the first water pipe (11) is arranged in the water tank (12), the water pump is characterized in that a second water pump (13) is fixedly connected in the water tank (12), a second water pipe (14) is fixedly connected on the second water pump (13), the second water pipe (14) is communicated with a spray head (22), an air extractor (17) is fixedly connected on the inner wall of the top of the machine body (1), and an air extracting pipe (19) and an air outlet pipe (21) are fixedly connected on the air extractor (17).

2. The cooling device for processing the aircraft parts according to claim 1, wherein the tank cover (6) is detachably connected to the liquid collecting tank (5), the liquid collecting tank (7) is formed on the top surface of the tank cover (6), the water inlet hole (24) is formed in the tank cover (6), and the liquid collecting tank (7) is communicated with the liquid collecting tank (5) through the water inlet hole (24).

3. The cooling device for processing the aircraft parts according to claim 2, wherein the filter plate (8) is fixedly connected in the liquid collecting tank (5), the water pumping end of the first water pump (10) is arranged in the liquid collecting tank (5), the first water pipe (11) is fixedly connected at the water outlet end of the first water pump (10), and the end of the first water pipe (11) far away from the liquid collecting tank (5) is fixedly connected in the water tank (12).

4. The cooling device for processing the aircraft parts according to claim 3, wherein a through hole (31) is formed in the outer wall of the left side of the machine body (1), the water tank (12) is fixedly connected to the through hole (31), a water injection pipe (15) is fixedly connected to the outer wall of the left side of the water tank (12), and a pipe plug (16) is arranged on the water injection pipe (15).

5. The cooling device for processing the aircraft parts according to claim 4, wherein the water pumping end of the second water pump (13) is arranged in the water tank (12), the second water pipe (14) is fixedly connected to the water outlet end of the second water pump (13), and one end of the second water pipe (14) arranged in the machine body (1) is fixedly connected to the support plate (2).

6. The cooling device for processing the aircraft component according to claim 5, wherein an inlet cavity (23) is formed in the square plate (4), the second water pipe (14) is communicated with the inlet cavity (23), and the spray head (22) is communicated with the inlet cavity (23).

7. The cooling device for processing the aircraft parts according to claim 1, wherein a mounting frame (18) is fixedly connected to the inner wall of the top of the machine body (1), the air extractor (17) is fixedly connected to the mounting frame (18), the air extraction pipe (19) is fixedly connected to the air inlet end of the air extractor (17), and the air outlet pipe (21) is fixedly connected to the air outlet end of the air extractor (17).

8. The cooling device for processing the aircraft parts according to claim 7, wherein an air exhaust head (20) is fixedly connected to one end of the air exhaust pipe (19) far away from the air exhaust machine (17), and one end of the air outlet pipe (21) far away from the air exhaust machine (17) penetrates through the outer wall of the right side of the machine body (1) and extends outwards.

9. The cooling device for processing the aircraft component according to claim 8, wherein the placing plate (3) is obliquely placed, a baffle plate (25) is fixedly connected to the bottom of the placing plate (3), and a plurality of round holes (26) are formed in the baffle plate (25).

10. The cooling device for processing the aircraft parts according to claim 1, wherein a sliding groove (27) is formed in the machine body (1), a sealing door (28) is connected to the sliding groove (27) in a sliding manner, an observation window (29) is formed in the sealing door (28), and a door handle (30) is fixedly mounted on the sealing door (28).