CN214950055U - Cooling device for machining of aircraft parts - Google Patents
Cooling device for machining of aircraft parts Download PDFInfo
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- CN214950055U CN214950055U CN202120479817.7U CN202120479817U CN214950055U CN 214950055 U CN214950055 U CN 214950055U CN 202120479817 U CN202120479817 U CN 202120479817U CN 214950055 U CN214950055 U CN 214950055U
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- cooling
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- pipeline
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Abstract
The utility model discloses a heat sink is used in aircraft parts processing belongs to parts machining technical field. The liquid outlet of the bottom of the shell is connected with a receiving box body below the shell through a pipeline, a liquid outlet pipeline on the receiving box body is connected with a pump body on the liquid outlet pipeline in a rotating mode, a filter plate on the inner wall of the receiving box body is arranged at a sewage outlet on the receiving box body, the electromagnet sucker on the sewage outlet is fixedly connected with a metal baffle on the receiving box body in a sliding mode, the metal baffle is connected with a storage box on the sewage outlet through a pipeline, and the storage box is fixedly connected with a cooling box on the receiving box body and wrapped on the liquid outlet pipeline. The utility model discloses a cooling box is cooled down the processing to the coolant liquid, makes shower nozzle subassembly spun coolant liquid can carry out quick cooling to spare part.
Description
Technical Field
The utility model relates to a parts machining technical field specifically is a heat sink is used in aircraft parts processing.
Background
The aircraft is in the manufacturing process, need carry out the processing to very many parts, however at the in-process that goes on to the spare part, need carry out the cooling treatment through the heat sink to the spare part of processing, at present, common heat sink adopts fan to lead to cold wind to cool down usually, or adopt the coolant liquid to cool down, but when adopting the coolant liquid to cool down, a large amount of coolant liquid of in-process waste at the cooling, if adopt the cyclic utilization coolant liquid, the coolant liquid is in cyclic utilization, because the coolant liquid is when carrying out the cooling treatment to the spare part, the temperature of coolant liquid has also improved, in cyclic utilization, unable fine refrigerated effect that reaches, lack in coolant liquid cyclic utilization, can mix with a lot of impurity in the coolant liquid, can cause the fish tail to the surface of spare part, and the coolant liquid shower nozzle easily blocks up.
SUMMERY OF THE UTILITY MODEL
The utility model discloses an it is not enough to exist among the prior art, provide a heat sink is used in aircraft parts processing, through to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a cooling device for processing aircraft parts comprises a shell, a through hole arranged on the shell, a spray head assembly fixedly connected in the shell, a liquid outlet arranged at the bottom of the shell, a receiving box body connected below the shell through a pipeline, a liquid outlet pipeline arranged on the receiving box body, a pump body connected on the liquid outlet pipeline, a filter plate rotationally connected on the inner wall of the receiving box body, a sewage outlet arranged on the receiving box body, an electromagnet sucker fixedly connected on the sewage outlet, a metal baffle plate slidably arranged on the receiving box body, a storage box connected on the sewage outlet through a pipeline, and a cooling box fixedly connected on the receiving box body and wrapping the liquid outlet pipeline; the other end of the liquid outlet pipeline is welded at the top of the shell, the other side of the filter plate is fixedly connected to the upper end of the metal baffle plate, the spray head assembly is communicated with the liquid outlet pipe, the electromagnet chuck is electrically connected with the pump body, cooling liquid is filtered through the filter plate, and filtered impurities are discharged through the sewage discharge port.
Preferably, the bottom surface of the shell is an inclined surface and is fixedly connected with the lowest surface of the edge of the liquid outlet.
Preferably, still including setting up first gravity sensor on the filter, first gravity sensor with electromagnet chuck electric connection, when impurity weight on the filter reached first gravity sensor setting value, first gravity sensor control electromagnet chuck's circular telegram condition was controlled, makes the impurity on the filter flow into in the storage case.
Preferably, the device further comprises electric push rods arranged in the material storage box, a moving plate fixedly connected to each electric push rod, a brush body arranged below the moving plate, an outlet arranged on the material storage box, and a second gravity sensor fixed at the bottom of the material storage box; and the second gravity sensor is connected with the electric push rod in a wiring way.
Preferably, the cooling box further comprises a cover body arranged on the cooling box, a visible window arranged on one side wall of the cooling box, and a thermometer adhered to the visible window, and the temperature condition in the cooling box is observed through the thermometer.
Preferably, the shower nozzle subassembly includes squirt, gondola water faucet and water smoke cooling shower nozzle, squirt, gondola water faucet and water smoke cooling shower nozzle respectively with go out the liquid pipe connection, through the shower nozzle of difference, effectually carry out quick cooling to spare part.
Has the advantages that: through setting up the impurity of filter in the box with the coolant liquid of accepting is carried out filtration treatment to collect impurity through the storage case, make the coolant liquid can obtain the use of cycle repetition, and cool down the processing through the cooling box to the coolant liquid, make shower nozzle subassembly spun coolant liquid can carry out quick cooling to cold parts.
Drawings
Fig. 1 is an internal schematic view of the present invention;
FIG. 2 is a schematic view of the overall structure of the present invention;
FIG. 3 is a schematic structural view of the present invention A;
FIG. 4 is a schematic view of the internal structure of the storage box of the present invention;
fig. 5 is an enlarged view of the present invention B.
In the figure: the device comprises a shell 1, a receiving box 2, a material storage box 3, a cooling box 4, a liquid outlet pipeline 7, a spray head assembly 8, a through hole 101, a filter plate 201, a first gravity sensor 202, an electromagnet sucker 203, a metal baffle 204, an electric push rod 303, a brush body 302, a moving plate 301, a second gravity sensor 304, a thermometer 401, a water gun 102, a shower head 103 and a water mist cooling spray head 104.
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.
In practical applications, the applicant has found that: in the production and manufacturing process of an airplane, a great number of parts need to be processed, however, in the process of processing the parts, the processed parts need to be cooled through a cooling device, at present, a common cooling device generally adopts a fan to blow cold air for cooling or adopts cooling liquid for cooling, but when cooling is carried out by adopting the cooling liquid, a great amount of cooling liquid is wasted in the cooling process, if the cooling liquid is recycled, the temperature of the cooling liquid is also increased when the cooling liquid is used for cooling the parts, in the recycling process, the cooling effect cannot be well achieved, but in the recycling process of the cooling liquid, a great number of impurities can be mixed in the cooling liquid, the outer surface of the parts can be scratched, and a cooling liquid nozzle is easy to be blocked, aiming at the problems, the cooling device for processing the parts of the airplane is invented, the problems can be effectively solved.
Referring to fig. 1, the present invention provides a technical solution: a cooling device for processing aircraft parts comprises a shell 1, a receiving box 2, a material storage box 3, a cooling box 4, a liquid outlet pipeline 7, a spray head assembly 8, a through hole 101, a filter plate 201, a first gravity sensor 202, an electromagnet sucker 203, a baffle 204, an electric push rod 303, a brush body 302, a movable plate 301, a second gravity sensor 304, a thermometer 401, a water gun 102, a shower head 103 and a water mist cooling spray head 104, wherein the shell 1 is provided with the through hole 101, the spray head assembly 8 is fixedly connected in the shell 1, the spray head assembly 8 comprises the water gun 102, the shower head 103 and the water mist cooling spray head 104, the water gun 102, the shower head 103 and the water mist cooling spray head 104 are respectively connected with the liquid outlet pipeline 7, the parts are effectively and rapidly cooled through different spray heads, a liquid outlet is arranged at the bottom of the shell 1, the bottom surface of the shell 1 is an inclined surface and is fixedly connected with the lowest surface at the edge of the liquid outlet, the device is characterized in that the device is connected with a bearing box 2 body below a shell 1 through a pipeline, a liquid outlet pipeline 7 is arranged on the bearing box 2 body, a pump body is connected onto the liquid outlet pipeline 7, a filter plate 201 is rotatably connected onto the inner wall of the bearing box 2 body, a first gravity sensor 202 is arranged on the filter plate 201, the first gravity sensor 202 is electrically connected with an electromagnet sucker 203, when the weight of impurities on the filter plate 201 reaches the set value of the first gravity sensor 202, the first gravity sensor 202 controls the electrifying condition of the electromagnet sucker 203 to control so that the impurities on the filter plate 201 flow into a storage box 3, a sewage discharge outlet is arranged on the bearing box 2 body, the electromagnet sucker 203 is fixedly connected onto the sewage discharge outlet, a metal baffle 204 is arranged on the bearing box 2 body in a sliding manner, the filter plate 201 is fixedly connected onto the metal baffle 204, the storage box 3 is connected onto the sewage discharge outlet through a pipeline, the cooling box 4 is fixedly connected to the receiving box 2, the cooling box 4 wraps the liquid outlet pipe 7, the cooling box 4 further comprises a cover body arranged on the cooling box 4, a visible window is arranged on one side wall of the cooling box 4, a thermometer 401 is bonded to the visible window, the temperature condition in the cooling box 4 is observed through the thermometer 401, the other end of the liquid outlet pipe 7 is welded to the top of the shell 1, the other side of the filter plate 201 is fixedly connected to the upper end of the metal baffle plate 204, the sprayer assembly 8 is communicated with the liquid outlet pipe, the electromagnet sucker 203 is electrically connected with the pump body, the filter plate 201 is used for filtering cooling liquid, filtered impurities are discharged to the material storage box 3 through a sewage discharge port, an electric push rod 303 is arranged in the material storage box 3, and the electromagnet sucker is fixedly connected to each electric push rod 303 moving plate 301, a brush 302 arranged below the moving plate 301, an outlet arranged on the storage tank 3, and a second gravity sensor 304 fixed at the bottom of the storage tank 3; the second gravity sensor 304 is connected with the electric push rod 303 in a wiring manner, the electric push rod 303 is controlled to be electrified through the second gravity sensor 304, the moving plate 301 is driven to move in the material storage box 3, and impurities in the material storage box 3 are moved to an outlet through the brush 302 and are discharged.
Description of the working principle:
the parts enter the shell 1 through the through hole 101, the parts are cooled by the cooling liquid sprayed by the spray head assembly 8, the sprayed cooling liquid flows into the receiving box 2 through the liquid outlet at the bottom of the shell 1, the cooling liquid is filtered by the filter plate 201, the filtered cooling liquid flows into the bottom of the receiving box 2, the cooling liquid is cooled by the cooling box 4 arranged at the bottom of the receiving box 2 and is conveyed to the spray head assembly 8 through the pump body, when the impurities on the filter plate 201 reach the preset value of the first gravity sensor 202, the electromagnet sucker 203 is powered off, the metal baffle plate 204 drives the filter plate 201 to rotate, so that the filter plate 201 is inclined in the receiving box 2, the filter plate 201 is washed by the cooling liquid, the impurities on the filter plate 201 are driven to move into the drain outlet to the storage box 3, when the impurities in the storage box 3 reach the preset value of the second gravity sensor 304, the electric push rod 303 drives the moving plate 301 to move, and the brush 302 below the moving plate 301 moves the impurities to the outlet of the storage box 3 for discharging.
It should be noted that the various features described in the above embodiments may be combined in any suitable manner without departing from the scope of the invention. In order to avoid unnecessary repetition, the present invention does not separately describe various possible combinations.
Claims (6)
1. A cooling device for processing aircraft parts is characterized by comprising a shell with an inlet and an outlet, a spray head assembly penetrating through the top of the shell and arranged in the shell, a receiving box body connected below the shell through a pipeline, a liquid outlet pipeline arranged on the receiving box body, a pump body connected on the liquid outlet pipeline, a filter plate rotationally connected on the inner wall of the receiving box body, a sewage discharge outlet arranged on the receiving box body, an electromagnet sucker fixedly connected on the sewage discharge outlet, a metal baffle plate slidably arranged on the receiving box body, a storage box connected on the sewage discharge outlet through a pipeline, and a cooling box fixedly connected on the receiving box body and wrapping the liquid outlet pipeline; the shell is communicated with the bearing box body through a pipeline, the other end of the liquid outlet pipeline is welded at the top of the shell, the other side of the filter plate is fixedly connected to the upper end of the metal baffle plate, the spray head assembly is communicated with the liquid outlet pipe, and the electromagnet sucker is electrically connected with the pump body.
2. The cooling device for processing the aircraft parts as claimed in claim 1, wherein: the casing bottom surface is the inclined plane, the casing bottom sets up the liquid outlet, and fixed connection be in the lowest on liquid outlet border.
3. The cooling device for processing the aircraft parts as claimed in claim 1, wherein: still including setting up first gravity sensor on the filter, first gravity sensor with electromagnet sucking disc electric connection.
4. The cooling device for processing the aircraft parts as claimed in claim 1, wherein: the device also comprises electric push rods arranged in the material storage box, a moving plate fixedly connected to each electric push rod, a brush body arranged below the moving plate, and a second gravity sensor fixed at the bottom of the material storage box; and the second gravity sensor is connected with the electric push rod in a wiring way.
5. The cooling device for processing the aircraft parts as claimed in claim 1, wherein: the cooling box further comprises a cover body arranged on the cooling box, a visible window arranged on one side wall of the cooling box, and a thermometer adhered to the visible window.
6. The cooling device for processing the aircraft parts as claimed in claim 1, wherein the nozzle assembly comprises a water gun, a shower head and a water mist cooling nozzle, and the water gun, the shower head and the water mist cooling nozzle are respectively connected with the liquid outlet pipeline.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120479817.7U CN214950055U (en) | 2021-03-05 | 2021-03-05 | Cooling device for machining of aircraft parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120479817.7U CN214950055U (en) | 2021-03-05 | 2021-03-05 | Cooling device for machining of aircraft parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214950055U true CN214950055U (en) | 2021-11-30 |
Family
ID=79118210
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120479817.7U Active CN214950055U (en) | 2021-03-05 | 2021-03-05 | Cooling device for machining of aircraft parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214950055U (en) |
-
2021
- 2021-03-05 CN CN202120479817.7U patent/CN214950055U/en active Active
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