CN214393508U - Smoothness processing device for aerospace shell - Google Patents
Smoothness processing device for aerospace shell Download PDFInfo
- Publication number
- CN214393508U CN214393508U CN202120148614.XU CN202120148614U CN214393508U CN 214393508 U CN214393508 U CN 214393508U CN 202120148614 U CN202120148614 U CN 202120148614U CN 214393508 U CN214393508 U CN 214393508U
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- CN
- China
- Prior art keywords
- pool
- polishing
- cleaning
- motor
- pipe
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 238000005498 polishing Methods 0.000 claims abstract description 60
- 238000004140 cleaning Methods 0.000 claims description 39
- 238000005192 partition Methods 0.000 claims description 13
- 238000003756 stirring Methods 0.000 claims description 12
- 238000003860 storage Methods 0.000 claims description 6
- 238000000034 method Methods 0.000 claims description 5
- 238000001035 drying Methods 0.000 claims description 4
- 238000005406 washing Methods 0.000 claims description 3
- 239000000725 suspension Substances 0.000 description 6
- 239000007788 liquid Substances 0.000 description 4
- 238000003754 machining Methods 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 238000007726 management method Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000036651 mood Effects 0.000 description 1
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- Cleaning By Liquid Or Steam (AREA)
Abstract
The utility model discloses a smoothness processing apparatus for aerospace casing, including first pillar, crossbeam, second pillar, first pillar top is provided with the crossbeam, the crossbeam bottom with first pillar one side is provided with the second pillar, the crossbeam bottom is provided with electric block, the electric block bottom is provided with the supporter, the supporter below is provided with first polishing pond, first polishing pond is preceding to be provided with first drain pipe, first polishing pond one side is provided with the second polishing pond, the second polishing pond is preceding to be provided with the second fluid-discharge tube, first polishing pond with be provided with the ultrasonic generator in the second polishing pond, still include the wiper mechanism that can wash and weather the aerospace casing. Has the advantages that: the utility model discloses be provided with wiper mechanism, can wash and weather after space flight casing polishing treatment to be convenient for workman's transportation or equipment purify operational environment.
Description
Technical Field
The utility model relates to an aerospace production technical field especially relates to a smoothness processing apparatus for aerospace casing.
Background
At present, many people like aeromodelling, the types of aeromodelling are many, and some aeromodelling have the function of flying although the size is small. In order to improve the flight capability of the model airplane, the processing precision of the model airplane is higher and higher, and the existing model airplane shell is not cleaned after being polished, so that the working environment is easily polluted during transportation, and the working mood of workers is influenced.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is just to provide a smoothness processing apparatus for aerospace casing in order to solve above-mentioned problem.
The utility model discloses a following technical scheme realizes above-mentioned purpose: a smoothness processing device for an aerospace shell comprises a first supporting column, a cross beam and a second supporting column, the top of the first support is provided with the beam, the bottom of the beam and one side of the first support are provided with the second support, the bottom of the beam is provided with an electric hoist, the input end of the electric hoist is electrically connected with the output end of a city department, a storage rack is arranged at the bottom of the electric hoist, a first polishing pool is arranged below the storage rack, a first liquid discharge pipe is arranged in front of the first polishing pool, a second polishing pool is arranged on one side of the first polishing pool, the front of the second polishing pool is provided with a second liquid discharge pipe, the first polishing pool and the second polishing pool are internally provided with an ultrasonic generator, the cleaning device can be used for washing and drying the aerospace shell, and the cleaning device is arranged on one side of the second polishing pool.
Preferably, wiper mechanism is including wasing pond, C type tuber pipe, nozzle, motor, pivot, straight type puddler, it sets up to wash the pond second polishing pond one side, it is provided with to wash the pond top C type tuber pipe, C type tuber pipe inside is provided with the nozzle, C type tuber pipe one side is provided with the gas-supply pipe, the gas-supply pipe bottom is provided with the air compressor machine, it is provided with the baffle to wash the pond inside, the baffle bottom is provided with the motor, the motor input links to each other with municipality output electrical property, the motor output is provided with the pivot, the pivot radially is provided with straight type puddler, wash the preceding drain pipe that is provided with in pond, the baffle welding is in wasing the pond, the motor passes through the bolt fastening and is in on the baffle.
Preferably, wiper mechanism is including wasing pond, C type tuber pipe, nozzle, motor, pivot, carousel, oblique type puddler, it sets up to wash the pond second polishing pond one side, it is provided with to wash the pond top C type tuber pipe, C type tuber pipe inside is provided with the nozzle, C type tuber pipe one side is provided with the gas-supply pipe, the gas-supply pipe bottom is provided with the air compressor machine, it is provided with the baffle to wash pond inside, the baffle bottom is provided with the motor, the motor input links to each other with city office output electrical property, the motor output is provided with the pivot, the pivot top is provided with the carousel, the carousel top is provided with oblique type puddler, wash the preceding drain pipe that is provided with in pond, the baffle welding is in wash the pond, the motor passes through the bolt fastening and is in on the baffle.
Preferably, the cross beam is fixed to the first support and the second support by bolts.
Preferably, the ultrasonic generator is fixed to the first polishing pool and the second polishing pool by bolts.
Has the advantages that: the utility model discloses be provided with wiper mechanism, can wash and weather after space flight casing polishing treatment to be convenient for workman's transportation or equipment purify operational environment.
Drawings
Fig. 1 is a structural view of a smoothness processing apparatus for an aerospace housing according to the present invention;
figure 2 is a cross-sectional view of an embodiment 1 of a smoothness processing apparatus for an aerospace housing in accordance with the present invention;
figure 3 is a partial top view of an embodiment 1 of a smoothness processing apparatus for an aerospace housing in accordance with the present invention;
figure 4 is a cross-sectional view of an embodiment 2 of a smoothness processing apparatus for an aerospace housing in accordance with the present invention;
figure 5 is a partial top view of embodiment 2 of a smoothness management apparatus for an aerospace housing according to the present invention.
Reference numerals: 1. a first support; 2. a cross beam; 3. a second support; 4. a cleaning mechanism; 401. a cleaning tank; 402. a C-shaped air pipe; 403. a nozzle; 404. a gas delivery pipe; 405. an air compressor; 406. a partition plate; 407. a motor; 408. a rotating shaft; 409. a straight type stirring rod; 410. a drain pipe; 411. a turntable; 412. an inclined stirring rod; 5. a first polishing pool; 6. a first drain pipe; 7. a second polishing pool; 8. a second drain pipe; 9. an electric hoist; 10. an ultrasonic generator; 11. a shelf.
Detailed Description
The present invention will be further explained with reference to the accompanying drawings:
a smoothness processing device for an aerospace shell comprises a first supporting column 1, a cross beam 2, the device comprises a second support column 3, a cross beam 2 is arranged at the top of the first support column 1, a second support column 3 is arranged at the bottom of the cross beam 2 and on one side of the first support column 1, an electric hoist 9 is arranged at the bottom of the cross beam 2, the input end of the electric hoist 9 is electrically connected with the output end of a city department, a storage rack 11 is arranged at the bottom of the electric hoist 9, a first polishing pool 5 is arranged below the storage rack 11, a first drainage pipe 6 is arranged in front of the first polishing pool 5, a second polishing pool 7 is arranged on one side of the first polishing pool 5, a second drainage pipe 8 is arranged in front of the second polishing pool 7, ultrasonic generators 10 are arranged in the first polishing pool 5 and the second polishing pool 7, the device further comprises a cleaning mechanism 4 capable of washing and drying the aerospace shell, and the cleaning mechanism 4 is arranged on one side of the second polishing pool 7.
Example 1
As shown in fig. 1, 2, and 3, the cleaning mechanism 4 includes a cleaning tank 401, a C-shaped air pipe 402, a nozzle 403, a motor 407, a rotating shaft 408, and a straight stirring rod 409, the cleaning tank 401 is disposed on one side of the second polishing tank 7, the C-shaped air pipe 402 is disposed on the top of the cleaning tank 401, the nozzle 403 is disposed inside the C-shaped air pipe 402, an air pipe 404 is disposed on one side of the C-shaped air pipe 402, an air compressor 405 is disposed at the bottom of the air pipe 404, a partition 406 is disposed inside the cleaning tank 401, the motor 407 is disposed at the bottom of the partition 406, an input end of the motor 407 is electrically connected to an output end of a city department, the rotating shaft 408 is disposed at an output end of the motor 407, the straight stirring rod 409 is radially disposed on the rotating shaft 408, a drain pipe 410 is disposed in front of the cleaning tank 401, the partition 406 is welded in the cleaning tank 401, and the motor 407 is fixed on the partition 406 by bolts; the cross beam 2 is fixed on the first support column 1 and the second support column 3 through bolts; the ultrasonic generator 10 is fixed on the first polishing pool 5 and the second polishing pool 7 through bolts.
The working principle and the using flow of the embodiment are as follows: when the device is used, different abrasive suspensions are injected into the first polishing pool 5 and the second polishing pool 7, a certain cleaning solution is injected into the cleaning pool 401, then the model airplane shell is placed on the article placing frame 11, then the electric hoist 9 is regulated and controlled to enable the article placing frame 11 to be immersed into the first polishing pool 5, then the ultrasonic generator 10 drives the abrasive suspension in the first polishing pool 5 to carry out rough machining on the model airplane shell, then the article placing frame 11 is lifted by the electric hoist 9 to move to the position above the second polishing pool 7, then the article placing frame 11 is immersed into the second polishing pool 7, the ultrasonic generator 10 drives the abrasive suspension in the second polishing pool 7 to carry out finish machining on the shell, then the article placing frame 11 is lifted by the electric hoist 9 to move to the position above the cleaning pool 401, the article placing frame 11 is placed in the cleaning pool 401, the motor 407 drives the rotating shaft 408 and the straight stirring rod 409 to rotate, so that the cleaning solution is opposite to the model airplane shell in the article placing frame 11 to be cleaned, the shelf 11 is lifted by the electric hoist 9, compressed air is conveyed to the C-shaped air pipe 402 by the air compressor 405 through the air conveying pipe 404 and is sprayed out from the nozzle 403 to blow the model airplane shell in the shelf 11 for drying, so that the transportation and the assembly of workers are facilitated.
Example 2
As shown in fig. 1, 4 and 5, the difference between the embodiment 2 and the embodiment 1 is that the straight stirring rod 409 is replaced by a rotary table 411 and an inclined stirring rod 412, when in use, different abrasive suspensions are injected into the first polishing pool 5 and the second polishing pool 7, a certain cleaning liquid is injected into the cleaning pool 401, then the model shell is placed on the rack 11, then the electric hoist 9 is regulated and controlled to immerse the rack 11 into the first polishing pool 5, then the abrasive suspension in the first polishing pool 5 is driven by the ultrasonic generator 10 to roughly machine the model shell, then the rack 11 is lifted by the electric hoist 9 to move above the second polishing pool 7, then the rack 11 is immersed into the second polishing pool 7, the abrasive suspension in the second polishing pool 7 is driven by the ultrasonic generator 10 to finely machine the shell, then the rack 11 is lifted by the electric hoist 9 to move above the cleaning pool 401, the shelf 11 is placed in the cleaning pool 401, the motor 407 drives the rotating shaft 408, the rotating disc 411 and the inclined stirring rod 412 to rotate, so that the cleaning liquid washes the model airplane shell in the shelf 11, the shelf 11 is lifted by the electric hoist 9, the compressed air is conveyed to the C-shaped air pipe 402 by the air compressor 405 through the air conveying pipe 404 and is sprayed out from the nozzle 403 to blow the model airplane shell in the shelf 11, and the transportation and the assembly of workers are facilitated.
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.
The foregoing illustrates and describes the principles, general features, and advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (5)
1. A smoothness processing device for an aerospace shell comprises a first support column (1), a cross beam (2) and a second support column (3), wherein the cross beam (2) is arranged at the top of the first support column (1), the second support column (3) is arranged at one side of the bottom of the cross beam (2) and the first support column (1), an electric hoist (9) is arranged at the bottom of the cross beam (2), a storage rack (11) is arranged at the bottom of the electric hoist (9), a first polishing pool (5) is arranged below the storage rack (11), a first drainage pipe (6) is arranged in front of the first polishing pool (5), a second polishing pool (7) is arranged at one side of the first polishing pool (5), a second drainage pipe (8) is arranged in front of the second polishing pool (7), and an ultrasonic wave generator (10) is arranged in the first polishing pool (5) and the second polishing pool (7), the method is characterized in that: the cleaning mechanism (4) capable of washing and drying the aerospace shell is further included, and the cleaning mechanism (4) is arranged on one side of the second polishing pool (7).
2. A smoothness processing apparatus for an aerospace housing according to claim 1, wherein: the cleaning mechanism (4) comprises a cleaning pool (401), a C-shaped air pipe (402), a nozzle (403), a motor (407), a rotating shaft (408) and a straight stirring rod (409), wherein the cleaning pool (401) is arranged on one side of the second polishing pool (7), the C-shaped air pipe (402) is arranged at the top of the cleaning pool (401), the nozzle (403) is arranged in the C-shaped air pipe (402), an air conveying pipe (404) is arranged on one side of the C-shaped air pipe (402), an air compressor (405) is arranged at the bottom of the air conveying pipe (404), a partition plate (406) is arranged in the cleaning pool (401), the motor (407) is arranged at the bottom of the partition plate (406), the rotating shaft (408) is arranged at the output end of the motor (407), the straight stirring rod (409) is radially arranged in the rotating shaft (408), a drain pipe (410) is arranged in front of the cleaning pool (401), the partition plate (406) is welded in the cleaning tank (401), and the motor (407) is fixed on the partition plate (406) through bolts.
3. A smoothness processing apparatus for an aerospace housing according to claim 1, wherein: the cleaning mechanism (4) comprises a cleaning pool (401), a C-shaped air pipe (402), a nozzle (403), a motor (407), a rotating shaft (408), a turntable (411) and an inclined stirring rod (412), the cleaning pool (401) is arranged on one side of the second polishing pool (7), the C-shaped air pipe (402) is arranged at the top of the cleaning pool (401), the nozzle (403) is arranged inside the C-shaped air pipe (402), an air pipe (404) is arranged on one side of the C-shaped air pipe (402), an air compressor (405) is arranged at the bottom of the air pipe (404), a partition plate (406) is arranged inside the cleaning pool (401), the motor (407) is arranged at the bottom of the partition plate (406), the rotating shaft (408) is arranged at the output end of the motor (407), the turntable (411) is arranged at the top of the rotating shaft (408), the inclined stirring rod (412) is arranged at the top of the turntable (411), a drain pipe (410) is arranged in front of the cleaning pool (401), the partition plate (406) is welded in the cleaning pool (401), and the motor (407) is fixed on the partition plate (406) through bolts.
4. A smoothness processing apparatus for an aerospace housing according to claim 1, wherein: the cross beam (2) is fixed on the first support column (1) and the second support column (3) through bolts.
5. A smoothness processing apparatus for an aerospace housing according to claim 1, wherein: the ultrasonic generator (10) is fixed on the first polishing pool (5) and the second polishing pool (7) through bolts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120148614.XU CN214393508U (en) | 2021-01-20 | 2021-01-20 | Smoothness processing device for aerospace shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120148614.XU CN214393508U (en) | 2021-01-20 | 2021-01-20 | Smoothness processing device for aerospace shell |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214393508U true CN214393508U (en) | 2021-10-15 |
Family
ID=78046510
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120148614.XU Expired - Fee Related CN214393508U (en) | 2021-01-20 | 2021-01-20 | Smoothness processing device for aerospace shell |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214393508U (en) |
-
2021
- 2021-01-20 CN CN202120148614.XU patent/CN214393508U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211015 |