CN218162577U - Aerospace is with automatic fog camera device that removes dust - Google Patents
Aerospace is with automatic fog camera device that removes dust Download PDFInfo
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- CN218162577U CN218162577U CN202221606583.9U CN202221606583U CN218162577U CN 218162577 U CN218162577 U CN 218162577U CN 202221606583 U CN202221606583 U CN 202221606583U CN 218162577 U CN218162577 U CN 218162577U
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Abstract
The utility model discloses an aerospace is with automatic fog camera device that removes dust, including casing, dust removal fog mechanism, glass cover fixed mounting is in the casing top, dust removal fog mechanism top sets up in glass cover top, dust removal fog mechanism bottom sets up inside the casing, dust removal fog mechanism comprises fixed block, motor, first spliced pole, second spliced pole, brush board, lens wiper, weeping mouth, water pump, through-hole, water pipe, detector, water tank, fixed block fixed mounting is positive in shells inner wall. This aerospace is with automatic dust and fog camera device that removes passes through the motor and drives brush board and lens wiper and remove on glass cover surface, can clear up dust and fog that glass cover surface is stained with, makes the effect of making a video recording of camera resume as before. This aerospace is with automatic dust and fog camera device that removes passes through the water pump and spouts the washing liquid in the water tank from the weeping mouth, and rethread lens wiper cleans, can clear away the difficult spot of cleaing away in glass cover surface.
Description
Technical Field
The utility model relates to an aerospace technical field specifically is an aerospace is with automatic fog camera device that removes dust.
Background
With the progress of science and technology, the aerospace technology is developed more and more, and both the aerospace technology for mysterious exploration of the space and the aerospace technology for facilitating the travel of people add a great deal to the life of people. However, aerospace requires the recording of a camera, the recording of the curiosity of the earth from the universe, and aviation also requires the recording of a beautiful view looking down at the river and the earth.
However, the camera is installed outside the spacecraft, and dust and moisture in the air are very easily attached to the lens of the camera when the spacecraft flies quickly, so that the shooting effect of the camera is greatly reduced, and the spacecraft is cleaned up by manpower, which wastes a lot of time and manpower.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aerospace is with automatic fog camera device that removes dust to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides an aerospace is with automatic fog camera device that removes dust, includes casing, dust removal fog mechanism, glass cover fixed mounting is in the casing top, dust removal fog mechanism top sets up in the glass cover top, dust removal fog mechanism bottom sets up inside the casing, casing top outside fixed mounting has the sunshading board, glass cover top both sides fixed mounting has the baffle, the inside fixed mounting of casing has the closing plate, closing plate top fixed mounting has the supporting shoe, supporting shoe top fixed mounting has the camera.
Dust removal fog mechanism comprises fixed block, motor, first spliced pole, second spliced pole, brush board, lens wiper, weeping mouth, water pump, through-hole, water pipe, detector, water tank, fixed block fixed mounting is openly at shells inner wall, motor fixed mounting is at the fixed block top, first spliced pole fixed mounting is at the motor back, second spliced pole fixed mounting is at the first spliced pole top back, brush board fixed mounting is at the second spliced pole back, lens wiper fixed mounting is in the brush board bottom, the weeping mouth is seted up inside the brush board, water pump fixed mounting is in the fixed block left side, the through-hole is seted up inside first spliced pole, second spliced pole, water pipe fixed mounting is in the water pump left side, detector fixed mounting is in the closing plate top, water tank fixed mounting is in the casing bottom.
Preferably, the camera is installed in the shell, the glass cover and the sealing plate surround the camera to form a sealing space, and a sealing gasket is fixedly installed at the joint of the sealing plate and the glass cover.
Preferably, the front and back faces of the sun visor are arc-shaped, and the left and right sides of the sun visor are rectangular, and the sun visor annularly surrounds the glass cover.
Preferably, the brush plate is arranged at the top of the glass cover, the brush plate is positioned between the left end baffle and the right end baffle, and the lens wiping cloth is slidably arranged at the top of the glass cover.
Preferably, the brush board internally mounted has the water pipe, the water pipe passes through the through-hole in first spliced pole, the second spliced pole and links to each other with the weeping mouth through the brush board.
Preferably, the water tank is fixedly arranged at the bottom of the shell and is connected with the water pump through a water pipe.
Preferably, the fixed block, the motor and the water pump are located on the outer side of the front face of the sealing plate and are not connected with the sealing plate.
Compared with the prior art, the beneficial effects of the utility model are that:
1. this aerospace is with automatic dust and fog camera device that removes passes through the motor and drives brush board and lens wiper and remove on glass cover surface, can clear up dust and fog that glass cover surface is stained with, makes the effect of making a video recording of camera resume as before.
2. This aerospace is with automatic dust and fog camera device that removes passes through the washing liquid blowout from the weeping mouth in the water tank of water pump, and rethread lens wiper cleans, can clear away the difficult spot of cleaing away in glass cover surface.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of a brush plate structure;
FIG. 3 is a schematic view of a motor installation;
fig. 4 is a partially enlarged view of a portion a in fig. 1.
In the figure: 1. a housing; 2. a dust and mist removing mechanism; 201. a fixed block; 202. a motor; 203. a first connecting column; 204. a second connecting column; 205. brushing a plate; 206. lens wiping cloth; 207. a liquid leakage port; 208. a water pump; 209. a through hole; 210. a water pipe; 211. a detector; 212. a water tank; 3. a sun visor; 4. a glass cover; 5. a baffle plate; 6. a sealing plate; 7. a support block; 8. a camera is provided.
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. 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.
Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides an aerospace is with automatic fog camera device that removes dust, including casing 1, dust removal fog mechanism 2, glass cover 4 fixed mounting is at casing 1 top, the front of sunshading board 3 and the shape on the back are the arc, the shape on sunshading board 3 left side and right side are the rectangle, sunshading board 3 annular surrounds glass cover 4, can cover the sunshine of direct projection for camera 8 through sunshading board 3 and make the effect of camera 8 make a video recording better, dust removal fog mechanism 2 tops set up in glass cover 4 tops, dust removal fog mechanism 2 bottoms set up inside casing 1, casing 1 top outside fixed mounting has sunshading board 3, glass cover 4 top both sides fixed mounting has baffle 5, can prevent through baffle 5 that brush board 205 from shifting out glass cover 4 surface, casing 1 inside fixed mounting has the sealing pad 6, sealing pad 6 top fixed mounting has supporting shoe 7, supporting shoe 7 top fixed mounting has camera 8, camera 8 is installed inside casing 1, glass cover 4 and sealing pad 6 surround camera 8 and form a confined space, sealing pad 6 fixed mounting has the sealed pad in glass cover 4 junction, can prevent dust in the air and the camera 8 surface that water smoke from getting into through sealing pad 6.
The dust and fog removing mechanism 2 comprises a fixed block 201, a motor 202, a first connecting column 203, a second connecting column 204, a brush plate 205, a lens wiper 206, a liquid leakage opening 207, a water pump 208, a through hole 209, a water pipe 210, a detector 211 and a water tank 212, wherein the fixed block 201 is fixedly arranged on the front surface of the inner wall of the shell 1, the motor 202 is fixedly arranged at the top of the fixed block 201, the first connecting column 203 is fixedly arranged on the back surface of the motor 202, the second connecting column 204 is fixedly arranged on the back surface of the top of the first connecting column 203, the brush plate 205 is fixedly arranged on the back surface of the second connecting column 204, the first connecting column 203 and the second connecting column 204 are driven to rotate by starting the motor 202, the lens wiper 206 is fixedly arranged at the bottom of the brush plate 205, dust on the surface of the glass cover 4 and the mist brush plate 205 are removed by the friction between the lens wiper 206 and the surface of the glass cover 4 and are arranged at the top of the glass cover 4, the brush plate 205 is positioned between a left baffle 5 and a right baffle 5, the lens wiper 206 is slidably arranged at the top of the glass cover 4, the liquid leakage port 207 is arranged inside the brush plate 205, the water pump 208 is fixedly arranged at the left side of the fixed block 201, the motor 202 and the water pump 208 are positioned at the outer side of the front surface of the sealing plate 6 and are not connected with the sealing plate 6, the through hole 209 is arranged inside the first connecting column 203 and the second connecting column 204, the water pipe 210 is fixedly arranged at the left side of the water pump 208, the water pipe 210 is arranged inside the brush plate 205, the water pipe 210 penetrates through the through hole 209 in the first connecting column 203 and the second connecting column 204 and is connected with the liquid leakage port 207 through the brush plate 205, the detector 211 is fixedly arranged at the top of the sealing plate 6, the water tank 212 is fixedly arranged at the bottom of the shell 1, the water tank 212 is connected with the water pump 208 through the water pipe 210, the cleaning agent is filled in the water tank 212, the cleaning agent is sucked by starting the water pump 208 and is sprayed out from the liquid leakage port 207 through the water pipe 210, the cleaning liquid cleans the surface of the glass cover 4 together with the lens wiper 206.
The working principle is as follows: when dust or water mist is adhered to the surface of the glass cover 4 of the automatic dust and mist removing camera device for aerospace, a detector 211 transmits a signal to a controller when detecting that the definition of the glass cover 4 does not reach a standard line, a starting motor 202 drives a first connecting column 203 and a second connecting column 204 to rotate, and drives a lens wiper 206 at the bottom of a brush plate 205 to move on the surface of the glass cover 4 and remove the dust or the water mist on the surface of the glass cover 4, if the surface of the glass cover 4 is still stained, a water pump 208 is started to suck cleaning liquid in a water tank 212, the cleaning liquid passes through a water pipe 210 and is sprayed out from a liquid leakage opening 207, the cleaning liquid and the lens wiper 206 clean the surface of the glass cover 4 together, and when the detector 211 detects that the definition of the surface of the glass cover 4 reaches the standard line, the brush plate 205 moves to the left end of the glass cover 4 and closes the motor 202 and the water pump 208.
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 (7)
1. The utility model provides an aerospace is with automatic fog camera device that removes dust, includes casing (1), dust removal fog mechanism (2), glass cover (4), its characterized in that: the glass cover (4) is fixedly arranged at the top of the shell (1), the top of the dust and fog removing mechanism (2) is arranged at the top of the glass cover (4), the bottom of the dust and fog removing mechanism (2) is arranged inside the shell (1), a sun shield (3) is fixedly arranged on the outer side of the top of the shell (1), baffles (5) are fixedly arranged on two sides of the top of the glass cover (4), a sealing plate (6) is fixedly arranged inside the shell (1), a supporting block (7) is fixedly arranged at the top of the sealing plate (6), and a camera (8) is fixedly arranged at the top of the supporting block (7);
the dust and mist removing mechanism (2) consists of a fixed block (201), a motor (202), a first connecting column (203), a second connecting column (204), a brush plate (205), a lens wiping cloth (206), a liquid leakage opening (207), a water pump (208), a through hole (209), a water pipe (210), a detector (211) and a water tank (212), the fixed block (201) is fixedly arranged on the front surface of the inner wall of the shell (1), the motor (202) is fixedly arranged at the top of the fixed block (201), the first connecting column (203) is fixedly arranged on the back of the motor (202), the second connecting column (204) is fixedly arranged on the back of the top of the first connecting column (203), the brush plate (205) is fixedly arranged on the back of the second connecting column (204), the lens wiper (206) is fixedly arranged at the bottom of the brush plate (205), the liquid leakage port (207) is arranged in the brush plate (205), the water pump (208) is fixedly arranged at the left side of the fixed block (201), the through hole (209) is arranged in the first connecting column (203) and the second connecting column (204), the water pipe (210) is fixedly arranged at the left side of the water pump (208), the detector (211) is fixedly arranged at the top of the sealing plate (6), the water tank (212) is fixedly arranged at the bottom of the shell (1).
2. The automatic dust and fog removing and camera shooting device for the aerospace use according to claim 1, wherein: the camera (8) is arranged inside the shell (1), the glass cover (4) and the sealing plate (6) surround the camera (8) to form a sealing space, and the sealing plate (6) is fixedly provided with a sealing gasket at the joint of the glass cover (4).
3. The automatic dust and fog removing and camera shooting device for aerospace use according to claim 1, wherein: the front and the back of the sun shield (3) are arc-shaped, the left and the right sides of the sun shield (3) are rectangular, and the sun shield (3) annularly surrounds the glass cover (4).
4. The automatic dust and fog removing and camera shooting device for the aerospace use according to claim 1, wherein: the brush plate (205) is arranged at the top of the glass cover (4), the brush plate (205) is positioned between the baffles (5) at the left end and the right end, and the lens wiping cloth (206) is slidably arranged at the top of the glass cover (4).
5. The automatic dust and fog removing and camera shooting device for the aerospace use according to claim 1, wherein: brush board (205) internally mounted has water pipe (210), through-hole (209) in water pipe (210) the through-hole that passes first spliced pole (203), second spliced pole (204) link to each other with weeping mouth (207) through brush board (205).
6. The automatic dust and fog removing and camera shooting device for the aerospace use according to claim 1, wherein: the water tank (212) is fixedly arranged at the bottom of the shell (1), and the water tank (212) is connected with the water pump (208) through a water pipe (210).
7. The automatic dust and fog removing and camera shooting device for aerospace use according to claim 1, wherein: the fixing block (201), the motor (202) and the water pump (208) are located on the outer side of the front face of the sealing plate (6) and are not connected with the sealing plate (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221606583.9U CN218162577U (en) | 2022-06-26 | 2022-06-26 | Aerospace is with automatic fog camera device that removes dust |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221606583.9U CN218162577U (en) | 2022-06-26 | 2022-06-26 | Aerospace is with automatic fog camera device that removes dust |
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| Publication Number | Publication Date |
|---|---|
| CN218162577U true CN218162577U (en) | 2022-12-27 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221606583.9U Active CN218162577U (en) | 2022-06-26 | 2022-06-26 | Aerospace is with automatic fog camera device that removes dust |
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| CN (1) | CN218162577U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117007529A (en) * | 2023-10-07 | 2023-11-07 | 哈尔滨海鸿基业科技发展有限公司 | Quick auto-focusing microscopic Raman spectrum diagnostic apparatus |
-
2022
- 2022-06-26 CN CN202221606583.9U patent/CN218162577U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117007529A (en) * | 2023-10-07 | 2023-11-07 | 哈尔滨海鸿基业科技发展有限公司 | Quick auto-focusing microscopic Raman spectrum diagnostic apparatus |
| CN117007529B (en) * | 2023-10-07 | 2024-01-12 | 哈尔滨海鸿基业科技发展有限公司 | Quick auto-focusing microscopic Raman spectrum diagnostic apparatus |
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