CN210284644U - Avionics monitoring equipment mounting bracket - Google Patents
Avionics monitoring equipment mounting bracket Download PDFInfo
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- CN210284644U CN210284644U CN201920846959.5U CN201920846959U CN210284644U CN 210284644 U CN210284644 U CN 210284644U CN 201920846959 U CN201920846959 U CN 201920846959U CN 210284644 U CN210284644 U CN 210284644U
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Abstract
The utility model discloses an avionics monitoring facilities installing support, including mounting panel, mounting hole, spliced pole, connection pad, fixed plate, connecting block, tooth trace groove, camera body, first motor, guide way, guide block, second motor, mounting groove, bearing, gear, round bar, thread groove and draw bolt. The connecting disc can be driven to rotate around the connecting column through the second motor, so that the camera body can rotate in the horizontal direction, and then under the action of the first motor, the first motor drives the gear and simultaneously enables the camera body to rotate in the vertical direction due to the fact that the gear is meshed with the tooth trace groove to rotate, and the problem that the angle of the camera body cannot be freely adjusted in the traditional technology is solved; can be with the guide block in the inside of guide way, the thread groove of guide block one end this moment can be to it with draw bolt's one end, and the rotatory draw bolt of accessible meshes with the thread groove, and the maintenance in the camera body later stage of being convenient for is changed.
Description
Technical Field
The utility model relates to an electronic monitoring equipment installing support specifically is an avionics monitoring equipment installing support belongs to aviation equipment technical field.
Background
The aerial survey of the unmanned aerial vehicle is a powerful supplement of the traditional aerial photogrammetry means, has the characteristics of flexibility, high efficiency, rapidness, fineness, accuracy, low operation cost, wide application range, short production period and the like, the method has obvious advantages in the aspect of fast obtaining of high-resolution images in small areas and areas with difficult flight, along with the development of unmanned aerial vehicles and digital camera technologies, the digital aerial photography technology based on an unmanned aerial vehicle platform has shown unique advantages, the combination of the unmanned aerial vehicles and aerial photogrammetry enables the 'unmanned aerial vehicle digital low-altitude remote sensing' to become a brand-new development direction in the field of aerial remote sensing, the aerial photography of the unmanned aerial vehicles can be widely applied to the aspects of national major engineering construction, disaster emergency and treatment, territorial supervision, resource development, new rural areas, small town construction and the like, and the method has wide prospects in the aspects of basic surveying and mapping, land resource investigation and monitoring, dynamic monitoring of land utilization, digital city construction, acquisition of emergency disaster relief surveying and mapping data and.
Along with the rapid development of unmanned aerial vehicle aerial survey technique, camera monitoring facilities has also obtained extensive application on unmanned aerial vehicle, what the installing support of monitoring unmanned aerial vehicle adopted usually among the prior art is the fixed bolster, and the scope of making a video recording can become comparatively to limit to in the use, is difficult to freely adjust its angle, and the camera on the present monitoring unmanned aerial vehicle is comparatively troublesome when dismantling, and the maintenance in later stage of not being convenient for is changed. Accordingly, an avionics monitoring device mounting bracket is proposed to address the above-mentioned problems.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is just in order to solve above-mentioned problem and provide an avionics monitoring facilities installing support.
The utility model discloses a technical scheme realizes above-mentioned purpose, an avionic monitoring device mounting bracket, including mounting panel, angle adjustment structure, guide block and camera body that install from top to bottom in proper order, the surface of the said mounting panel is opened with the mounting hole;
the angle adjusting structure comprises a connecting column, a connecting disc, a fixing plate, a connecting block, a bearing and a round rod, wherein the connecting column is fixedly connected to the lower surface of the mounting plate, a mounting groove is formed in the upper surface of the connecting disc, the bottom end of the connecting column is clamped inside the mounting groove, and the bottom end of the connecting column is rotatably connected with the connecting disc through the bearing; a second motor is embedded at the bottom end of the connecting column, and the tail end of an output shaft of the second motor is fixedly connected with the bottom of the inner cavity of the mounting groove; the fixed plate is fixedly connected to the lower surface of the connecting disc, a first motor is fixedly connected to one side of the fixed plate, the tail end of an output shaft of the first motor penetrates through one side of the fixed plate, and a gear is sleeved at the tail end of the output shaft of the first motor; the connecting block is clamped between the two side plates of the fixing plate and is rotationally connected with the fixing plate through the round rod, a tooth mark groove is formed in the upper surface of the connecting block, and the gear is meshed with the tooth mark groove;
the lower surface of connecting block is opened there is the guide way, the top rigid coupling of camera body has the guide block, the guide block is in the inside of guide way, open one side of guide block has the thread groove, the one end terminal surface of connecting block runs through there is traction bolt, traction bolt passes through the bearing with the connecting block is rotated and is connected, just traction bolt with the thread groove meshing is connected.
Preferably, the number of the mounting holes is four, and the mounting holes are symmetrically distributed on the upper surface of the mounting plate.
Preferably, the connecting column and the connecting disc are both of a columnar structure, and the size of the connecting column is matched with that of the mounting groove.
Preferably, the fixing plate is of a U-shaped structure, and the upper surface of the connecting block is of a semicircular structure.
Preferably, the guide groove is of a concave structure, the guide block is of a convex structure, and the sizes of the guide groove and the guide block are matched.
Preferably, the gear is of a cylindrical structure, and the length of the gear is the same as the width of the connecting block.
The utility model has the advantages that:
1. the utility model discloses can drive the connection pad through the second motor and rotate around the spliced pole to this realizes the rotation of camera body in the horizontal direction, then under the effect of first motor, first motor can make camera body rotate in the vertical direction this moment because gear and tooth trace groove meshing rotate in the same time of drive gear, has solved the problem that it is difficult to freely adjust its angle in the traditional art;
2. the utility model discloses install the guide block at the top of camera body, it has the guide way to open in the bottom of connecting block, because the guide block is protruding type structure and guide way and is concave type structure, can be with the guide block in the inside of guide way, the thread groove of guide block one end this moment can be to it with traction bolt's one end, and the rotatory traction bolt of accessible meshes with the thread groove, and the maintenance in the camera body later stage of being convenient for is changed.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without inventive exercise.
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a half sectional view of the overall structure of the present invention;
fig. 3 is a schematic view of the structure of the guide block of the present invention.
In the figure: 1. mounting panel, 2, mounting hole, 3, spliced pole, 4, connection pad, 5, fixed plate, 6, connecting block, 61, tooth trace groove, 7, camera body, 8, first motor, 9, guide way, 10, guide block, 11, second motor, 12, mounting groove, 13, bearing, 14, gear, 15, round bar, 16, thread groove, 17, draw bolt.
Detailed Description
In order to make the objects, features and advantages of the present invention more obvious and understandable, the drawings in the embodiments of the present invention are combined below to clearly and completely describe the technical solutions in the embodiments of the present invention, and obviously, the embodiments described below are only some embodiments of the present invention, but not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
The technical solution of the present invention is further explained by the following embodiments with reference to the accompanying drawings.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those 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 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.
Referring to fig. 1-3, an avionic monitoring device mounting bracket comprises a mounting plate 1, an angle adjusting structure, a guide block 10 and a camera body 7 which are sequentially mounted from top to bottom, wherein a mounting hole 2 is formed in the surface of the mounting plate 1;
the angle adjusting structure comprises a connecting column 3, a connecting disc 4, a fixing plate 5, a connecting block 6, a bearing 13 and a round rod 15, wherein the connecting column 3 is fixedly connected to the lower surface of the mounting plate 1, a mounting groove 12 is formed in the upper surface of the connecting disc 4, the bottom end of the connecting column 3 is clamped in the mounting groove 12, and the bottom end of the connecting column 3 is rotatably connected with the connecting disc 4 through the bearing 13; a second motor 11 is embedded at the bottom end of the connecting column 3, and the tail end of an output shaft of the second motor 11 is fixedly connected with the bottom of an inner cavity of the mounting groove 12; the fixing plate 5 is fixedly connected to the lower surface of the connecting plate 4, a first motor 8 is fixedly connected to one side of the fixing plate 5, the tail end of an output shaft of the first motor 8 penetrates through one side of the fixing plate 5, and a gear 14 is sleeved at the tail end of the output shaft of the first motor 8; the connecting block 6 is clamped between two side plates of the fixing plate 5, the connecting block 6 is rotatably connected with the fixing plate 5 through the round rod 15, a tooth mark groove 61 is formed in the upper surface of the connecting block 6, and the gear 14 is meshed with the tooth mark groove 61;
the lower surface of connecting block 6 is opened there is guide way 9, the top rigid coupling of camera body 7 has guide block 10, guide block 10 block is in the inside of guide way 9, threaded groove 16 has been opened to one side of guide block 10, the one end terminal surface of connecting block 6 runs through there is traction bolt 17, traction bolt 17 passes through bearing 13 with connecting block 6 rotates to be connected, just traction bolt 17 with the threaded groove 16 meshing is connected.
The number of the mounting holes 2 is four, and the mounting holes are symmetrically distributed on the upper surface of the mounting plate 1, so that the mounting plate 1 can be conveniently fixed on the unmanned aerial vehicle body; the connecting column 3 and the connecting disc 4 are both of a columnar structure, and the size of the connecting column 3 is matched with that of the mounting groove 12, so that the connecting disc 4 is driven by the second motor 11 to rotate around the connecting column 3; the fixing plate 5 is of a U-shaped structure, and the upper surface of the connecting block 6 is of a semicircular structure, so that the connecting block 6 is conveniently and rotatably connected with the fixing plate 5; the guide groove 9 is of a concave structure, the guide block 10 is of a convex structure, and the sizes of the guide groove and the guide block are matched, so that the guide block 10 is conveniently connected with the bottom end of the connecting block 6 in a sliding manner; the gear 14 is of a cylindrical structure, and the length of the gear 14 is the same as the width of the connecting block 6, so that the gear 14 is driven by the first motor 8 to rotate and the gear 14 is meshed with the tooth trace groove 61 on the surface of the connecting block 6 for transmission.
When the utility model is used, the electrical components in the application are externally connected with a power supply and a control switch, firstly, the guide block 10 arranged at the top of the camera body 7 is clamped inside the guide groove 9 at the lower surface of the connecting block 6, at the moment, the thread groove 16 at one end of the guide block 10 is aligned with one end of the traction bolt 17 at the side surface of the connecting block 6, and one end of the traction bolt 17 is meshed into the thread groove 16 by rotating the traction bolt 17, so that the connecting block 6 and the guide block 10 are fixed;
when the angle of the mounting bracket is adjusted, the gear 14 is driven to rotate by the first motor 8, and simultaneously, the gear 14 is meshed with the tooth mark groove 61 on the upper surface of the connecting block 6, so that the connecting block 6 is driven by the first motor 8 to rotate around the round rod 15, and the angle of the camera body 7 in the vertical direction is adjusted; then the second motor 11 rotates, and meanwhile, the connecting column 3 and the connecting disc 4 are rotatably connected through the bearing 13, and the angle of the camera body 7 in the horizontal direction can be adjusted through rotation of the second motor 11.
The first motor 8 and the second motor 11 are both ZGA37RG model provided by zhengk flagship store and related matched power supply and circuit.
It is well within the skill of those in the art to implement, without undue experimentation, the present invention does not relate to software and process improvements, as related to circuits and electronic components and modules.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
The above-mentioned embodiments are only used for illustrating the technical solutions of the present invention, and not for limiting the same; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions of the embodiments of the present invention.
Claims (6)
1. The utility model provides an avionics monitoring device installing support which characterized in that: the angle adjusting device comprises a mounting plate (1), an angle adjusting structure, a guide block (10) and a camera body (7) which are sequentially mounted from top to bottom, wherein a mounting hole (2) is formed in the surface of the mounting plate (1);
the angle adjusting structure comprises a connecting column (3), a connecting disc (4), a fixing plate (5), a connecting block (6), a bearing (13) and a round rod (15), wherein the connecting column (3) is fixedly connected to the lower surface of the mounting plate (1), a mounting groove (12) is formed in the upper surface of the connecting disc (4), the bottom end of the connecting column (3) is clamped inside the mounting groove (12), and the bottom end of the connecting column (3) is rotatably connected with the connecting disc (4) through the bearing (13); a second motor (11) is embedded at the bottom end of the connecting column (3), and the tail end of an output shaft of the second motor (11) is fixedly connected with the bottom of an inner cavity of the mounting groove (12); the fixing plate (5) is fixedly connected to the lower surface of the connecting plate (4), a first motor (8) is fixedly connected to one side of the fixing plate (5), the tail end of an output shaft of the first motor (8) penetrates through one side of the fixing plate (5), and a gear (14) is sleeved at the tail end of the output shaft of the first motor (8); the connecting block (6) is clamped between two side plates of the fixing plate (5), the connecting block (6) is rotatably connected with the fixing plate (5) through the round rod (15), a tooth mark groove (61) is formed in the upper surface of the connecting block (6), and the gear (14) is meshed with the tooth mark groove (61);
the lower surface of connecting block (6) is opened there are guide way (9), the top rigid coupling of camera body (7) has guide block (10), guide block (10) block is in the inside of guide way (9), threaded groove (16) are opened to one side of guide block (10), the one end terminal surface of connecting block (6) runs through there is traction bolt (17), traction bolt (17) pass through bearing (13) with connecting block (6) rotate to be connected, just traction bolt (17) with threaded groove (16) meshing is connected.
2. The avionics monitoring device mounting bracket of claim 1, further comprising: the number of the mounting holes (2) is four, and the mounting holes are symmetrically distributed on the upper surface of the mounting plate (1).
3. The avionics monitoring device mounting bracket of claim 1, further comprising: the connecting column (3) and the connecting disc (4) are of a columnar structure, and the size of the connecting column (3) is matched with that of the mounting groove (12).
4. The avionics monitoring device mounting bracket of claim 1, further comprising: the fixing plate (5) is of a U-shaped structure, and the upper surface of the connecting block (6) is of a semicircular structure.
5. The avionics monitoring device mounting bracket of claim 1, further comprising: the guide groove (9) is of a concave structure, the guide block (10) is of a convex structure, and the sizes of the guide groove and the guide block are matched.
6. The avionics monitoring device mounting bracket of claim 1, further comprising: the gear (14) is of a columnar structure, and the length of the gear is the same as the width of the connecting block (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920846959.5U CN210284644U (en) | 2019-06-05 | 2019-06-05 | Avionics monitoring equipment mounting bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920846959.5U CN210284644U (en) | 2019-06-05 | 2019-06-05 | Avionics monitoring equipment mounting bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210284644U true CN210284644U (en) | 2020-04-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920846959.5U Expired - Fee Related CN210284644U (en) | 2019-06-05 | 2019-06-05 | Avionics monitoring equipment mounting bracket |
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| Country | Link |
|---|---|
| CN (1) | CN210284644U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112498724A (en) * | 2020-11-27 | 2021-03-16 | 广东电网有限责任公司肇庆供电局 | Airborne camera capable of freely rotating |
| CN112833298A (en) * | 2021-01-18 | 2021-05-25 | 中研电子(杭州)有限公司 | Panoramic photography head rifle ball aggregate unit |
| CN113479330A (en) * | 2021-07-02 | 2021-10-08 | 江西师范高等专科学校 | Unmanned aerial vehicle shower nozzle that can realize crops multiaspect and spray based on 5G thing networking |
| CN114845045A (en) * | 2022-03-24 | 2022-08-02 | 安徽超清科技股份有限公司 | High-speed video inspection device based on 5G |
-
2019
- 2019-06-05 CN CN201920846959.5U patent/CN210284644U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112498724A (en) * | 2020-11-27 | 2021-03-16 | 广东电网有限责任公司肇庆供电局 | Airborne camera capable of freely rotating |
| CN112498724B (en) * | 2020-11-27 | 2022-04-05 | 广东电网有限责任公司肇庆供电局 | Airborne camera capable of freely rotating |
| CN112833298A (en) * | 2021-01-18 | 2021-05-25 | 中研电子(杭州)有限公司 | Panoramic photography head rifle ball aggregate unit |
| CN113479330A (en) * | 2021-07-02 | 2021-10-08 | 江西师范高等专科学校 | Unmanned aerial vehicle shower nozzle that can realize crops multiaspect and spray based on 5G thing networking |
| CN114845045A (en) * | 2022-03-24 | 2022-08-02 | 安徽超清科技股份有限公司 | High-speed video inspection device based on 5G |
| CN114845045B (en) * | 2022-03-24 | 2023-08-29 | 安徽超清科技股份有限公司 | High-speed video inspection device based on 5G |
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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 |
Granted publication date: 20200410 Termination date: 20210605 |
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| CF01 | Termination of patent right due to non-payment of annual fee |