CN211108037U - Unmanned vehicles camera cloud platform - Google Patents
Unmanned vehicles camera cloud platform Download PDFInfo
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- CN211108037U CN211108037U CN201921685340.7U CN201921685340U CN211108037U CN 211108037 U CN211108037 U CN 211108037U CN 201921685340 U CN201921685340 U CN 201921685340U CN 211108037 U CN211108037 U CN 211108037U
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Abstract
The utility model discloses a belonging to the technical field of aircrafts, in particular to an unmanned aerial vehicle camera tripod head, which comprises an aircraft main body, a camera, a control box and a signal amplifier, wherein a mounting groove is arranged in the middle of the top of the aircraft main body, the camera is arranged in the mounting groove, the control box is arranged in the middle of the bottom of the aircraft main body, a signal transmission module, a voltage stabilizing module, a filtering module, a power supply and a controller are arranged in the control box, through arranging the signal amplifier, the signal of the image collected by the camera in the transmission process of transmitting the image to the controller through the signal transmission module can be enhanced, through arranging the voltage stabilizing module, the voltage in the image transmission process can be more stable, through arranging the filtering module, the external interference electric wave can be filtered, and the stability of the image data in the transmission process can be improved, the practicability and the working efficiency are improved.
Description
Technical Field
The utility model relates to an aircraft technical field specifically is an unmanned vehicles camera cloud platform.
Background
The tripod head camera is installed on the unmanned aerial vehicle through the tripod head, can be used for target tracking and monitoring and the like under the unmanned aerial vehicle aerial photography or special scenes, and can provide stable and clear pictures in the flight process of the unmanned aerial vehicle, however, the existing aircraft camera tripod head usually causes the situations of slow transmission or data transmission loss and the like due to various reasons of poor signals, unstable voltage and external electric wave interference when transmitting shot image data to the outside, and the efficiency is low.
SUMMERY OF THE UTILITY MODEL
This section is for the purpose of summarizing some aspects of embodiments of the invention and to briefly introduce some preferred embodiments. Some simplifications or omissions may be made in this section and in the abstract of the specification and the title of the application to avoid obscuring the purpose of this section, the abstract of the specification and the title of the application, and such simplifications or omissions are not intended to limit the scope of the invention.
In view of the problem that exists in the current aircraft camera cloud platform, provided the utility model discloses.
Therefore, the utility model aims at providing an unmanned vehicles camera cloud platform, through being provided with signal amplifier, the image that can gather the camera strengthens the signal of the transmission in-process of transmitting for the controller through signal transmission module, through being provided with voltage stabilizing module, and the voltage when can making the transmission image is more stable, through being provided with filtering module, can filter the interference electric wave of external world, has improved the stability of image data in transmission process, has improved practicality and work efficiency.
For solving the technical problem, according to the utility model discloses an aspect, the utility model provides a following technical scheme:
an unmanned aerial vehicle camera cloud platform, it includes: aircraft main part, camera, control box and signal amplifier, be provided with the mounting groove in the middle of the top of aircraft main part, set up in the mounting groove the camera, set up in the middle of the bottom of aircraft main part the control box, the inside of control box is provided with signal transmission module, voltage stabilizing module, filter module, power and controller, the bottom right side wall of aircraft main part sets up signal amplifier, the camera passes through signal transmission module signal amplifier, voltage stabilizing module and filter module electric connection in controller, power electric connection in controller, the inside of controller is provided with the WIFI module, the controller passes through WIFI module electric connection in external cloud platform.
As an unmanned vehicles camera cloud platform an preferred scheme, wherein: the aircraft body's bottom four corners department all is provided with the bracing piece, and the front side is two between the bracing piece and the rear side is two all be provided with the bottom plate between the bracing piece, the bottom of bottom plate all is provided with the protection gasket.
As an unmanned vehicles camera cloud platform an preferred scheme, wherein: the aircraft is characterized in that connecting rods are arranged at four corners of the top of the aircraft body, a rotating shaft is arranged on each connecting rod, and propellers are arranged at the top end of each rotating shaft.
As the utility model discloses an optimal selection scheme of unmanned vehicles camera cloud platform, wherein the top left and right sides wall symmetry of mounting groove is provided with two hinges, be provided with L type pole on the hinge, the left side the other end of L type pole is provided with the fixture block, the right side wall the other end of L type pole is provided with the draw-in groove with fixture block matched with.
As an unmanned vehicles camera cloud platform an preferred scheme, wherein: the four side walls of the aircraft main body are provided with protective plates.
As an unmanned vehicles camera cloud platform an preferred scheme, wherein: an image acquisition head is arranged in the middle of the front side wall of the camera, and a transparent glass protection plate is arranged on the image acquisition head.
Compared with the prior art, the beneficial effects of the utility model are that: through being provided with signal amplifier, can strengthen the signal of the image of gathering the camera in the transmission course that the transmission module transmits for the controller through signal transmission module, through being provided with voltage stabilizing module, the voltage when can making the transmission image is more stable, through being provided with filtering module, can filter the interference electric wave in the external world, has improved the stability of image data in transmission course, has improved practicality and work efficiency.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the present invention will be described in detail below with reference to the accompanying drawings and detailed embodiments, and 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 these drawings without inventive labor. Wherein:
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the structure of the fixture block of the present invention;
fig. 3 is a block diagram of the system structure of the present invention.
In the figure, the aircraft comprises an aircraft body 100, a support rod 110, a bottom plate 120, a connecting rod 130, a rotating shaft 140, a propeller 150, a mounting groove 160, an L-type rod 170, a fixture block 180, a camera 200, a control box 300 and a signal amplifier 400.
Detailed Description
In order to make the above objects, features and advantages of the present invention more comprehensible, embodiments of the present invention are described in detail below with reference to the accompanying drawings.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, but the present invention may be implemented in other ways than those specifically described herein, and one skilled in the art may similarly generalize the present invention without departing from the spirit of the present invention, and therefore the present invention is not limited to the specific embodiments disclosed below.
Next, the present invention will be described in detail with reference to the schematic drawings, and in the detailed description of the embodiments of the present invention, for convenience of explanation, the sectional view showing the device structure will not be enlarged partially according to the general scale, and the schematic drawings are only examples, and should not limit the scope of the present invention. In addition, the three-dimensional dimensions of length, width and depth should be included in the actual fabrication.
In order to make the objects, technical solutions and advantages of the present invention clearer, embodiments of the present invention will be described in further detail below with reference to the accompanying drawings.
The utility model provides a following technical scheme: an unmanned aerial vehicle camera cloud platform comprises an aerial vehicle main body 100, a video camera 200, a control box 300 and a signal amplifier 400;
referring to fig. 1 and 2, the aircraft body 100 includes support rods 110, a bottom plate 120, a connecting rod 130, a rotating shaft 140, propellers 150, mounting grooves 160, L-shaped rods 170, a fixture block 180 and a clamping groove, the support rods 110 are installed at four corners of the bottom of the aircraft body 100, the bottom plate 120 is installed between the two support rods 110 at the front side and the two support rods 110 at the rear side, the connecting rod 130 is installed at four corners of the top of the aircraft body 100, the rotating shaft 140 is installed on the connecting rod 130, the propellers 150 are installed at the top end of the rotating shaft 140, the mounting groove 160 is installed at the middle of the top of the aircraft body 100, the L-shaped rods 170 are installed at the left and right side walls of the top of the mounting groove 160, the fixture block 180 and the clamping groove are respectively installed at the two viewing ends of the L-shaped rods 170 at the left and right sides, the aircraft body 100 is used for bearing components, the support rods 110 are used for supporting the aircraft body 100 in cooperation with the bottom plate 120, the connecting rod 130 is used for installing the propellers 150 through the rotating;
referring to fig. 1 again, the camera 200 is installed in the installation groove 160, and the camera 200 is used for capturing images and transmitting the images or video data to the controller;
referring to fig. 1 and 3, a control box 300 includes a signal transmission module, a voltage stabilizing module, a filtering module, a controller and a power supply, the control box 300 is installed in the middle of the bottom of an aircraft main body 100, the signal transmission module, the voltage stabilizing module, the filtering module, the controller and the power supply are all installed inside the control box 300, the signal transmission module is used for being matched with a camera 200 and transmitting image data shot by the camera 200 to the controller, the voltage stabilizing module can enable voltage during image transmission to be more stable, the filtering module can filter external interference electric waves and improve stability of the image data in the transmission process, the controller is used for analyzing and converting received image data and transmitting the image data to an external cradle head through a WIFI module, the power supply is used for supplying power to each component, the signal transmission module specifically adopts a wireless signal transmitter with a model of DTD110H, the voltage stabilizing module specifically adopts a model of 1N4727 voltage stabilizer, the filtering module specifically adopts a model of T L F-91FS filter, the controller specifically adopts a single chip microcomputer with a model of 32, and the power supply specifically is a;
referring again to fig. 1 and 3, a signal amplifier 400 is installed on the bottom right side wall of the aircraft body 100, the signal amplifier 400 is used for enhancing signals of the images acquired by the camera 200 in the transmission process of the images transmitted to the controller through a signal transmission module, and the signal amplifier 400 is specifically a signal amplifier with model number XBK8134 AII.
The working principle is as follows: technical personnel in this technical field start through remote control unit control aircraft main part 100, rethread remote control unit opens camera 200 and shoots, camera 200 passes through signal transmission module and gives the controller with the image or the video transmission who shoots, in transmission process, signal amplifier 400 can strengthen the signal of the image of gathering camera 200 in the transmission process of giving the controller through signal transmission module transmission, voltage when steady voltage module can make the transmission image is more stable, filter module can filter the interference electric wave in the external world, the stability of image data in transmission process has been improved, practicality and work efficiency have been improved, after the controller received image data, give external cloud platform image data transmission through the WIFI module.
While the invention has been described above with reference to an embodiment, various modifications may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In particular, as long as there is no structural conflict, the various features of the disclosed embodiments of the present invention can be used in any combination with each other, and the non-exhaustive description of these combinations in this specification is merely for the sake of brevity and resource conservation. Therefore, it is intended that the invention not be limited to the particular embodiments disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.
Claims (6)
1. The utility model provides an unmanned vehicles camera cloud platform which characterized in that: comprises an aircraft body (100), a camera (200), a control box (300) and a signal amplifier (400), the middle of the top of the aircraft main body (100) is provided with a mounting groove (160), the camera (200) is arranged in the mounting groove (160), the middle of the bottom of the aircraft body (100) is provided with the control box (300), the control box (300) is internally provided with a signal transmission module, a voltage stabilizing module, a filtering module, a power supply and a controller, the bottom right side wall of the aircraft body (100) is provided with the signal amplifier (400), the camera (200) is electrically connected with the controller through the signal transmission module, the signal amplifier (400), the voltage stabilizing module and the filtering module, the power electric connection is in the controller, the inside of controller is provided with the WIFI module, the controller passes through WIFI module electric connection in external cloud platform.
2. The unmanned aerial vehicle camera cloud platform of claim 1, characterized in that: the aircraft body (100) is characterized in that supporting rods (110) are arranged at four corners of the bottom of the aircraft body (100), a bottom plate (120) is arranged between the supporting rods (110) on the front side and between the supporting rods (110) on the rear side, and protective gaskets are arranged at the bottom of the bottom plate (120).
3. The unmanned aerial vehicle camera cloud platform of claim 1, characterized in that: the aircraft is characterized in that connecting rods (130) are arranged at four corners of the top of the aircraft body (100), a rotating shaft (140) is arranged on each connecting rod (130), and propellers (150) are arranged at the top end of each rotating shaft (140).
4. The unmanned aerial vehicle camera tripod head of claim 1, wherein two hinges are symmetrically arranged on the left and right side walls of the top of the mounting groove (160), an L-shaped rod (170) is arranged on the hinges, a clamping block (180) is arranged at the other end of the L-shaped rod (170) on the left side, and a clamping groove matched with the clamping block (180) is arranged at the other end of the L-shaped rod (170) on the right side wall.
5. The unmanned aerial vehicle camera cloud platform of claim 1, characterized in that: the front, the rear, the left and the right side walls of the aircraft main body (100) are provided with protection plates.
6. The unmanned aerial vehicle camera cloud platform of claim 1, characterized in that: an image acquisition head is arranged in the middle of the front side wall of the camera (200), and a transparent glass protection plate is arranged on the image acquisition head.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921685340.7U CN211108037U (en) | 2019-10-09 | 2019-10-09 | Unmanned vehicles camera cloud platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921685340.7U CN211108037U (en) | 2019-10-09 | 2019-10-09 | Unmanned vehicles camera cloud platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211108037U true CN211108037U (en) | 2020-07-28 |
Family
ID=71689249
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921685340.7U Expired - Fee Related CN211108037U (en) | 2019-10-09 | 2019-10-09 | Unmanned vehicles camera cloud platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211108037U (en) |
-
2019
- 2019-10-09 CN CN201921685340.7U patent/CN211108037U/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 |
Granted publication date: 20200728 Termination date: 20211009 |
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| CF01 | Termination of patent right due to non-payment of annual fee |