CN215596862U - Composite material unmanned aerial vehicle control support - Google Patents
Composite material unmanned aerial vehicle control support Download PDFInfo
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- CN215596862U CN215596862U CN202122326425.XU CN202122326425U CN215596862U CN 215596862 U CN215596862 U CN 215596862U CN 202122326425 U CN202122326425 U CN 202122326425U CN 215596862 U CN215596862 U CN 215596862U
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Abstract
A composite material unmanned aerial vehicle monitoring support relates to the technical field of unmanned aerial vehicles. For solving current unmanned aerial vehicle control support generally be a whole, camera device installs inside camera support, but when dismantling and assembling, because camera support generally can not dismantle, lead to camera device's dismantlement and assembly very inconvenient to can produce the vibration when unmanned aerial vehicle descends, can lead to the problem that monitoring facility damaged when serious. When using, be connected whole device through the bottom of screw thread spliced pole with unmanned aerial vehicle, and place the upper surface of mounting panel with supervisory equipment, and utilize control fixing bolt, fix supervisory equipment's bottom to the mounting panel on, the adjusting bolt of rotatory both sides again adopts the screw hole cooperation on adjusting bolt and the curb plate, rotatory adjusting bolt can promote adjusting baffle and slide on the mounting panel, thereby realize the horizontal location to supervisory equipment, and then accomplish supervisory equipment's installation. The utility model is suitable for the technical field of unmanned aerial vehicles.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a composite material unmanned aerial vehicle monitoring support.
Background
In the field of avionics, an unmanned aerial vehicle (unmanned aerial vehicle, UAV for short) has the characteristics of small volume, light weight, low cost, flexible operation and high safety, and can be widely applied to the fields of monitoring, search and rescue, resource exploration, agricultural irrigation and the like.
The important function as unmanned aerial vehicle of taking photo by plane, accessible camera device realizes. The existing camera device is installed on the unmanned aerial vehicle by using a holder. The pan and tilt head generally includes a shock absorbing module, a yaw module, and a pitch module. During the in-service use, install a camera device on the every single move module, and the shock attenuation module is fixed with unmanned aerial vehicle's fuselage and is used for keeping apart the vibration between cloud platform and unmanned aerial vehicle, the damping module is connected to the driftage module and can rotate around the yaw axle for the damping module, the every single move module is connected the driftage module and can rotate around the roll axle for the driftage module, moreover, the every single move module can also rotate around the pitch axle, and three axles are mutually perpendicular.
Wherein, when camera device installs on the every single move module, the inside camera support that generally has of every single move module, camera device installs on this camera support, the output shaft of camera support and pitch motor for the camera support can rotate around the pitch axle under the drive of motor, thereby realizes that camera device rotates around the pitch axle in the every single move module.
The unmanned aerial vehicle control support that has now generally is a whole, and camera device installs inside camera support, but when dismantling and assembling, because camera support generally can not dismantle, and the dismantlement and the assembly that lead to camera device are very inconvenient to can produce the vibration when unmanned aerial vehicle descends, can lead to the problem that monitoring facility damaged when serious.
SUMMERY OF THE UTILITY MODEL
The utility model provides a composite material unmanned aerial vehicle monitoring support, which aims to solve the problems that an existing unmanned aerial vehicle monitoring support is generally an integral body, a camera device is installed in a camera support, but the camera support cannot be disassembled generally during disassembly and assembly, so that the disassembly and assembly of the camera device are very inconvenient, vibration is generated during landing of an unmanned aerial vehicle, and monitoring facilities are damaged seriously.
The utility model discloses a composite material unmanned aerial vehicle monitoring support which comprises a cover plate, side plates, adjusting bolts, adjusting baffle plates, sliding rails, a base, monitoring fixing bolts, a damping unit and a mounting plate, wherein the side plates are arranged on the side plates;
the two sides of the upper surface of the base are respectively provided with a side plate, the middle of each side plate is provided with a threaded hole, an adjusting bolt is arranged inside each threaded hole, the middle of the upper surface of the base is provided with a mounting plate, n damping units are arranged between the upper surface of the base and the lower surface of the mounting plate, n is a positive integer, the middle of the upper surface of the mounting plate is provided with a through hole, the middle of the bottom surface of the base is provided with a threaded hole, a monitoring fixing bolt is arranged in each threaded hole, the top of the monitoring fixing bolt penetrates through the through hole in the mounting plate, two ends of the upper surface of the mounting plate are respectively provided with a sliding rail, each sliding rail is provided with an adjusting baffle, the adjusting baffles are in sliding connection with the sliding rails, one side of the lower surface of the cover plate is fixedly connected with the top end of one side plate, and the other side of the lower surface of the cover plate is fixedly connected with the top end of the other side plate;
furthermore, the outer side of each adjusting baffle is in contact with one end of an adjusting bolt;
furthermore, a rubber pad is arranged between the outer side of the adjusting baffle and one end of the adjusting bolt;
furthermore, the number n of the damping units is more than or equal to 10 and less than or equal to 50;
further, the damping unit comprises a push rod, a sleeve and a spring; the upper surface of the sleeve is provided with a through hole, a push rod is arranged in the through hole, and a spring is arranged between the bottom of the push rod and the inner bottom surface of the sleeve;
furthermore, a disc is arranged at the bottom of the push rod;
furthermore, the diameter of the end face of the push rod is smaller than that of the end face of the disc;
furthermore, a threaded connecting column is arranged in the center of the upper surface of the cover plate;
further, when using, be connected whole device through the bottom of screw thread spliced pole with unmanned aerial vehicle, and place the upper surface of mounting panel with supervisory equipment, and utilize control fixing bolt, fix supervisory equipment's bottom to the mounting panel, the adjusting bolt of rotatory both sides again adopts the screw hole cooperation on adjusting bolt and the curb plate, rotatory adjusting bolt can promote adjusting the baffle and slide on the mounting panel, thereby realize the horizontal location to supervisory equipment, and then accomplish supervisory equipment's installation.
Compared with the prior art, the utility model has the following beneficial effects:
the utility model overcomes the defects of the prior art, adopts a frame type bracket, the front side and the rear side of the frame type bracket are not provided with a baffle, monitoring equipment is placed on the upper surface of the mounting plate, the bottom of the monitoring equipment is fixed on the mounting plate by utilizing a monitoring fixing bolt, then adjusting bolts at the two sides are rotated, the adjusting bolts are matched with threaded holes on the side plates, and the adjusting bolts are rotated to push the adjusting baffle to slide on the mounting plate, thereby realizing the transverse positioning of the monitoring equipment;
adopt to be equipped with a plurality of shock attenuation units between the upper surface of base and the lower surface of mounting panel, when unmanned aerial vehicle takes off and descends, usable shock attenuation unit offsets the vibration when unmanned aerial vehicle takes off or descends, avoids supervisory equipment to damage, improves life.
Drawings
Fig. 1 is a main sectional view of a composite material unmanned aerial vehicle monitoring support according to the present invention;
fig. 2 is a sectional view of a damping unit in a composite material unmanned aerial vehicle monitoring bracket according to the utility model.
Detailed Description
The first embodiment is as follows: the embodiment is described with reference to fig. 1, and the composite material unmanned aerial vehicle monitoring support in the embodiment comprises a cover plate 1, a side plate 2, an adjusting bolt 3, an adjusting baffle 4, a slide rail 5, a base 6, a monitoring fixing bolt 7, a damping unit 8 and a mounting plate 9;
two sides of the upper surface of the base 6 are respectively provided with a side plate 2, the middle part of each side plate 2 is provided with a threaded hole, and the inner part of the threaded hole is provided with an adjusting bolt 3, the middle part of the upper surface of the base 6 is provided with a mounting plate 9, and n damping units 8 are arranged between the upper surface of the base 6 and the lower surface of the mounting plate 9, n is a positive integer, the middle part of the upper surface of the mounting plate 9 is provided with a through hole, the middle part of the bottom surface of the base 6 is provided with a threaded hole, and the threaded hole is provided with a monitoring fixing bolt 7, the top of the monitoring fixing bolt 7 passes through the through hole on the mounting plate 9, two ends of the upper surface of the mounting plate 9 are respectively provided with a sliding rail 5, each sliding rail 5 is provided with an adjusting baffle 4, the adjusting baffle 4 is connected with the sliding rail 5 in a sliding manner, one side of the lower surface of the cover plate 1 is fixedly connected with the top end of one side plate 2, and the other side of the lower surface of the cover plate 1 is fixedly connected with the top end of the other side plate 2;
this embodiment, when using, be connected whole device through threaded connection post 10 and unmanned aerial vehicle's bottom, and place the upper surface of mounting panel 9 with supervisory equipment, and utilize control fixing bolt 7, fix supervisory equipment's bottom to mounting panel 9 on, the adjusting bolt 3 of rotatory both sides again, adopt the screw hole cooperation on adjusting bolt 3 and the curb plate 2, rotatory adjusting bolt 3, can promote adjusting baffle 4 and slide on mounting panel 9, thereby realize the horizontal location to supervisory equipment, and then accomplish supervisory equipment's installation.
The second embodiment is as follows: the embodiment is described with reference to fig. 1, and the embodiment is a further limitation to the monitoring bracket described in the first embodiment, and in the composite material unmanned aerial vehicle monitoring bracket described in the embodiment, the outer side of each adjusting baffle 4 is in contact with one end of an adjusting bolt 3.
The third concrete implementation mode: the embodiment is described with reference to fig. 1, and the embodiment is a further limitation to the monitoring bracket described in the second embodiment, in the composite material unmanned aerial vehicle monitoring bracket described in the embodiment, a rubber pad is arranged between the outer side of the adjusting baffle 4 and one end of the adjusting bolt 3;
in the specific embodiment, a rubber pad is arranged between the outer side of the adjusting baffle 4 and one end of the adjusting bolt 3, so that the outer side of the adjusting baffle 4 and one end of the adjusting bolt 3 are prevented from being abraded, and the service life is prolonged.
The fourth concrete implementation mode: the embodiment is described with reference to fig. 1, and the embodiment is a further limitation to the monitoring support described in the first embodiment, and in the monitoring support for a composite material unmanned aerial vehicle described in the embodiment, the number n of the damping units 8 is greater than or equal to 10 and less than or equal to 50.
The fifth concrete implementation mode: the embodiment is described with reference to fig. 2, and the embodiment is a further limitation to the monitoring bracket described in the first embodiment, and the composite material unmanned aerial vehicle monitoring bracket described in the embodiment includes that the damping unit 8 includes a push rod 8-1, a sleeve 8-2 and a spring 8-3; the upper surface of the sleeve 8-2 is provided with a through hole, a push rod 8-1 is arranged in the through hole, and a spring 8-3 is arranged between the bottom of the push rod 8-1 and the inner bottom surface of the sleeve 8-2;
this embodiment adopts and is equipped with a plurality of shock attenuation units between the upper surface of base and the lower surface of mounting panel, when unmanned aerial vehicle takes off and descends, and usable shock attenuation unit offsets the vibration when unmanned aerial vehicle takes off or descends, avoids supervisory equipment to damage, improves life.
The sixth specific implementation mode: the embodiment is described with reference to fig. 2, and is a further limitation to the monitoring support described in the fifth embodiment, in the composite material unmanned aerial vehicle monitoring support described in the embodiment, a disc is provided at the bottom of the push rod 8-1.
The seventh embodiment: the embodiment is described with reference to fig. 2, and is a further limitation to the monitoring support according to the sixth embodiment, in the composite material unmanned aerial vehicle monitoring support according to the embodiment, the end surface diameter of the push rod 8-1 is smaller than the end surface diameter of the disc;
in the specific embodiment, the diameter of the end face of the push rod 8-1 is smaller than that of the end face of the disc, so that the push rod 8-1 is limited.
The specific implementation mode is eight: the embodiment is described with reference to fig. 1, and the embodiment is a further limitation to the monitoring bracket of the first embodiment, in which a threaded connection column 10 is disposed at the center of the upper surface of the cover plate 1;
this embodiment, the upper surface central part that adopts apron 1 is equipped with a threaded connection post 10, and threaded connection post 10 is used for being connected unmanned aerial vehicle and control leg.
The specific implementation method nine: the present embodiment is described with reference to fig. 1, and is a further limitation to the monitoring bracket described in the first embodiment, and in the monitoring bracket for a composite material unmanned aerial vehicle described in the present embodiment, the cover plate 1, the side plate 2, the base 6, and the mounting plate 9 are all made of composite materials.
The theory of operation is when using, pass through threaded connection post 10 with whole device and be connected with unmanned aerial vehicle's bottom, and place the upper surface of mounting panel 9 with supervisory equipment, and utilize control fixing bolt 7, fix supervisory equipment's bottom to mounting panel 9 on, the adjusting bolt 3 of rotatory both sides again, adopt adjusting bolt 3 and the screw hole cooperation on the curb plate 2, rotatory adjusting bolt 3, can promote adjusting the baffle 4 and slide on mounting panel 9, thereby realize the horizontal location to supervisory equipment, and then accomplish supervisory equipment's installation.
Claims (8)
1. The utility model provides a combined material unmanned aerial vehicle control support which characterized in that: the device comprises a cover plate (1), side plates (2), adjusting bolts (3), adjusting baffle plates (4), slide rails (5), a base (6), monitoring fixing bolts (7), a damping unit (8) and a mounting plate (9);
the two sides of the upper surface of a base (6) are respectively provided with a side plate (2), the middle part of each side plate (2) is provided with a threaded hole, an adjusting bolt (3) is arranged inside the threaded hole, the middle part of the upper surface of the base (6) is provided with a mounting plate (9), n damping units (8) are arranged between the upper surface of the base (6) and the lower surface of the mounting plate (9), n is a positive integer, the middle part of the upper surface of the mounting plate (9) is provided with a through hole, the middle part of the bottom surface of the base (6) is provided with a threaded hole, a monitoring fixing bolt (7) is arranged in the threaded hole, the top of the monitoring fixing bolt (7) penetrates through the through hole on the mounting plate (9), two ends of the upper surface of the mounting plate (9) are respectively provided with a sliding rail (5), each sliding rail (5) is provided with an adjusting baffle (4), and the adjusting baffles (4) are connected with the sliding rails (5) in a sliding way, one side of the lower surface of the cover plate (1) is fixedly connected with the top end of one side plate (2), and the other side of the lower surface of the cover plate (1) is fixedly connected with the top end of the other side plate (2).
2. The composite material unmanned aerial vehicle monitoring support of claim 1, wherein: the outer side of each adjusting baffle (4) is in contact with one end of each adjusting bolt (3).
3. The composite material unmanned aerial vehicle monitoring support of claim 2, wherein: a rubber pad is arranged between the outer side of the adjusting baffle (4) and one end of the adjusting bolt (3).
4. The composite material unmanned aerial vehicle monitoring support of claim 1, wherein: the number n of the damping units (8) is more than or equal to 10 and less than or equal to 50.
5. The composite material unmanned aerial vehicle monitoring support of claim 1, wherein: the damping unit (8) comprises a push rod (8-1), a sleeve (8-2) and a spring (8-3);
the upper surface of the sleeve (8-2) is provided with a through hole, a push rod (8-1) is arranged in the through hole, and a spring (8-3) is arranged between the bottom of the push rod (8-1) and the inner bottom surface of the sleeve (8-2).
6. The composite material unmanned aerial vehicle monitoring support of claim 5, wherein: the bottom of the push rod (8-1) is provided with a disc.
7. The composite material unmanned aerial vehicle monitoring support of claim 6, wherein: the diameter of the end face of the push rod (8-1) is smaller than that of the end face of the disc.
8. The composite material unmanned aerial vehicle monitoring support of claim 1, wherein: the center of the upper surface of the cover plate (1) is provided with a threaded connecting column (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122326425.XU CN215596862U (en) | 2021-09-24 | 2021-09-24 | Composite material unmanned aerial vehicle control support |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122326425.XU CN215596862U (en) | 2021-09-24 | 2021-09-24 | Composite material unmanned aerial vehicle control support |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215596862U true CN215596862U (en) | 2022-01-21 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122326425.XU Active CN215596862U (en) | 2021-09-24 | 2021-09-24 | Composite material unmanned aerial vehicle control support |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215596862U (en) |
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2021
- 2021-09-24 CN CN202122326425.XU patent/CN215596862U/en active Active
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