CN216233041U - Unmanned aerial vehicle survey and drawing data acquisition device - Google Patents
Unmanned aerial vehicle survey and drawing data acquisition device Download PDFInfo
- Publication number
- CN216233041U CN216233041U CN202123095058.3U CN202123095058U CN216233041U CN 216233041 U CN216233041 U CN 216233041U CN 202123095058 U CN202123095058 U CN 202123095058U CN 216233041 U CN216233041 U CN 216233041U
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- Prior art keywords
- aerial vehicle
- unmanned aerial
- control box
- fixedly connected
- vehicle body
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- 238000013507 mapping Methods 0.000 claims abstract description 12
- 238000013016 damping Methods 0.000 claims description 12
- 230000005540 biological transmission Effects 0.000 claims description 9
- 230000003139 buffering effect Effects 0.000 claims description 5
- 238000005096 rolling process Methods 0.000 claims description 5
- 238000013480 data collection Methods 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 4
- 238000000034 method Methods 0.000 description 7
- 230000035939 shock Effects 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
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Abstract
The utility model belongs to the technical field of surveying and mapping devices, and discloses an unmanned aerial vehicle surveying and mapping data acquisition device, which is technically characterized in that: including the unmanned aerial vehicle body, the unmanned aerial vehicle body is provided with the supporting leg all around respectively, unmanned aerial vehicle body diapire rotates installs the control box, slidable mounting has the connecting rod that extends the control box in the control box, the multiunit the connecting rod is located the common fixedly connected with mounting panel of the outer one end of control box, be provided with fixture in the mounting panel, be provided with the buffer gear who is connected with the connecting rod in the control box, install the steering mechanism who is connected with unmanned aerial vehicle body diapire in the control box, be provided with damper in the supporting leg.
Description
Technical Field
The utility model relates to the technical field of surveying and mapping devices, in particular to an unmanned aerial vehicle surveying and mapping data acquisition device.
Background
As is well known, an unmanned aerial vehicle mapping data acquisition device is an auxiliary device for measuring and acquiring the shape, size, spatial position, attributes and the like of natural geographic elements or surface artificial facilities, and is widely used in the mapping field; the existing unmanned aerial vehicle surveying and mapping data acquisition device comprises an unmanned aerial vehicle, a controller, a support and a camera, wherein the support is arranged at the bottom end of the unmanned aerial vehicle, the camera is arranged at the bottom end of the support, the controller is arranged on the right side of the top end of the support, and the controller is connected with the unmanned aerial vehicle and the camera through electric wires; when the unmanned aerial vehicle surveying and mapping data acquisition device is used, the unmanned aerial vehicle is controlled to move through the controller, and the camera is controlled to make a video.
But current unmanned aerial vehicle is when using, and the fixed unable regulation that can't of the direction of making a video recording of unmanned aerial vehicle surface mounting's camera, in the use, need control unmanned aerial vehicle usually and rotate and then shoot the equidirectional, but unmanned aerial vehicle's the rotation in-process shake is great, and stability is relatively poor to current unmanned aerial vehicle lacks corresponding protection shock attenuation measure at the in-process of taking off and landing.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an unmanned aerial vehicle surveying and mapping data acquisition device to solve the problems in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme:
the utility model provides an unmanned aerial vehicle survey and drawing data collection system, includes the unmanned aerial vehicle body, the unmanned aerial vehicle body is provided with the supporting leg all around respectively, the unmanned aerial vehicle body diapire rotates installs the control box, slidable mounting has the connecting rod that extends the control box in the control box, the multiunit the connecting rod is located the common fixedly connected with mounting panel of the outer one end of control box, be provided with fixture in the mounting panel, be provided with the buffer gear who is connected with the connecting rod in the control box, install the steering mechanism who is connected with unmanned aerial vehicle body diapire in the control box, be provided with damper in the supporting leg.
As a further scheme of the utility model: fixture is including the spout of the rectangular shape that the mounting panel diapire was seted up, the threaded rod is installed to the spout internal rotation, the screw thread opposite direction of threaded rod both sides, threaded rod surface threaded connection has two sets of relative distribution's sliding block, the supporting rod of spout and fixedly connected with L type is extended to the sliding block bottom, the mounting panel and fixedly connected with rolling disc are extended to the one end of threaded rod, the multiunit is the joint groove of annular distribution on the rolling disc surface, mounting panel surface rotation installs the joint pole of mutually supporting with the joint groove.
As a further scheme of the utility model: buffer gear is including fixed mounting's multiunit slide bar between the control box inner wall, slide bar sliding connection has the control panel, control panel and connecting rod fixed connection, control box inner wall fixed mounting has the buffer spring who encircles slide bar and control panel fixed connection.
As a further scheme of the utility model: steering mechanism is the solid fixed ring that the annular distributes around the control box including unmanned aerial vehicle body diapire fixed mounting, gu fixed ring's inner wall fixed mounting has annular ring gear, control box inner wall fixed mounting has the motor, the spread groove has been seted up to the control box lateral wall of motor one side, the output shaft fixedly connected with transmission fluted disc of motor, the transmission fluted disc passes the spread groove and is connected with the ring gear meshing.
As a still further scheme of the utility model: the damping mechanism comprises a telescopic cavity formed in the bottom of the supporting leg, a damping spring is fixedly mounted in the telescopic cavity, a sliding plate is fixedly connected with the telescopic end of the damping spring, a supporting column is fixedly connected to the surface of the sliding plate, and one end, far away from the sliding plate, of the supporting column extends out of the supporting leg and is fixedly connected with a supporting pad.
Compared with the prior art, the utility model has the beneficial effects that: through setting up by solid fixed ring, the ring gear, including a motor, an end cap, a controller, and a cover plate, the spread groove, the transmission fluted disc, the rotary rod, steering mechanism and the control box that the swivelling chute was constituteed mutually support, can carry out the position at the convenient control camera of flight in-process and adjust, by setting up the slide bar, buffer gear and the damper that buffer spring constitutes mutually support, can take off and land at the unmanned aerial vehicle body, carry out effectual shock attenuation protection to the camera, it can't adjust when using to have solved current unmanned aerial vehicle, it advances and shoots not equidirectional to need control unmanned aerial vehicle to rotate usually, but unmanned aerial vehicle's the rotation in-process shake is great, and stability is relatively poor, and current unmanned aerial vehicle lacks the problem of corresponding protection shock attenuation measure at the in-process of taking off and land.
Drawings
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle surveying and mapping data acquisition device.
Fig. 2 is an enlarged schematic view of a in fig. 1.
Fig. 3 is an enlarged structural diagram of B in fig. 1.
Wherein: unmanned aerial vehicle body 1, supporting leg 2, control box 3, connecting rod 4, mounting panel 5, fixture 6, spout 61, threaded rod 62, sliding block 63, clamping rod 64, rolling disc 65, joint pole 66, joint groove 67, buffer gear 7, slide bar 71, buffer spring 72, steering mechanism 8, solid fixed ring 81, ring gear 82, motor 83, spread groove 84, driving fluted disc 85, rotary rod 86, rotatory groove 87, damper 9, flexible chamber 91, damping spring 92, sliding plate 93, support column 94, supporting pad 95.
Detailed Description
It should be noted that the embodiments and features of the embodiments may be combined with each other without conflict.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.
Specific implementations of the present invention are described in detail below with reference to specific embodiments.
As shown in fig. 1, a structure diagram of an unmanned aerial vehicle surveying and mapping data acquisition device provided for an embodiment of the utility model comprises an unmanned aerial vehicle body 1, wherein support legs 2 are respectively arranged on the periphery of the unmanned aerial vehicle body 1, a control box 3 is rotatably arranged on the bottom wall of the unmanned aerial vehicle body 1, connecting rods 4 extending out of the control box 3 are slidably arranged in the control box 3, a mounting plate 5 is fixedly connected to one end of each of a plurality of groups of connecting rods 4 positioned outside the control box 3, a clamping mechanism 6 is arranged in the mounting plate 5, a buffer mechanism 7 connected with the connecting rods 4 is arranged in the control box 3, a steering mechanism 8 connected with the bottom wall of the unmanned aerial vehicle body 1 is arranged in the control box 3, a damping mechanism 9 is arranged in each support leg 2, and a camera for data acquisition is fixed on the surface of the mounting plate 5 through the clamping mechanism 6 when in use, when unmanned aerial vehicle body 1 was flying in the air, can drive control box 3 through steering mechanism 8 and rotate and then adjust the direction of making a video recording of camera at 1 diapire of unmanned aerial vehicle body, at 1 in-process of taking off and land of unmanned aerial vehicle body, through the damper 9 in the supporting leg 2 and the buffer gear 7 in the control box 3 mutually support, can carry out effectual protection shock attenuation to the camera, avoid the camera to take place to damage.
As shown in fig. 1 and fig. 3, as a preferred embodiment of the present invention, the clamping mechanism 6 includes a long sliding groove 61 formed in the bottom wall of the mounting plate 5, a threaded rod 62 is rotatably mounted in the sliding groove 61, the thread directions of two sides of the threaded rod 62 are opposite, two sets of sliding blocks 63 distributed oppositely are connected to the surface of the threaded rod 62 in a threaded manner, the bottom end of each sliding block 63 extends out of the sliding groove 61 and is fixedly connected to an L-shaped clamping rod 64, one end of the threaded rod 62 extends out of the mounting plate 5 and is fixedly connected to a rotating disc 65, a plurality of sets of clamping grooves 67 distributed annularly are formed in the surface of the rotating disc 65, a clamping rod 66 mutually matched with the clamping grooves 67 is rotatably mounted on the surface of the mounting plate 5, when in use, the rotating disc 65 drives the threaded rod 62 to rotate and further drives the two sets of clamping rods 64 to move relatively through the two sets of sliding blocks 63 distributed oppositely, the two groups of clamping rods 64 move relatively to fix the camera on the surface of the mounting plate 5 stably so as to acquire data in the air.
As shown in fig. 1, as a preferred embodiment of the present invention, the buffering mechanism 7 includes a plurality of sets of sliding rods 71 fixedly installed between inner walls of the control box 3, the sliding rods 71 are slidably connected with a control panel, the control panel is fixedly connected with the connecting rod 4, the inner wall of the control box 3 is fixedly installed with a buffering spring 72 fixedly connected with the control panel around the sliding rods 71, and when in use, the buffering spring 72 and the control panel are matched with each other, so as to effectively reduce impact on the camera caused by the main body 1 of the unmanned aerial vehicle during landing.
As shown in fig. 1 and fig. 2, as a preferred embodiment of the present invention, the steering mechanism 8 includes a fixed ring 81 fixedly mounted on the bottom wall of the main body 1 of the unmanned aerial vehicle and annularly distributed around the control box 3, an annular gear ring 82 is fixedly mounted on an inner wall of the fixed ring 81, a motor 83 is fixedly mounted on an inner wall of the control box 3, a connecting groove 84 is formed on a side wall of the control box 3 on one side of the motor 83, an output shaft of the motor 83 is fixedly connected with a transmission gear disc 85, the transmission gear disc 85 is engaged with the gear ring 82 through the connecting groove 84, a rotating rod 86 is fixedly mounted on the bottom wall of the main body 1 of the unmanned aerial vehicle, a rotating groove 87 slidably connected with the rotating rod 86 is formed on the top wall of the control box 3, when in use, the motor 83 is started to drive the transmission gear disc 85 to rotate, and then drive the control box 3 to rotate through the transmission gear disc 85 being engaged with the gear ring 82, control box 3 is rotatory can be convenient drive the camera and rotate and then carry out data acquisition to different position.
As shown in fig. 1, as a preferred embodiment of the present invention, the damping mechanism 9 includes a telescopic cavity 91 formed at the bottom inside the supporting leg 2, a damping spring 92 is fixedly installed inside the telescopic cavity 91, a sliding plate 93 is fixedly connected to the telescopic end of the damping spring 92, a supporting column 94 is fixedly connected to the surface of the sliding plate 93, and one end of the supporting column 94, which is far away from the sliding plate 93, extends out of the supporting leg 2 and is fixedly connected with a supporting pad 95.
The working principle of the utility model is as follows: when using, fix the camera of data acquisition usefulness on mounting panel 5 surfaces through fixture 6, unmanned aerial vehicle body 1 is when aerial flight, can drive control box 3 through steering mechanism 8 and rotate and then adjust the direction of making a video recording of camera at 1 diapire of unmanned aerial vehicle body, at 1 in-process of taking off and land of unmanned aerial vehicle body, damping mechanism 9 through in the supporting leg 2 and the buffer gear 7 of control box 3 mutually support, can carry out effectual protection shock attenuation to the camera, avoid the camera to take place to damage.
Although the preferred embodiments of the present patent have been described in detail, the present patent is not limited to the above embodiments, and various changes can be made without departing from the spirit of the present patent within the knowledge of those skilled in the art.
Claims (5)
1. The utility model provides an unmanned aerial vehicle survey and drawing data collection system, includes the unmanned aerial vehicle body, the unmanned aerial vehicle body is provided with the supporting leg all around respectively, its characterized in that, unmanned aerial vehicle body diapire rotates installs the control box, slidable mounting has the connecting rod that extends the control box in the control box, the multiunit the connecting rod is located the common fixedly connected with mounting panel of the outer one end of control box, be provided with fixture in the mounting panel, be provided with the buffer gear who is connected with the connecting rod in the control box, install the steering mechanism who is connected with unmanned aerial vehicle body diapire in the control box, be provided with damper in the supporting leg.
2. The unmanned aerial vehicle survey and drawing data collection system of claim 1, characterized in that, fixture includes the spout of the rectangular shape that the mounting panel diapire was seted up, the spout internal rotation is installed the threaded rod, the screw thread opposite direction of threaded rod both sides, threaded rod surface threaded connection has two sets of sliding blocks that distribute relatively, the supporting rod of spout and fixedly connected with L type is extended to the sliding block bottom, the mounting panel and fixedly connected with rolling disc are extended to the one end of threaded rod, the rolling disc surface is seted up the multiunit and is the joint groove of annular distribution, mounting panel surface rotation installs the joint pole of mutually supporting with the joint groove.
3. The device of claim 1, wherein the buffering mechanism comprises a plurality of sets of sliding rods fixedly mounted between inner walls of the control box, the sliding rods are slidably connected with a control panel, the control panel is fixedly connected with the connecting rod, and the inner walls of the control box are fixedly mounted with a buffering spring fixedly connected with the control panel around the sliding rods.
4. The unmanned aerial vehicle survey and drawing data collection system of claim 1, characterized in that steering mechanism includes the solid fixed ring that is the annular distribution around the control box of unmanned aerial vehicle body bottom wall fixed mounting, gu fixed ring's inner wall fixed mounting has annular ring gear, control box inner wall fixed mounting has the motor, the control box lateral wall of motor one side has seted up the spread groove, the output shaft fixedly connected with transmission fluted disc of motor, the transmission fluted disc passes the spread groove and is connected with the ring gear meshing.
5. The unmanned aerial vehicle surveying and mapping data acquisition device according to any one of claims 1-4, wherein the damping mechanism comprises a telescopic cavity formed in the bottom of the support leg, a damping spring is fixedly mounted in the telescopic cavity, a sliding plate is fixedly connected to the telescopic end of the damping spring, a support pillar is fixedly connected to the surface of the sliding plate, and one end of the support pillar, which is far away from the sliding plate, extends out of the support leg and is fixedly connected with a support pad.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123095058.3U CN216233041U (en) | 2021-12-10 | 2021-12-10 | Unmanned aerial vehicle survey and drawing data acquisition device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123095058.3U CN216233041U (en) | 2021-12-10 | 2021-12-10 | Unmanned aerial vehicle survey and drawing data acquisition device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216233041U true CN216233041U (en) | 2022-04-08 |
Family
ID=80961902
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123095058.3U Expired - Fee Related CN216233041U (en) | 2021-12-10 | 2021-12-10 | Unmanned aerial vehicle survey and drawing data acquisition device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216233041U (en) |
-
2021
- 2021-12-10 CN CN202123095058.3U patent/CN216233041U/en not_active Expired - Fee Related
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220408 |
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| CF01 | Termination of patent right due to non-payment of annual fee |