CN219809677U - Engineering investigation mapping instrument based on satellite positioning system - Google Patents
Engineering investigation mapping instrument based on satellite positioning system Download PDFInfo
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- CN219809677U CN219809677U CN202321163534.7U CN202321163534U CN219809677U CN 219809677 U CN219809677 U CN 219809677U CN 202321163534 U CN202321163534 U CN 202321163534U CN 219809677 U CN219809677 U CN 219809677U
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- groove
- rod
- satellite positioning
- positioning system
- sliding
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- 238000013507 mapping Methods 0.000 title claims abstract description 17
- 238000011835 investigation Methods 0.000 title abstract description 10
- 239000003550 marker Substances 0.000 claims description 13
- 206010039203 Road traffic accident Diseases 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000007306 turnover Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/30—Assessment of water resources
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- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The utility model relates to the technical field of satellite positioning engineering investigation mapping instruments and discloses an engineering investigation mapping instrument based on a satellite positioning system, which comprises a loading table, wherein a placing groove is formed in one side above the loading table, a sliding mechanism is arranged at the bottom of an inner cavity of the placing groove, the sliding mechanism comprises a sliding groove and a sliding block, the sliding groove is formed in the bottom of the inner cavity of the placing groove, the sliding block is slidably arranged in the inner cavity of the sliding groove, and a supporting rod is arranged in the inner cavity of one side of the placing groove. According to the utility model, the electric push rod is controlled by the controller to push the sliding block in the sliding mechanism to move, so that the movable rod movably mounted on one side wall of the sliding block can pull or push the supporting rod to move, the supporting rod can move under the cooperation of the rotating mechanism, and the situation that the supporting rod is not dropped and reset is ensured by the movable rod, so that the upper profile recognition camera falls into the sliding mechanism, and the sliding mechanism is more practical and suitable for wide popularization and use.
Description
Technical Field
The utility model belongs to the technical field of satellite positioning engineering investigation mapping instruments, and particularly relates to an engineering investigation mapping instrument based on a satellite positioning system.
Background
In the engineering construction process, the original survey and mapping result cannot be suitable for the subsequent construction due to factors such as construction errors, accidents (such as settlement and collapse) and the like on site, so that the site needs to be surveyed and mapped again, and in order to improve the efficiency, some survey and positioning systems are based on satellite positioning and are integrally mounted on movable equipment such as vehicles.
In the prior art, as CN207050725U, a satellite-based vehicle-mounted traffic accident scene survey positioning system is disclosed, which comprises a loading platform provided with a radar, a profile marker storage tank and an aircraft tank, a profile recognition camera, a profile marker, an aircraft with a camera mounting seat and a system controller; the profile recognition camera is detachably mounted on the loading table through a turnover supporting rod, and the profile recognition camera shell is also provided with a mounting groove for being fixed on an aircraft camera mounting seat; the system controller is used for controlling and communicating all components through control lines, and the satellite-based vehicle-mounted traffic accident scene investigation positioning system can be arranged on a vehicle, is convenient to quickly arrive at an accident scene, can complete investigation and mapping on the scene in real time through an image contour recognition technology and can complete positioning and transmission through a satellite system.
But the present inventors have found that this technical solution still has at least the following drawbacks:
according to the satellite-based vehicle-mounted traffic accident scene investigation positioning system, the overturning support rod is matched with the groove formed above the loading table, but is in a vertical state after overturning, and is not provided with a supporting mechanism, so that the overturning support rod is easily subjected to some external force, namely, is directly reset, and the profile identification camera above is directly dropped into the groove, so that damage is caused.
The present utility model has been made in view of this.
Disclosure of Invention
In order to solve the technical problem that in the prior art, a turnover supporting rod is in a vertical state after being turned and is not provided with a supporting mechanism, the basic conception of the technical scheme adopted by the utility model is as follows:
engineering reconnaissance mapping appearance based on satellite positioning system, including loading the platform, the standing groove has been seted up to loading platform top one side, and standing groove inner chamber bottom is provided with slide mechanism, slide mechanism includes spout and slider, the spout is seted up in standing groove inner chamber bottom, and spout inner chamber slidable mounting has the slider, one side inner chamber of standing groove is provided with the bracing piece, and the bracing piece is close to slide mechanism's a side wall movable mounting has the movable rod, and movable rod other end swing joint is on the slider, be provided with electric putter in the spout, and the electric putter other end is connected in the slider. The electric putter is controlled through the controller to remove because the slider in sliding mechanism is fixed to the electric putter other end to make the slider remove, and because slider a lateral wall is swing joint has the movable rod, and the movable rod other end is swing joint in bracing piece a lateral wall, thereby make the slider at the in-process that removes, can rotate under the assistance of rotary rod in the rotation mechanism through movable rod drive bracing piece this moment, thereby make the bracing piece can keep away from the standing groove, make when needing the profile identification camera to work, the bracing piece can receive a holding power this moment, guarantee that it can not appear the condition that drops.
As a preferable implementation mode of the utility model, a universal joint is respectively arranged on one side wall of the sliding block opposite to the supporting rod, and two ends of the movable rod are respectively clamped in the universal joint. The movable rod is ensured to be capable of changing the angle.
As a preferred embodiment of the utility model, the supporting rod is fixedly arranged on the rotating mechanism, the rotating mechanism comprises two mutually symmetrical bearings, the two mutually symmetrical bearings are respectively and fixedly arranged on two opposite side walls of the placing groove, the two bearings are respectively internally and fixedly provided with the rotating rod in a clamping way, and the supporting rod is fixedly arranged on the rotating rod. The support rod is driven by the movable rod to rotate under the assistance of the rotating rod in the rotating mechanism, so that the support rod can be far away from the placing groove.
As a preferable implementation mode of the utility model, the loading platform is provided with a contour marker groove and an aircraft groove on one side of the placing groove, the inner cavity of the contour marker groove is provided with a contour marker, and the aircraft groove is provided with an unmanned aerial vehicle. The placement positions of the drone and the profile marker are determined.
In a preferred embodiment of the present utility model, a radar is disposed at an upper end of the loading platform, and the loading platform is wirelessly connected to the controller. It is ensured that it can be detected by the satellite and thus operated.
As a preferred embodiment of the present utility model, an end of the support rod remote from the rotation mechanism is provided with a contour recognition camera. The mounting position of the contour recognition camera is determined.
Compared with the prior art, the utility model has the following beneficial effects:
according to the utility model, the electric push rod is controlled by the controller to push the sliding block in the sliding mechanism to move, so that the movable rod movably mounted on one side wall of the sliding block can pull or push the supporting rod to move, the supporting rod can move under the cooperation of the rotating mechanism, and the situation that the sliding rod is not dropped and reset is ensured by the movable rod, so that the upper contour recognition camera falls into the sliding rod.
The following describes the embodiments of the present utility model in further detail with reference to the accompanying drawings.
Drawings
In the drawings:
FIG. 1 is a schematic side view of an engineering survey mapper based on a satellite positioning system;
FIG. 2 is a schematic perspective view of an engineering survey mapper based on a satellite positioning system;
FIG. 3 is a schematic view of the local structure of the engineering survey mapper A based on the satellite positioning system;
fig. 4 is a schematic view of the local structure of the B site of the engineering survey mapper based on the satellite positioning system.
In the figure: 1. a loading table; 2. a placement groove; 3. a profile identifier slot; 4. a profile identifier; 5. a radar; 6. an aircraft slot; 7. a support rod; 8. a controller; 9. a contour recognition camera; 10. a chute; 11. a bearing; 12. a rotating rod; 13. a slide block; 14. a universal joint; 15. a movable rod; 16. an electric push rod.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present utility model more apparent, the technical solutions in the embodiments will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model, and the following embodiments are used to illustrate the present utility model.
As shown in fig. 1 to 4, an engineering investigation mapping instrument based on a satellite positioning system comprises a loading table 1, a placing groove 2 is formed in one side above the loading table 1, a sliding mechanism is arranged at the bottom of an inner cavity of the placing groove 2, the sliding mechanism comprises a sliding groove 10 and a sliding block 13, the sliding groove 10 is formed in the bottom of the inner cavity of the placing groove 2, the sliding block 13 is slidably mounted in the inner cavity of the sliding groove 10, a supporting rod 7 is arranged in one side inner cavity of the placing groove 2, the supporting rod 7 is close to a movable rod 15 movably mounted on one side wall of the sliding mechanism, the other end of the movable rod 15 is movably connected to the sliding block 13, an electric push rod 16 is arranged in the sliding groove 10, and the other end of the electric push rod 16 is connected to the sliding block 13. The electric push rod 16 is controlled to move through the controller 8, because the other end of the electric push rod 16 is fixedly connected with the sliding block 13 in the sliding mechanism, the sliding block 13 can move, and because one side wall of the sliding block 13 is movably connected with the movable rod 15, the other end of the movable rod 15 is movably connected with one side wall of the supporting rod 7, so that the sliding block 13 can rotate under the assistance of the rotating rod 12 in the rotating mechanism through the movable rod 15 at the moment when the sliding block 13 moves, the supporting rod 7 can be far away from the placing groove 2, and the supporting rod 7 can be supported by a supporting force when the contour recognition camera 9 is required to work, so that falling can be prevented.
As shown in fig. 1 to 3, in the specific embodiment, a side wall of the slider 13 opposite to the support rod 7 is respectively provided with a universal joint 14, and two ends of the movable rod 15 are respectively clamped in the universal joint 14. In this arrangement, it is ensured that the movable lever 15 is capable of angular variation.
As shown in fig. 1 to 3, further, the supporting rod 7 is fixedly mounted on the rotating mechanism, the rotating mechanism comprises two mutually symmetrical bearings 11, the two mutually symmetrical bearings 11 are respectively fixedly mounted on two opposite side walls of the placement groove 2, the two bearings 11 are respectively internally clamped with a rotating rod 12, and the supporting rod 17 is fixedly mounted on the rotating rod 12. In this setting, the support bar 7 is driven by the movable bar 15 to rotate with the aid of the rotating bar 12 in the rotating mechanism, so that the support bar 7 can be far away from the placement groove 2.
As shown in fig. 1 to 3, further, a profile marker groove 3 and an aircraft groove 6 are formed in one side of the placement groove 2 of the loading platform 1, a profile marker 4 is placed in an inner cavity of the profile marker groove 3, and an unmanned aerial vehicle is placed in the aircraft groove 6. In this arrangement the placement position of the drone and the profile marker 4 is determined.
As shown in fig. 1 to 3, further, a radar 5 is disposed at one end above the loading table 1, and the loading table 1 is wirelessly connected to a controller 8. In this setting, it has been guaranteed that it can detect through the satellite to operate.
As shown in fig. 1 to 3, further, the end of the support rod 7 remote from the rotation mechanism is provided with a contour recognition camera 9. In this setting, the installation position of the contour recognition camera 9 is determined.
The implementation principle of the engineering survey and mapping instrument based on the satellite positioning system in this embodiment is as follows: firstly, the electric push rod 16 is controlled to move through the controller 8, because the other end of the electric push rod 16 is fixedly connected with the sliding block 13 in the sliding mechanism, the sliding block 13 can move, and because one side wall of the sliding block 13 is movably connected with the movable rod 15, the other end of the movable rod 15 is movably connected with one side wall of the supporting rod 7, so that the sliding block 13 can rotate under the assistance of the rotating rod 12 in the rotating mechanism through the movable rod 15 at the moment, the supporting rod 7 can be far away from the placing groove 2, and when the contour recognition camera 9 is required to work, the supporting rod 7 can be subjected to a supporting force, and the falling condition of the supporting rod is guaranteed not to occur.
Claims (6)
1. Engineering reconnaissance mapping appearance based on satellite positioning system, including loading the platform, its characterized in that, loading platform top one side has seted up the standing groove, and standing groove inner chamber bottom is provided with slide mechanism, slide mechanism includes spout and slider, the spout sets up in standing groove inner chamber bottom, and spout inner chamber slidable mounting has the slider, one side inner chamber of standing groove is provided with the bracing piece, and the bracing piece is close to slide mechanism's a side wall movable mounting has the movable rod, and the movable rod other end swing joint is on the slider, be provided with electric putter in the spout, and the electric putter other end is connected in the slider.
2. The engineering survey and mapping instrument based on the satellite positioning system according to claim 1, wherein a universal joint is respectively arranged on one side wall of the sliding block opposite to the supporting rod, and two ends of the movable rod are respectively clamped in the universal joint.
3. The satellite positioning system-based engineering survey and mapping instrument according to claim 1, wherein the support rod is fixedly mounted on the rotating mechanism, the rotating mechanism comprises two mutually symmetrical bearings, the two mutually symmetrical bearings are respectively and fixedly mounted on two opposite side walls of the placing groove, the two bearings are respectively internally and fixedly mounted with a rotating rod in a clamping manner, and the support rod is fixedly mounted on the rotating rod.
4. The satellite positioning system-based engineering survey and mapping instrument of claim 1, wherein the loading platform is provided with a contour marker groove and an aircraft groove on one side of the placement groove, a contour marker is placed in an inner cavity of the contour marker groove, and an unmanned aerial vehicle is placed in the aircraft groove.
5. The satellite positioning system-based engineering survey and mapping instrument of claim 4, wherein the radar is disposed at an upper end of the loading platform, and the loading platform is wirelessly connected to the controller.
6. A satellite positioning system based engineering survey and mapping instrument according to claim 3, wherein the end of the support bar remote from the rotation mechanism is provided with a profile recognition camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321163534.7U CN219809677U (en) | 2023-05-15 | 2023-05-15 | Engineering investigation mapping instrument based on satellite positioning system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321163534.7U CN219809677U (en) | 2023-05-15 | 2023-05-15 | Engineering investigation mapping instrument based on satellite positioning system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219809677U true CN219809677U (en) | 2023-10-10 |
Family
ID=88217290
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321163534.7U Active CN219809677U (en) | 2023-05-15 | 2023-05-15 | Engineering investigation mapping instrument based on satellite positioning system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219809677U (en) |
-
2023
- 2023-05-15 CN CN202321163534.7U patent/CN219809677U/en active Active
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