CN220430552U - Unmanned aerial vehicle earthwork measuring device - Google Patents
Unmanned aerial vehicle earthwork measuring device Download PDFInfo
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- CN220430552U CN220430552U CN202320862296.2U CN202320862296U CN220430552U CN 220430552 U CN220430552 U CN 220430552U CN 202320862296 U CN202320862296 U CN 202320862296U CN 220430552 U CN220430552 U CN 220430552U
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- aerial vehicle
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- 230000000694 effects Effects 0.000 claims abstract description 27
- 238000005259 measurement Methods 0.000 claims description 7
- 238000003780 insertion Methods 0.000 claims 1
- 230000037431 insertion Effects 0.000 claims 1
- 238000009434 installation Methods 0.000 abstract description 7
- 230000003014 reinforcing effect Effects 0.000 abstract description 6
- 239000000872 buffer Substances 0.000 description 10
- 238000013507 mapping Methods 0.000 description 5
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 4
- 230000003139 buffering effect Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 3
- 239000007853 buffer solution Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000002457 bidirectional effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
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Abstract
The application discloses unmanned aerial vehicle earthwork measuring device relates to earthwork measuring technical field, including the unmanned aerial vehicle main part, the bottom fixed mounting of unmanned aerial vehicle main part has the mount pad, the bottom of unmanned aerial vehicle main part is provided with the surveying instrument main part, the mounting groove has been seted up to the bottom of mount pad, the surveying instrument main part with the mounting groove activity is pegged graft, the mount pad is located the cavity has all been seted up on the both sides of mounting groove, the mount pad is located the cavity rotation is installed bi-directional screw rod, the equal screw thread in both sides of bi-directional screw rod installs movable inserted block, the slot has all been seted up to the top both sides of unmanned aerial vehicle main part, movable inserted block with slot activity is pegged graft, one side fixed mounting of bi-directional screw rod has the hand wheel, the bottom fixed mounting of unmanned aerial vehicle main part has the bracing piece. An unmanned aerial vehicle earthwork measuring device, simple structure, the surveying instrument installation of being convenient for with dismantle, improve dismouting efficiency, reinforcing practicality.
Description
Technical Field
The application relates to the technical field of earthwork measurement, in particular to an unmanned aerial vehicle earthwork measurement device.
Background
In recent years, with rapid development of national remote sensing and mapping technologies, unmanned aerial vehicle low-altitude photogrammetry technology is gradually applied to the fields of national basic mapping, digital city construction, ecological environment monitoring, national resource management and the like. The unmanned aerial vehicle low-altitude photogrammetry technology has the characteristics of high speed, high efficiency, flexibility, high resolution, high processing speed, low operation cost and the like. And measuring, excavating and backfilling the engineering earthwork by using a novel unmanned aerial vehicle technology.
An existing earth measurement unmanned aerial vehicle device comprises a machine body, a mapping instrument and supporting legs, wherein at least two rotary wings are arranged and fixed on the machine body, as described in patent publication No. CN 210971533U; the surveying instrument is arranged below the machine body through a buffer mechanism; landing leg fixed connection is in the below of organism, including the slope section and with the vertical section of slope section fixed connection, vertical section includes opening decurrent buffer sleeve and buffer base, the opening has been seted up on buffer sleeve's diapire, buffer base includes piston from the top down sets gradually, connecting rod and pedestal, the upper end and the piston fixed connection of connecting rod, the lower extreme and the pedestal fixed connection of connecting rod, the piston setting just with buffer sleeve's lateral wall's internal face sliding seal cooperation in buffer sleeve, the connecting rod stretches out in the opening on the buffer sleeve diapire, the pedestal sets up outside buffer sleeve, the piston encloses into the buffer chamber with buffer sleeve, it has high-pressure gas to fill in the buffer chamber.
To the above related art, the inventor considers that the existing mapping instrument is installed with the unmanned aerial vehicle through a plurality of screws, and the process of the mapping instrument is comparatively loaded down with trivial details when installing or dismantling, wastes time and energy, for this reason, we propose an unmanned aerial vehicle earthwork measuring device.
Disclosure of Invention
The purpose of this application is solved or at least alleviates current surveying instrument and installs through a plurality of screws and unmanned aerial vehicle, and the surveying instrument is comparatively loaded down with trivial details in the process when installation or dismantlement, the problem of wasting time and energy.
In order to achieve the above purpose, the application provides an unmanned aerial vehicle earthwork measuring device, adopts following technical scheme:
the utility model provides an unmanned aerial vehicle earthwork measuring device, includes the unmanned aerial vehicle main part, the bottom fixed mounting of unmanned aerial vehicle main part has the mount pad, the bottom of unmanned aerial vehicle main part is provided with the surveying instrument main part, the mounting groove has been seted up to the bottom of mount pad, the surveying instrument main part with the mounting groove activity is pegged graft, the mount pad is located the cavity has all been seted up to the both sides of mounting groove, the mount pad is located the cavity internal rotation is installed bi-directional screw rod, the equal screw thread installation in both sides of bi-directional screw rod has movable insert, the slot has all been seted up on the top both sides of unmanned aerial vehicle main part, movable insert with slot activity is pegged graft, one side fixed mounting of bi-directional screw rod has the hand wheel, the bottom fixed mounting of unmanned aerial vehicle main part has the bracing piece.
Through adopting above-mentioned technical scheme, through inserting the top of surveying instrument in the mounting groove, through rotating two-way screw rod, make to simulate google activity inserted block and move in opposite directions, insert in the slot, lock the surveying instrument, strengthen the stability of placing of surveying instrument, be convenient for surveying instrument installation and dismantlement, improve dismouting efficiency, reinforcing practicality.
Optionally, the mount pad is located offer the guide way in the cavity, movable insert's top fixed mounting has the guide block, the guide block with guide way sliding connection.
Through adopting above-mentioned technical scheme, through the cooperation of guide block and guide way, play the spacing effect of direction to the removal of movable plug.
Optionally, the holding tank has been seted up to the bottom of bracing piece, the bracing piece is located be provided with the movable rod in the holding tank, the bottom fixed mounting of movable rod has the base, the bottom fixed mounting of bracing piece has the spring, the spring with base fixed connection, the spring is located the outside of movable rod.
Through adopting above-mentioned technical scheme, through being provided with movable rod and spring, play the cushioning effect.
Optionally, the outside cover of spring is equipped with the bellows, the bellows with bracing piece fixed connection, the bottom of bellows with fixed connection between the base.
Through adopting above-mentioned technical scheme, through being provided with the bellows, play the guard action to the spring.
Optionally, the bracing piece is located offer the spout in the holding tank, the side fixed mounting of movable rod has the stopper, the stopper with spout sliding connection.
Through adopting above-mentioned technical scheme, through being provided with the spout, play the effect that the direction was supported to the removal of movable rod.
Optionally, the bracing piece is located the holding tank internal fixation has the gasbag, the gasbag with movable rod butt.
Through adopting above-mentioned technical scheme, through being provided with the gasbag, further play the buffering effect.
Optionally, the bottom fixed mounting of base has the rubber pad, the top fixed mounting of unmanned aerial vehicle main part has the handle.
Through adopting above-mentioned technical scheme, through being provided with the rubber pad, play wear-resisting effect.
Optionally, a fluorescent strip is fixedly adhered to the side end of the unmanned aerial vehicle main body.
Through adopting above-mentioned technical scheme, through being provided with the phosphor strip, be convenient for observe the position of unmanned aerial vehicle main part at night.
In summary, the present application includes the following beneficial effects:
through inserting the mounting groove with the top of surveying instrument in, through rotating bi-directional screw rod, make to simulate google activity inserted block and remove in opposite directions, insert in the slot, lock the surveying instrument, the stability of placing of reinforcing surveying instrument, the surveying instrument installation of being convenient for is with dismantling, improve dismouting efficiency, the reinforcing practicality, through the cooperation of guide block and guide way, play the spacing effect of direction to the removal of activity inserted block, through being provided with movable rod and spring, play cushioning effect, through being provided with the bellows, play guard action to the spring, through being provided with the spout, play the effect that the direction was supported to the removal of movable rod, through being provided with the gasbag, further play buffering effect, through being provided with the rubber pad, play wear-resisting effect, through being provided with the handle, be convenient for mention unmanned aerial vehicle main part, through being provided with the phosphor strip, be convenient for observe the position of unmanned aerial vehicle main part at night.
Drawings
FIG. 1 is a schematic overall structure of the present application;
FIG. 2 is a schematic view of the internal structure of the mounting base of the present application;
FIG. 3 is an enlarged schematic view of the area A in FIG. 2;
fig. 4 is an enlarged schematic view of the area B in fig. 2.
Reference numerals illustrate: 1. an unmanned aerial vehicle main body; 2. a mounting base; 3. a surveying instrument body; 4. a mounting groove; 5. a cavity; 6. a bidirectional screw; 7. a movable plug; 8. a slot; 9. a guide block; 10. a guide groove; 11. a support rod; 12. a receiving groove; 13. a movable rod; 14. a base; 15. a spring; 16. a bellows; 17. a chute; 18. an air bag; 19. a rubber pad; 20. a handle; 21. a fluorescent strip.
Detailed Description
The present application is described in further detail below in conjunction with figures 1-4.
Examples:
the embodiment of the application discloses unmanned aerial vehicle earthwork measuring device. Referring to fig. 1-3, an unmanned aerial vehicle earthwork measuring device, including unmanned aerial vehicle main part 1, the lateral end of unmanned aerial vehicle main part 1 is fixed to bond has phosphor strip 21, through being provided with phosphor strip 21, is convenient for observe the position of unmanned aerial vehicle main part 1 at night. The bottom fixed mounting of unmanned aerial vehicle main part 1 has bracing piece 11.
Referring to fig. 1-3, a receiving groove 12 is formed in the bottom end of a supporting rod 11, the supporting rod 11 is located in the receiving groove 12 and is slidably connected with a movable rod 13, a base 14 is fixedly mounted at the bottom end of the movable rod 13, a spring 15 is fixedly mounted at the bottom end of the supporting rod 11, the spring 15 is fixedly connected with the base 14, and the spring 15 is located on the outer side of the movable rod 13.
Referring to fig. 1-3, a bellows 16 is sleeved on the outer side of the spring 15, the bellows 16 is fixedly connected with the supporting rod 11, the bottom end of the bellows 16 is fixedly connected with the base 14, and the bellows 16 is arranged to protect the spring 15. The supporting rod 11 is positioned in the accommodating groove 12 and provided with a sliding groove 17, a limiting block is fixedly arranged at the side end of the movable rod 13 and is in sliding connection with the sliding groove 17, and the sliding groove 17 plays a role in guiding and supporting the movement of the movable rod 13.
Referring to fig. 1 to 3, the supporting rod 11 is fixedly provided with an air bag 18 in the accommodating groove 12, the air bag 18 is abutted against the movable rod 13, and the air bag 18 is arranged to further play a role in buffering. The bottom fixed mounting of base 14 has rubber pad 19, and unmanned aerial vehicle body 1's top fixed mounting has handle 20, through being provided with rubber pad 19, plays wear-resisting effect.
Referring to fig. 2-4, the bottom fixed mounting of unmanned aerial vehicle main part 1 has mount pad 2, the bottom of unmanned aerial vehicle main part 1 is provided with surveying instrument main part 3, mounting groove 4 has been seted up to the bottom of mount pad 2, surveying instrument main part 3 and the activity of mounting groove 4 are pegged graft, cavity 5 has all been seted up to the both sides that mount pad 2 is located mounting groove 4, mount pad 2 is located cavity 5 internal rotation and installs bi-directional screw rod 6, movable insert 7 is all installed to the equal screw thread in both sides of bi-directional screw rod 6, slot 8 has all been seted up on the top both sides of unmanned aerial vehicle main part 1, movable insert 7 and slot 8 activity peg graft, one side fixed mounting of bi-directional screw rod 6 has the hand wheel, through inserting the top of surveying instrument in mounting groove 4, through rotating bi-directional screw rod 6, make to simulate google activity insert 7 and remove in the slot 8, carry out locking to the surveying instrument, the stability of placing of reinforcing surveying instrument, be convenient for surveying instrument installation and dismantlement, the efficiency of reinforcing practicality.
The mounting seat 2 is positioned in the cavity 5 and is provided with a guide groove 10, the top end of the movable insert block 7 is fixedly provided with a guide block 9, the guide block 9 is in sliding connection with the guide groove 10, and the guide block 9 and the guide groove 10 are matched to play a role in guiding and limiting the movement of the movable insert block 7.
The implementation principle of the unmanned aerial vehicle earthwork measuring device of the embodiment of the application is as follows:
when earthwork is measuring, insert mounting groove 4 through using unmanned aerial vehicle main part 1 with the top of surveying instrument main part 3, through rotating bi-directional screw rod 6, make to simulate google activity inserted block 7 and remove in opposite directions, insert in slot 8, lock the surveying instrument, strengthen the stability of placing of surveying instrument, be convenient for surveying instrument installation and dismantlement, improve dismouting efficiency, strengthen the practicality, survey through surveying instrument main part 3, through the cooperation of guide block 9 and guide way 10, play the spacing effect of direction to the removal of activity inserted block 7, play cushioning effect through being provided with movable rod 13 and spring 15, play the guard action through being provided with bellows 16, play the effect of direction support to the removal of movable rod 13, through being provided with gasbag 18, further play buffering effect, through being provided with rubber pad 19, play wear-resisting effect, through being provided with handle 20, be convenient for mention unmanned aerial vehicle main part 1, through being provided with fluorescent strip 21, be convenient for observe the position of unmanned aerial vehicle main part 1 at night.
The foregoing are all preferred embodiments of the present application, and are not intended to limit the scope of the present application in any way, therefore: all equivalent changes in structure, shape and principle of this application should be covered in the protection scope of this application.
Claims (7)
1. The utility model provides an unmanned aerial vehicle earthwork measuring device, includes unmanned aerial vehicle main part (1), its characterized in that: the utility model discloses a mobile station, including unmanned aerial vehicle main part (1), unmanned aerial vehicle main part (1)'s bottom fixed mounting has mount pad (2), the bottom of unmanned aerial vehicle main part (1) is provided with surveying instrument main part (3), mounting groove (4) have been seted up to the bottom of mount pad (2), surveying instrument main part (3) with mounting groove (4) activity grafting, mount pad (2) are located cavity (5) both sides have all been seted up cavity (5), mount pad (2) are located cavity (5) internal rotation installs bi-directional screw (6), all threaded mounting has movable insert (7) in the both sides of bi-directional screw (6), slot (8) have all been seted up on the top both sides of unmanned aerial vehicle main part (1), movable insert (7) with slot (8) activity grafting, one side fixed mounting of bi-directional screw (6) has the hand wheel, the bottom fixed mounting of unmanned aerial vehicle main part (1) has bracing piece (11), holding groove (12) have been seted up to the bottom of bracing piece (11), bracing piece (11) are located holding groove (12) in holding groove (13) bottom fixed connection spring (14) have base (14), the spring (15) is positioned outside the movable rod (13).
2. The unmanned aerial vehicle earthwork measurement device of claim 1, wherein: the mounting seat (2) is positioned in the cavity (5) and is provided with a guide groove (10), the top end of the movable insertion block (7) is fixedly provided with a guide block (9), and the guide block (9) is in sliding connection with the guide groove (10).
3. The unmanned aerial vehicle earthwork measurement device of claim 1, wherein: the outside cover of spring (15) is equipped with bellows (16), bellows (16) with bracing piece (11) fixed connection, the bottom of bellows (16) with fixed connection between base (14).
4. An unmanned aerial vehicle earthwork measuring device according to claim 3, in which: the supporting rod (11) is positioned in the accommodating groove (12) and provided with a sliding groove (17), a limiting block is fixedly arranged at the side end of the movable rod (13), and the limiting block is in sliding connection with the sliding groove (17).
5. The unmanned aerial vehicle earthwork measuring device of claim 4, in which: the supporting rod (11) is positioned in the accommodating groove (12), an air bag (18) is fixedly arranged in the accommodating groove, and the air bag (18) is abutted to the movable rod (13).
6. The unmanned aerial vehicle earthwork measurement device of claim 1, wherein: the bottom fixed mounting of base (14) has rubber pad (19), the top fixed mounting of unmanned aerial vehicle main part (1) has handle (20).
7. The unmanned aerial vehicle earthwork measurement device of claim 1, wherein: and a fluorescent strip (21) is fixedly adhered to the side end of the unmanned aerial vehicle main body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320862296.2U CN220430552U (en) | 2023-04-15 | 2023-04-15 | Unmanned aerial vehicle earthwork measuring device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320862296.2U CN220430552U (en) | 2023-04-15 | 2023-04-15 | Unmanned aerial vehicle earthwork measuring device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220430552U true CN220430552U (en) | 2024-02-02 |
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ID=89691458
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320862296.2U Active CN220430552U (en) | 2023-04-15 | 2023-04-15 | Unmanned aerial vehicle earthwork measuring device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220430552U (en) |
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2023
- 2023-04-15 CN CN202320862296.2U patent/CN220430552U/en active Active
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