CN220410911U - Unmanned aerial vehicle positioner - Google Patents
Unmanned aerial vehicle positioner Download PDFInfo
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- CN220410911U CN220410911U CN202321501369.1U CN202321501369U CN220410911U CN 220410911 U CN220410911 U CN 220410911U CN 202321501369 U CN202321501369 U CN 202321501369U CN 220410911 U CN220410911 U CN 220410911U
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- aerial vehicle
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- 230000007246 mechanism Effects 0.000 claims abstract description 11
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- 238000010586 diagram Methods 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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- 239000011505 plaster Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle positioning device, which comprises: a support base and a fixing mechanism; the top of the supporting seat is fixedly connected with a fixed clamping block, one side of the fixed clamping block is tightly adhered with a GPS (global positioning system) positioner, one side of the GPS positioner is tightly adhered with a movable clamping block, the bottom of the movable clamping block is movably connected with the supporting seat, one side of the movable clamping block is rotatably connected with a threaded rod, and the outer wall of the threaded rod is in threaded connection with a block body; according to the unmanned aerial vehicle positioning device, the fixing mechanism is arranged on the supporting block, so that the movable clamping block can be driven to clamp the GPS positioner on the fixed clamping block after the threaded rod is screwed up, and when the first binding band and the second binding band are wound on the unmanned aerial vehicle, the inserting block can be driven to be inserted into the slot in a mode of pulling the elastic band, and therefore the inserting rod can be inserted into the through slot to position the inserting block under the reset action of the spring; through the arrangement, the GPS positioner can be conveniently and quickly assembled and disassembled on the unmanned aerial vehicle.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle positioning device.
Background
Unmanned aerial vehicles are well known, and unmanned aerial vehicles are unmanned aerial vehicles operated by using radio remote control equipment and a self-contained program control device and are mainly used for image shooting, topography reconnaissance, safety monitoring and other works.
The problem that current unmanned aerial vehicle leads to being difficult to searching in order to avoid falling off by accident in the sky when using, can supporting installation positioner on unmanned aerial vehicle generally, but current positioner is because carry out the erection joint with unmanned aerial vehicle through connecting piece such as bolt to lead to positioner to be inconvenient for carry out quick assembly disassembly on unmanned aerial vehicle, and then can cause positioner to produce inconveniently when overhauling.
The above information disclosed in the background section is only for enhancement of understanding of the background of the disclosure and therefore it may include information that does not form the prior art that is already known to a person of ordinary skill in the art.
Disclosure of Invention
The utility model aims to provide an unmanned aerial vehicle positioning device for solving the problems in the background technology.
In order to achieve the above purpose, the present utility model provides the following technical solutions: an unmanned aerial vehicle positioning device, comprising: a support base and a fixing mechanism;
the top of the supporting seat is fixedly connected with a fixed clamping block, one side of the fixed clamping block is tightly adhered with a GPS (global positioning system) positioner, one side of the GPS positioner is tightly adhered with a movable clamping block, the bottom of the movable clamping block is movably connected with the supporting seat, one side of the movable clamping block is rotatably connected with a threaded rod, the outer wall of the threaded rod is in threaded connection with a block, and one side of the block is fixedly connected with the supporting seat;
the fixing mechanism comprises a first binding belt and a second binding belt which are respectively and fixedly connected to two sides of a supporting seat, one side of the first binding belt is fixedly connected with an elastic belt through a connecting block, one end of the elastic belt is fixedly connected with an inserting block, a through groove is formed in the inserting block, one side of the second binding belt is fixedly connected with a shell, a slot is formed in the shell, one side of the shell is fixedly connected with a support, an inserting rod is connected to the inner portion of the support in a sliding mode, one end of the inserting rod is fixedly connected with a stop block, a spring is sleeved on the inserting rod, and two ends of the spring are respectively fixedly connected with the stop block and the support.
By adopting the technical scheme, after the GPS positioner is clung to one side of the fixed clamping block, the movable clamping block can be driven to move by screwing the threaded rod, so that the movable clamping block can clamp the GPS positioner, and the GPS positioner can be conveniently dismounted on the supporting seat; in addition, when the GPS locator needs to be fixed on the unmanned aerial vehicle for use, the first binding band and the second binding band can be wound on the unmanned aerial vehicle body, and then the elastic band is pulled, so that the insert block can be inserted into the slot of the shell, and the insert rod can be driven to be inserted into the through slot of the insert block under the reset action of the spring after the stop block is loosened, and then the insert block can be positioned, so that the GPS locator can be fixed on the unmanned aerial vehicle through the supporting seat for use.
Preferably, one side of the outer wall of the inserted link is inserted into the slot and provided with a limit groove.
Through adopting above-mentioned technical scheme, can make the inserted bar insert behind the logical groove, the inserted bar outside can not be rocked any more.
Preferably, one side of the first binding band is fixedly connected with a magic female patch, and one side of the second binding band is fixedly connected with a magic male patch.
Through adopting above-mentioned technical scheme, after first bandage and second bandage are wound up tightly on unmanned aerial vehicle, the magic is sub-to be pasted and is pasted with the magic mother can fix first bandage and second bandage through the mode of adhesion.
Preferably, a sliding groove is formed in one side of the supporting seat, and a sliding block is connected to the inner side wall of the sliding groove in a sliding mode.
By adopting the technical scheme, the sliding block can be more stable in the moving process.
Preferably, one side of the sliding block is fixedly connected with the movable clamping block.
By adopting the technical scheme, the stability of the movable clamping block during movement can be improved.
Preferably, one end of the threaded rod is fixedly connected with a bump.
Through adopting above-mentioned technical scheme, can be convenient for twist the threaded rod.
Preferably, a groove is formed in one side of the protruding block.
Through adopting above-mentioned technical scheme, can be convenient for insert the spanner to the lug inside and operate the threaded rod.
In summary, the present application includes at least one of the following beneficial technical effects:
according to the unmanned aerial vehicle positioning device, the fixing mechanism is arranged on the supporting block, so that the movable clamping block can be driven to clamp the GPS positioner on the fixed clamping block after the threaded rod is screwed up, and when the first binding band and the second binding band are wound on the unmanned aerial vehicle, the inserting block can be driven to be inserted into the slot in a mode of pulling the elastic band, and therefore the inserting rod can be inserted into the through slot to position the inserting block under the reset action of the spring; through the arrangement, the GPS positioner can be conveniently and quickly assembled and disassembled on the unmanned aerial vehicle.
Drawings
Fig. 1 is a schematic structural view of a positioning device for an unmanned aerial vehicle according to the present utility model;
fig. 2 is an enlarged schematic diagram of a region a of a schematic diagram of a structure in the unmanned aerial vehicle positioning device of the present utility model;
fig. 3 is a schematic structural view of a support base and a second strap in the unmanned aerial vehicle positioning device of the present utility model;
fig. 4 is an enlarged schematic view of a region B of a schematic view of a supporting seat and a second strap in the positioning device of the unmanned aerial vehicle of the present utility model.
In the figure: 1. a support base; 10. fixing the clamping blocks; 11. a GPS locator; 12. a movable clamping block; 13. a threaded rod; 14. a block; 15. a chute; 16. a slide block; 17. a bump; 18. a groove; 2. a fixing mechanism; 20. a first strap; 21. a second strap; 22. magic tape; 23. magic mother plaster; 24. a connecting block; 25. an elastic band; 26. inserting blocks; 27. a through groove; 28. a housing; 29. a slot; 201. a bracket; 202. a stop block; 203. a spring; 204. a rod; 205. and a limit groove.
Description of the embodiments
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-4, the present utility model provides a technical solution: an unmanned aerial vehicle positioning device, comprising: a supporting seat 1 and a fixing mechanism 2;
firstly, in order to enable the GPS positioner 11 to be tightly attached to one side of the fixed clamping block 10, the movable clamping block 12 can be driven to move by screwing the threaded rod 13, so that the movable clamping block 12 can clamp the GPS positioner 11, and further the GPS positioner 11 can be conveniently detached and assembled on the supporting seat 1, the fixed clamping block 10 is fixedly connected to the top of the supporting seat 1, the GPS positioner 11 is tightly attached to one side of the fixed clamping block 10, the movable clamping block 12 is tightly attached to one side of the GPS positioner 11, the bottom of the movable clamping block 12 is movably connected with the supporting seat 1, one side of the movable clamping block 12 is rotatably connected with the threaded rod 13, the outer wall of the threaded rod 13 is in threaded connection with the block 14, and one side of the block 14 is fixedly connected with the supporting seat 1; in order to enable the movable clamping block 12 to be more stable in the moving process, a sliding groove 15 is formed in one side of the supporting seat 1, the inner side wall of the sliding groove 15 is connected with a sliding block 16 in a sliding manner, and one side of the sliding block 16 is fixedly connected with the movable clamping block 12; in order to facilitate screwing of the threaded rod 13, one end of the threaded rod 13 is fixedly connected with a lug 17; in order to facilitate the insertion of a wrench into the inside of the lug 17 to operate the threaded rod 13, a groove 18 is formed in one side of the lug 17;
secondly, in order to enable the GPS positioner 11 to be fixed on the unmanned aerial vehicle for use, the first strap 20 and the second strap 21 can be wound on the unmanned aerial vehicle body first, then the elastic band 25 is pulled, the insert block 26 can be inserted into the slot 29 of the housing 28, so that the stop block 202 can be driven to be inserted into the through slot 27 of the insert block 26 under the reset action of the spring 203 after being loosened, the insert block 26 can be positioned, the GPS positioner 11 can be fixed on the unmanned aerial vehicle for use through the supporting seat 1, the fixing mechanism 2 comprises a first strap 20 and a second strap 21 which are respectively and fixedly connected to two sides of the supporting seat 1, one side of the first strap 20 is fixedly connected with the elastic band 25 through the connecting block 24, one end of the elastic band 25 is fixedly connected with the insert block 26, the through slot 27 is formed in the interior of the insert block 26, one side of the second strap 21 is fixedly connected with the housing 28, the slot 29 is formed in the interior of the housing 28, one side of the housing 28 is fixedly connected with the bracket 201, the interior of the bracket 201 is fixedly connected with the insert rod 204, one end 202 of the insert rod 204 is fixedly connected with the spring 204, and the two ends of the bracket 203 are fixedly connected with the stop block 203, and the two ends of the spring 202 are fixedly connected with the stop block 203 respectively; in order to prevent the insert block 26 from shaking outside the insert rod 204 after the insert rod 204 is inserted into the through groove 27, one side of the outer wall of the insert rod 204 is inserted into the slot 29 and provided with a limit groove 205; for the first bandage 20 and the second bandage 21 wind up on unmanned aerial vehicle after, the magic is sub-to be pasted 22 and the female mode of pasting of magic 23 can be fixed first bandage 20 and second bandage 21 through the mode of adhesion, and one side fixedly connected with magic of first bandage 20 is female to be pasted 23, and one side fixedly connected with of second bandage 21 is sub-to be pasted 22.
It should be noted that: the GPS locator 11 is model C6.
According to the technical scheme, the working steps of the scheme are summarized and carded: when the GPS positioning device is used, the GPS positioning device 11 is clung to one side of the fixed clamping block 10, and then the movable clamping block 12 is driven to move in a mode of tightening the threaded rod 13, so that the movable clamping block 12 can clamp the GPS positioning device 11, and the GPS positioning device 11 can be conveniently disassembled and assembled on the supporting seat 1; in addition, when the GPS positioner 11 needs to be fixed on the unmanned aerial vehicle for use, the first strap 20 and the second strap 21 can be wound on the body of the unmanned aerial vehicle, and then the elastic band 25 is pulled, so that the insert block 26 can be inserted into the slot 29 of the housing 28, and the stop block 202 can be loosened to drive the insert rod 204 to be inserted into the through slot 27 of the insert block 26 under the reset action of the spring 203, so that the insert block 26 can be positioned, and the GPS positioner 11 can be fixed on the unmanned aerial vehicle for use through the supporting seat 1; moreover, the insertion rod 204 can be pulled out of the through groove 27 by the stopper 202, and the first strap 20 and the second strap 21 can be easily removed from the unmanned aerial vehicle.
To sum up: according to the unmanned aerial vehicle positioning device, the fixing mechanism 2 is arranged on the supporting block, the movable clamping block 12 can be driven to clamp the GPS positioner 11 on the fixed clamping block 10 after the threaded rod 13 is screwed, and when the first binding band 20 and the second binding band 21 are wound on the unmanned aerial vehicle, the inserting block 26 can be driven to be inserted into the slot 29 by pulling the elastic band 25, so that the inserting rod 204 can be inserted into the through slot 27 to position the inserting block 26 under the reset action of the spring 203; through the above arrangement, the GPS positioner 11 can be conveniently and quickly assembled and disassembled on the unmanned aerial vehicle.
None of the utility models are related to the same or are capable of being practiced in the prior art. Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. An unmanned aerial vehicle positioner, characterized by comprising: a supporting seat (1) and a fixing mechanism (2);
the top of the supporting seat (1) is fixedly connected with a fixed clamping block (10), one side of the fixed clamping block (10) is tightly adhered with a GPS (global positioning system) positioner (11), one side of the GPS positioner (11) is tightly adhered with a movable clamping block (12), the bottom of the movable clamping block (12) is movably connected with the supporting seat (1), one side of the movable clamping block (12) is rotatably connected with a threaded rod (13), the outer wall of the threaded rod (13) is in threaded connection with a block body (14), and one side of the block body (14) is fixedly connected with the supporting seat (1);
the utility model provides a fixing mechanism (2) is including first bandage (20) and second bandage (21) of fixed connection on supporting seat (1) both sides respectively, one side of first bandage (20) is through connecting block (24) fixedly connected with elastic band (25), the one end fixedly connected with inserted block (26) of elastic band (25), logical groove (27) have been seted up to the inside of inserted block (26), one side fixedly connected with casing (28) of second bandage (21), slot (29) have been seted up to the inside of casing (28), one side fixedly connected with support (201) of casing (28), the inside sliding connection of support (201) has inserted bar (204), one end fixedly connected with dog (202) of inserted bar (204), the cover is equipped with spring (203) on inserted bar (204), the both ends of spring (203) are respectively with dog (202) and support (201) fixed connection.
2. The unmanned aerial vehicle positioning device of claim 1, wherein: one side of the outer wall of the inserted link (204) is inserted into the slot (29) and provided with a limit groove (205).
3. The unmanned aerial vehicle positioning device of claim 1, wherein: one side of the first binding band (20) is fixedly connected with a magic female patch (23), and one side of the second binding band (21) is fixedly connected with a magic child patch (22).
4. The unmanned aerial vehicle positioning device of claim 1, wherein: a sliding groove (15) is formed in one side of the supporting seat (1), and a sliding block (16) is connected to the inner side wall of the sliding groove (15) in a sliding mode.
5. The unmanned aerial vehicle positioning device of claim 4, wherein: one side of the sliding block (16) is fixedly connected with the movable clamping block (12).
6. The unmanned aerial vehicle positioning device of claim 1, wherein: one end of the threaded rod (13) is fixedly connected with a lug (17).
7. The unmanned aerial vehicle positioning device of claim 6, wherein: a groove (18) is formed in one side of the protruding block (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321501369.1U CN220410911U (en) | 2023-06-13 | 2023-06-13 | Unmanned aerial vehicle positioner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321501369.1U CN220410911U (en) | 2023-06-13 | 2023-06-13 | Unmanned aerial vehicle positioner |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220410911U true CN220410911U (en) | 2024-01-30 |
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ID=89640310
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321501369.1U Active CN220410911U (en) | 2023-06-13 | 2023-06-13 | Unmanned aerial vehicle positioner |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220410911U (en) |
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2023
- 2023-06-13 CN CN202321501369.1U patent/CN220410911U/en active Active
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