CN210882628U - Assembled unmanned aerial vehicle of surveying of photographic arrangement quick assembly disassembly structure - Google Patents
Assembled unmanned aerial vehicle of surveying of photographic arrangement quick assembly disassembly structure Download PDFInfo
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- CN210882628U CN210882628U CN201921776872.1U CN201921776872U CN210882628U CN 210882628 U CN210882628 U CN 210882628U CN 201921776872 U CN201921776872 U CN 201921776872U CN 210882628 U CN210882628 U CN 210882628U
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- aerial vehicle
- unmanned aerial
- fixedly connected
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- fixed frame
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Abstract
The utility model discloses an unmanned aerial vehicle is surveyed to assembled of photographic arrangement quick assembly disassembly structure, including the unmanned aerial vehicle body, unmanned aerial vehicle body outside fixedly connected with mounting groove, and the inside wing that can dismantle of mounting groove is connected with, the inside swing joint of wing has the movable rod, and movable rod outside fixedly connected with install bin, the inside fixedly connected with driving motor of install bin, and driving motor output fixedly connected with rotor, the fixed frame of unmanned aerial vehicle body upper end fixedly connected with, and the fixed spout of having seted up in unmanned aerial vehicle body upper end, the inside sliding connection of spout has the slider, and slider upper end fixedly connected with compressed particleboard, fixed frame and compressed particleboard swing joint, and the inboard fixedly connected with spring body of fixed frame, the spring body outside fixedly connected with pressure strip. This unmanned aerial vehicle is surveyed to assembled of photographic arrangement quick assembly disassembly structure, the convenience is changed spare part, has increased holistic flexibility, and conveniently carries.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle is surveyed to assembled of photographic arrangement quick assembly disassembly structure.
Background
Compared with a manned airplane, the unmanned aerial vehicle has the advantages of small volume, low manufacturing cost, convenient use, low requirement on the operation environment and the like, and the unmanned aerial vehicle has remarkable function in disaster rescue by the accurate, efficient and flexible reconnaissance and search of the unmanned aerial vehicle,
the chinese patent discloses that its publication number of unmanned aerial vehicle is (201721036775. X), this unmanned aerial vehicle structural design, reasonable in layout, stock solution container and battery are dismantled conveniently, easy to operate, it stops subaerial time to have reduced unmanned aerial vehicle, unmanned aerial vehicle's operating efficiency has been improved, but holistic shape is fixed, holistic flexibility is relatively poor, it is inconvenient to change according to narrow and small topography, holistic practicality has been reduced, and current unmanned aerial vehicle is inconvenient to carry out quick installation and dismantlement to the camera, it is inconvenient to carry out quick replacement to the camera, whole flexibility has been reduced.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle is surveyed to assembled of photographic arrangement quick assembly disassembly structure to it is fixed to provide the holistic shape of unmanned aerial vehicle in solving above-mentioned background art, holistic flexibility is relatively poor, and is inconvenient to change according to narrow and small topography, has reduced holistic practicality, and current unmanned aerial vehicle is inconvenient to install fast and dismantle the camera, and is inconvenient to carry out quick replacement to the camera, has reduced the problem of whole flexibility.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle is surveyed to assembled of photographic arrangement quick assembly disassembly structure, includes the unmanned aerial vehicle body, unmanned aerial vehicle body outside fixedly connected with mounting groove, and the inside wing that can dismantle of mounting groove is connected with, the inside swing joint of wing has the movable rod, and movable rod outside fixedly connected with install bin, the inside fixedly connected with driving motor of install bin, and driving motor output fixedly connected with rotor, the fixed frame of unmanned aerial vehicle body upper end fixedly connected with, and the fixed spout of having seted up in unmanned aerial vehicle body upper end, the inside sliding connection of spout has the slider, and slider upper end fixedly connected with compressed particleboard, fixed frame and compressed particleboard swing joint, and the inboard fixedly connected with spring body of fixed frame, spring body outside fixedly connected with pressure strip, and the pressure strip passes through spring.
Preferably, the upper end of the unmanned aerial vehicle body is provided with a first fixing screw hole, the first fixing screw hole is communicated with the inside of the mounting groove, the rear end of the wing is internally provided with a second fixing screw hole, the specification of the second fixing screw hole is consistent with that of the first fixing screw hole, and the mounting groove and the wing are correspondingly provided with four groups.
Preferably, a first positioning screw hole is formed in the front end of the wing, a second positioning screw hole is formed in the movable rod, the first positioning screw hole and the second positioning screw hole are consistent in specification, and the second positioning screw holes are distributed in the movable rod at equal intervals.
Preferably, positioning clamping grooves are formed in the upper end of the fixing frame and are distributed on the upper end of the fixing frame at equal intervals, and movable grooves are formed in the fixing frame.
Preferably, the inside guide way that has seted up of spout, the slider outside fixedly connected with guide block, and guide block and guide way swing joint.
Preferably, the pressfitting board outside fixedly connected with fly leaf, and fly leaf and activity groove swing joint, the inside swing joint of fly leaf has the spring card button, and spring card button and positioning groove shape size looks adaptation.
Compared with the prior art, the beneficial effects of the utility model are that:
1. according to the assembled detection unmanned aerial vehicle with the rapid disassembly and assembly structure of the photographic device, the wings are connected with the unmanned aerial vehicle body by using screws to penetrate through the first fixing screw holes and the second fixing screw holes, the whole unmanned aerial vehicle is convenient to disassemble and assemble, and the rotor wings are provided with driving motors, so that parts are convenient to replace, the whole flexibility is increased, and the assembled detection unmanned aerial vehicle is convenient to carry;
2. according to the assembled detection unmanned aerial vehicle with the rapid disassembly and assembly structure of the photographic device, the movable rod is used for moving in the wing, so that the distance between the rotor wing and the unmanned aerial vehicle body can be integrally and conveniently adjusted, the overall flexibility is improved, the shape change can be conveniently carried out according to different terrains, and more places can be conveniently detected;
3. this assembled unmanned aerial vehicle of surveying of photographic arrangement quick assembly disassembly structure removes inside fixed frame through using the pressboard to make whole convenience fix the camera of different specifications, and fix through the spring clip button, make wholly can install fast and change under the condition that photographic arrangement goes wrong, increased holistic practicality.
Drawings
FIG. 1 is a schematic perspective view of the present invention;
fig. 2 is a schematic view of the three-dimensional structure of the unmanned aerial vehicle body of the present invention;
FIG. 3 is a schematic view of the wing of the present invention;
fig. 4 is the utility model discloses fixed frame split structure sketch map.
In the figure: 1. an unmanned aerial vehicle body; 2. mounting grooves; 3. an airfoil; 4. a movable rod; 5. installing a box; 6. a drive motor; 7. a rotor; 8. a fixing frame; 9. a chute; 10. a slider; 11. pressing the plywood; 12. a spring body; 13. a compression plate; 14. a first fixing screw hole; 15. a second fixing screw hole; 16. a first positioning screw hole; 17. a second positioning screw hole; 18. positioning the clamping groove; 19. a movable groove; 20. a guide groove; 21. a guide block; 22. a movable plate; 23. the spring is clamped with the button.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: an assembled detection unmanned aerial vehicle with a photographic device quick disassembly and assembly structure comprises an unmanned aerial vehicle body 1, wherein the outer side of the unmanned aerial vehicle body 1 is fixedly connected with a mounting groove 2, the inside of the mounting groove 2 is detachably connected with a wing 3, the inside of the wing 3 is movably connected with a movable rod 4, and the outer side of the movable rod 4 is fixedly connected with a mounting box 5, the interior of the mounting box 5 is fixedly connected with a driving motor 6, and the output end of the driving motor 6 is fixedly connected with a rotor wing 7, the upper end of the unmanned aerial vehicle body 1 is fixedly connected with a fixed frame 8, and the upper end of the unmanned aerial vehicle body 1 is fixedly provided with a chute 9, the chute 9 is connected with a slide block 10 in a sliding way, the upper end of the sliding block 10 is fixedly connected with a pressed plate 11, the fixed frame 8 is movably connected with the pressed plate 11, and fixed frame 8 inboard fixedly connected with spring body 12, spring body 12 outside fixedly connected with pressure strip 13, and pressure strip 13 passes through spring body 12 and fixed frame 8 swing joint.
Further, first fixed screw 14 has been seted up to unmanned aerial vehicle body 1 upper end, and first fixed screw 14 communicates with mounting groove 2 is inside each other, the fixed screw 15 of second has been seted up to 3 rear ends of wing inside, and the fixed screw 15 of second is unanimous with and the 14 specifications of first fixed screw, mounting groove 2 has four groups with the corresponding distribution of wing 3, use the screw to pass first fixed screw 14 and the fixed screw 15 of second and fix, can make the stable installation of wing 3 and unmanned aerial vehicle body 1.
Furthermore, a first positioning screw hole 16 is formed in the front end of the wing 3, a second positioning screw hole 17 is formed in the movable rod 4, the first positioning screw hole 16 and the second positioning screw hole 17 are in the same specification, the second positioning screw holes 17 are distributed in the movable rod 4 at equal intervals, and screws penetrate through the first positioning screw hole 16 and the second positioning screw holes 17 distributed at equal intervals to be fixed, so that the position of the rotor wing 7 can be conveniently adjusted.
Furthermore, a positioning clamping groove 18 is formed in the upper end of the fixing frame 8, the positioning clamping grooves 18 are distributed at the upper end of the fixing frame 8 at equal intervals, a movable groove 19 is formed in the fixing frame 8, and the positioning clamping groove 18 can be clamped with a spring clamping button 23, so that the photographic device is fixed.
Furthermore, a guide groove 20 is formed in the sliding groove 9, a guide block 21 is fixedly connected to the outer side of the sliding block 10, the guide block 21 is movably connected with the guide groove 20, the guide block 21 moves in the guide groove 20, and stability of overall movement can be improved.
Further, the outside of the pressing plate 11 is fixedly connected with a movable plate 22, the movable plate 22 is movably connected with the movable groove 19, the inside of the movable plate 22 is movably connected with a spring clip button 23, the spring clip button 23 is matched with the positioning clip groove 18 in shape and size, and the spring clip button 23 is clamped with different positioning clip grooves 18, so that the whole body can conveniently fix the photographic devices with different specifications.
The working principle is as follows: firstly, the wings 3 and the unmanned aerial vehicle body 1 can be stably installed by fixing the screws through the first fixing screw holes 14 and the second fixing screw holes 15, then the position of the movable rod 4 is adjusted according to actual terrain, the screws penetrate through the first positioning screw holes 16 and are fixed with the second positioning screw holes 17 which are distributed at equal intervals, so that the rotor wings 7 are fixed at different positions to reduce the size of the whole body, the whole body can be conveniently used in narrow terrain, meanwhile, the photographic device is placed in the fixing frame 8, the pressing plate 11 moves in the sliding groove 9 through the movable sliding block 10, so that the pressing plate 11 is close to the photographic device, the guide block 21 moves in the guide groove 20 in the moving process of the pressing plate 11, the stability of the whole body movement can be increased, and meanwhile, the spring clamping button 23 at the upper end of the movable plate 22 is clamped with the positioning clamping groove 18, so that the whole body can fix the photographic device, and the spring body 12 applies pressure to the photographic device through the pressing plate 13, so that the stability of the connection of the photographic device is improved.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an unmanned aerial vehicle is surveyed to assembled of photographic arrangement quick assembly disassembly structure, includes the unmanned aerial vehicle body, its characterized in that: unmanned aerial vehicle body outside fixedly connected with mounting groove, and the inside wing that can dismantle of mounting groove is connected with, the inside swing joint of wing has the movable rod, and the fixed connection of movable rod outside install bin, the inside fixedly connected with driving motor of install bin, and driving motor output fixedly connected with rotor, the fixed frame of unmanned aerial vehicle body upper end fixedly connected with, and the fixed spout of having seted up in unmanned aerial vehicle body upper end, the inside sliding connection of spout has the slider, and slider upper end fixedly connected with pressboard, fixed frame and pressboard swing joint, and the inboard fixedly connected with spring body of fixed frame, spring body outside fixedly connected with pressure strip, and the pressure strip passes through spring body and fixed frame swing joint.
2. The assembled unmanned aerial vehicle for detecting of quick assembly and disassembly structure of photographic device of claim 1, wherein: first fixed screw has been seted up to unmanned aerial vehicle body upper end, and first fixed screw communicates each other with the mounting groove is inside, the fixed screw of second has been seted up to wing rear end inside, and the fixed screw of second and just first fixed screw specification are unanimous, the mounting groove corresponds to the wing and distributes and have four groups.
3. The assembled unmanned aerial vehicle for detecting of quick assembly and disassembly structure of photographic device of claim 1, wherein: the wing is characterized in that a first positioning screw hole is formed in the front end of the wing, a second positioning screw hole is formed in the movable rod, the first positioning screw hole and the second positioning screw hole are in the same specification, and the second positioning screw holes are distributed in the movable rod at equal intervals.
4. The assembled unmanned aerial vehicle for detecting of quick assembly and disassembly structure of photographic device of claim 1, wherein: positioning slot has been seted up to fixed frame upper end, and positioning slot is at fixed frame equidistant distribution in upper end, the movable groove has been seted up to fixed frame inside.
5. The assembled unmanned aerial vehicle for detecting of quick assembly and disassembly structure of photographic device of claim 1, wherein: the inside guide way of having seted up of spout, slider outside fixedly connected with guide block, and guide block and guide way swing joint.
6. The assembled unmanned aerial vehicle for detecting of quick release structure of camera device of claim 4, wherein: the pressfitting board outside fixedly connected with fly leaf, and fly leaf and activity groove swing joint, the inside swing joint of fly leaf has the spring card button, and spring card button and positioning groove shape size looks adaptation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921776872.1U CN210882628U (en) | 2019-10-22 | 2019-10-22 | Assembled unmanned aerial vehicle of surveying of photographic arrangement quick assembly disassembly structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921776872.1U CN210882628U (en) | 2019-10-22 | 2019-10-22 | Assembled unmanned aerial vehicle of surveying of photographic arrangement quick assembly disassembly structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210882628U true CN210882628U (en) | 2020-06-30 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921776872.1U Expired - Fee Related CN210882628U (en) | 2019-10-22 | 2019-10-22 | Assembled unmanned aerial vehicle of surveying of photographic arrangement quick assembly disassembly structure |
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| Country | Link |
|---|---|
| CN (1) | CN210882628U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112874800A (en) * | 2021-04-02 | 2021-06-01 | 劳子路 | Semi-modular unmanned aerial vehicle stores pylon device |
| CN114291257A (en) * | 2022-01-24 | 2022-04-08 | 歌尔科技有限公司 | Unmanned aerial vehicle |
-
2019
- 2019-10-22 CN CN201921776872.1U patent/CN210882628U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112874800A (en) * | 2021-04-02 | 2021-06-01 | 劳子路 | Semi-modular unmanned aerial vehicle stores pylon device |
| CN114291257A (en) * | 2022-01-24 | 2022-04-08 | 歌尔科技有限公司 | Unmanned aerial vehicle |
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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: 20200630 Termination date: 20201022 |
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| CF01 | Termination of patent right due to non-payment of annual fee |