CN220518611U - Lightweight unmanned aerial vehicle flight platform - Google Patents
Lightweight unmanned aerial vehicle flight platform Download PDFInfo
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- CN220518611U CN220518611U CN202322066703.1U CN202322066703U CN220518611U CN 220518611 U CN220518611 U CN 220518611U CN 202322066703 U CN202322066703 U CN 202322066703U CN 220518611 U CN220518611 U CN 220518611U
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- 230000035939 shock Effects 0.000 claims description 10
- 230000000694 effects Effects 0.000 abstract description 11
- 238000000034 method Methods 0.000 description 8
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 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 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a lightweight unmanned aerial vehicle flight platform, which relates to the technical field of unmanned aerial vehicle flight platforms, and particularly relates to a lightweight unmanned aerial vehicle flight platform. This lightweight unmanned aerial vehicle flight platform, through the setting of crane, make this lightweight unmanned aerial vehicle flight platform possess and be convenient for adjust its height to the screw is difficult to strike the object and leads to unmanned aerial vehicle damage's effect around when making unmanned aerial vehicle drop, thereby has played not fragile unmanned aerial vehicle's effect, has reached the stronger purpose of practicality.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle flight platforms, in particular to a lightweight unmanned aerial vehicle flight platform.
Background
Unmanned plane is called unmanned plane for short and can carry out the project such as aerial photography, resource investigation, patrol, delivery relief of disaster material, and its demand in social life is higher and higher, and along with the popularization of aircraft attitude control system and aerospace technique, unmanned plane of various sizes gradually gets into civilian market.
In the prior art, due to the fact that the height of a flight base of the unmanned aerial vehicle multifunctional flight platform is not easy to adjust, a propeller is easy to strike on surrounding objects when the unmanned aerial vehicle takes off, the unmanned aerial vehicle is easy to damage, the practicability is poor, and in addition, in the existing process, especially, the landing gear of the unmanned aerial vehicle can be subjected to large impact force, and then the landing gear of the unmanned aerial vehicle is damaged, so that the phenomenon that the normal service lives of the unmanned aerial vehicle and the landing gear are generally short occurs is caused, and the unmanned aerial vehicle multifunctional flight platform is inconvenient to use.
Disclosure of Invention
(one) solving the technical problems
Aiming at the defects of the prior art, the utility model provides a lightweight unmanned aerial vehicle flight platform, which solves the problems in the background art.
(II) technical scheme
In order to achieve the above purpose, the utility model is realized by the following technical scheme: the utility model provides a lightweight unmanned aerial vehicle flight platform, includes the base, the top fixed mounting of base has the fixed column, the outside fixed mounting of fixed column has the swivel ring, the outside fixed mounting of swivel ring has first support, one side of first support rotates and is connected with the second support, the top of base is provided with the crane, the bottom fixed mounting of crane has the connecting seat, the top of second support rotates to be connected in the bottom of connecting seat, the outside fixed mounting of swivel ring has electric telescopic handle, electric telescopic handle's the fixed mounting that stretches out has the propelling movement seat, the one end of propelling movement seat rotates to be connected in one side of second support, one side fixed mounting of bottom of crane has the slide rail, the inside sliding connection of slide rail has the sliding seat, one end of first support rotates to be connected in one side of sliding seat, the top sliding connection of base has the movable seat, the inside fixed mounting of movable seat has the support column, the other end of second support rotates to be connected in the top of movable seat, threaded hole has been seted up at the top of crane, threaded hole's internal thread connection has the bolt.
Optionally, the outside of bolt is provided with the mounting panel, the top fixed mounting of mounting panel has the platform base.
Optionally, the lifting groove is formed in the platform base, and the lifting plate is connected to the lifting groove in a sliding mode.
Optionally, a shock absorber is fixedly installed at the bottom of the lifting plate, and the bottom of the shock absorber is fixedly installed at the inner bottom wall of the lifting groove.
Optionally, a lifting column is fixedly installed at the top of the lifting plate, and a platform body is fixedly installed at the top of the lifting column.
Optionally, the number of the platform bodies is two, and the two platform bodies are rotationally connected through a hinge.
Optionally, the expansion tank has been seted up to the one end of fixed column, the inside sliding connection in expansion tank has the expansion column.
Optionally, the number of the base is two, and the other end of the telescopic column is fixedly arranged at one side of the other base.
(III) beneficial effects
The utility model provides a lightweight unmanned aerial vehicle flight platform, which has the following beneficial effects:
1. this lightweight unmanned aerial vehicle flight platform, through the setting of crane, make this lightweight unmanned aerial vehicle flight platform possess and be convenient for adjust its height, and the screw is difficult to strike the object around and lead to the effect of unmanned aerial vehicle damage when making unmanned aerial vehicle drop, through the fixed column, first support, the second support, the crane, the slide rail, electric telescopic handle, the sliding seat, the cooperation setting of movable seat and support column, can open electric telescopic handle when needs adjust its height in the in-process of using, electric telescopic handle's the end of stretching out can drive the second support motion through the propelling movement seat, the second support can drive first support motion, electric telescopic handle's bottom can drive the outward movement of swivel ring at the fixed column simultaneously, and the top of second support can drive the sliding seat at the inside slip of slide rail, the top of first support can take place the motion in the bottom of connecting seat simultaneously, and then make the crane can upward movement, the bottom of second support can drive the movable seat and can drive the motion support column, and then make whole lift in-process more steady when needing to adjust its height, thereby the effect of unmanned aerial vehicle is not fragile has been reached.
2. This lightweight unmanned aerial vehicle flight platform, through the setting of bumper shock absorber, make this lightweight unmanned aerial vehicle flight platform possess the in-process of descending, unmanned aerial vehicle's undercarriage can not receive very big impact force, and then can not easily cause the damage to unmanned aerial vehicle's undercarriage, and be convenient for fold it, and then the effect of convenient transport, through the mounting panel, the bolts, a pedestal, the lift groove, the lifter plate, the bumper shock absorber, the lifter post, the cooperation setting of platform body and telescopic column, can be when unmanned aerial vehicle falls at flight platform in the in-process of use, unmanned aerial vehicle's opportunity is through the undercarriage downward pressure flight platform, flight platform can drive lifter post downward movement, the lifter plate can drive the inside downward movement of lifter plate at the lift groove, the lifter plate can be downward pressure to move the bumper shock absorber, and the impact force that can absorb, and then make unmanned aerial vehicle more steady descends at flight platform's surface, when needs to fold it, the one end of messenger's bolt breaks away from the inside of screw hole, then move flight platform passes through the hinge and folds one side at the base, the base can drive the motion, the telescopic column can be driven at the telescopic column, the telescopic column has been stretched out and the telescopic column has reached convenient for use, and has reached the convenient use.
Drawings
FIG. 1 is a schematic view of a three-dimensional structure of the present utility model;
FIG. 2 is a schematic illustration of the structure of the equal side of the present utility model;
FIG. 3 is a schematic view of a folded structure of the present utility model;
FIG. 4 is a schematic view of the folded cross-section of the present utility model;
FIG. 5 is an enlarged schematic view of the structure of FIG. 2A according to the present utility model;
FIG. 6 is a schematic view of the structure of the present utility model with the base in cross section;
FIG. 7 is an enlarged schematic view of the structure of FIG. 1B according to the present utility model;
fig. 8 is an enlarged schematic view of the structure of fig. 2C according to the present utility model.
In the figure: 1. a base; 2. fixing the column; 3. a first bracket; 4. a second bracket; 5. a lifting frame; 501. a slide rail; 6. an electric telescopic rod; 7. a sliding seat; 8. a movable seat; 9. a support column; 10. a mounting plate; 11. a bolt; 12. a platform base; 13. a lifting groove; 14. a lifting plate; 15. a damper; 16. lifting columns; 17. a platform body; 18. and (5) a telescopic column.
Detailed Description
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.
Example 1
Referring to fig. 1 to 5, the present utility model provides the following technical solutions: the utility model provides a lightweight unmanned aerial vehicle flight platform, the on-line screen storage device comprises a base 1, the top fixed mounting of base 1 has fixed column 2, the outside fixed mounting of fixed column 2 has the swivel ring, the outside fixed mounting of swivel ring has first support 3, one side rotation of first support 3 is connected with second support 4, the top of base 1 is provided with crane 5, the bottom fixed mounting of crane 5 has the connecting seat, the top of second support 4 rotates the bottom of connecting seat to be connected, the outside fixed mounting of swivel ring has electric telescopic handle 6, electric telescopic handle 6 stretches out and fixes and has the propelling movement seat, the one end of propelling movement seat rotates to be connected in one side of second support 4, the bottom one side fixed mounting of crane 5 has slide rail 501, the inside sliding connection of slide rail 501 has slide seat 7, the one end of first support 3 rotates to be connected in one side of slide seat 7, the top sliding connection of base 1 has movable seat 8, the inside fixed mounting of movable seat 8 has support column 9, the other end rotation of second support 4 is connected in the top of movable seat 8, threaded hole is seted up at the top of crane 5, threaded hole's internal thread connection has 11, the inside screw thread connection has the 11, the inside 10 is provided with the mounting plate 12 at the inside of lift plate 13, the fixed mounting plate 13 of bottom of lift plate 13 fixed mounting plate 13, the fixed mounting plate 13 is provided with the bottom of two fixed mounting plate 13, the fixed mounting plate 13 fixed platform of bottom 17 is arranged at the bottom of jack-up through the fixed slot of jack-up, the fixed platform 17, the fixed platform is fixed platform 17 is fixed bottom of jack-up 13, the fixed platform is arranged at the top of jack-up 13, the fixed platform is mounted 13, the inside of the inside is mounted 13 is mounted through the inside is connected with the jack-up through the jack-up 13, the jack-up has the jack-down has the jack 9, the jack-box has and has the jack 9, the jack has and has the jack 9, the inside sliding connection in flexible groove has flexible post 18, and the quantity of base 1 is two, and the other end fixed mounting of flexible post 18 has one side at another base 1, through the setting of crane 5, makes this lightweight unmanned aerial vehicle flight platform possess and is convenient for adjust its height to the screw is difficult to strike the object and leads to unmanned aerial vehicle damage's effect around when making unmanned aerial vehicle drop, thereby has played the effect of not fragile unmanned aerial vehicle, has reached the stronger purpose of practicality.
When in use, when the height of the electric telescopic rod is required to be adjusted, the electric telescopic rod 6 is opened, the extending end of the electric telescopic rod 6 can drive the second support 4 to move through the pushing seat, the second support 4 can drive the first support 3 to move, meanwhile, the bottom of the electric telescopic rod 6 can drive the rotating ring to move outside the fixed column 2, the top of the second support 4 can drive the sliding seat 7 to slide in the sliding rail 501, meanwhile, the top of the first support 3 can move at the bottom of the connecting seat, the lifting frame 5 can move upwards, meanwhile, the bottom of the second support 4 can drive the movable seat 8 to move at the top of the base 1, the movable seat 8 can drive the supporting column 9 to move, and the whole lifting process is stable, so that the effect of a unmanned aerial vehicle which is not easy to damage is achieved, and the purpose of high practicability is achieved.
Example 2
Referring to fig. 1 to 8, the present utility model provides the following technical solutions: the utility model provides a lightweight unmanned aerial vehicle flight platform, the on-line screen storage device comprises a base 1, the top fixed mounting of base 1 has fixed column 2, the outside fixed mounting of fixed column 2 has the swivel ring, the outside fixed mounting of swivel ring has first support 3, one side rotation of first support 3 is connected with second support 4, the top of base 1 is provided with crane 5, the bottom fixed mounting of crane 5 has the connecting seat, the top of second support 4 rotates the bottom of connecting seat to be connected, the outside fixed mounting of swivel ring has electric telescopic handle 6, electric telescopic handle 6 stretches out and fixes and has the propelling movement seat, the one end of propelling movement seat rotates to be connected in one side of second support 4, the bottom one side fixed mounting of crane 5 has slide rail 501, the inside sliding connection of slide rail 501 has slide seat 7, the one end of first support 3 rotates to be connected in one side of slide seat 7, the top sliding connection of base 1 has movable seat 8, the inside fixed mounting of movable seat 8 has support column 9, the other end rotation of second support 4 is connected in the top of movable seat 8, threaded hole is seted up at the top of crane 5, threaded hole's internal thread connection has 11, the inside screw thread connection has the 11, the inside 10 is provided with the mounting plate 12 at the inside of lift plate 13, the fixed mounting plate 13 of bottom of lift plate 13 fixed mounting plate 13, the fixed mounting plate 13 is provided with the bottom of two fixed mounting plate 13, the fixed mounting plate 13 fixed platform of bottom 17 is arranged at the bottom of jack-up through the fixed slot of jack-up, the fixed platform 17, the fixed platform is fixed platform 17 is fixed bottom of jack-up 13, the fixed platform is arranged at the top of jack-up 13, the fixed platform is mounted 13, the inside of the inside is mounted 13 is mounted through the inside is connected with the jack-up through the jack-up 13, the jack-up has the jack-down has the jack 9, the jack-box has and has the jack 9, the jack has and has the jack 9, the inside sliding connection in flexible groove has flexible post 18, and the quantity of base 1 is two, and flexible post 18's other end fixed mounting has one side at another base 1, through the setting of bumper shock absorber 15, makes this lightweight unmanned aerial vehicle flight deck possess at the in-process of landing, and unmanned aerial vehicle's undercarriage can not receive very big impact force, and then is difficult for causing the damage to unmanned aerial vehicle's undercarriage to be convenient for fold it, and then the effect of convenient transport has played the effect of extension its life, has reached convenient purpose more.
When the unmanned aerial vehicle falls on the flying platform 5, the flying platform 5 can drive the lifting column 16 to move downwards through the landing gear, the lifting column 16 can drive the lifting plate 14 to move downwards in the lifting groove 13, the lifting plate 14 can downwards press the shock absorber 15, the shock absorber 15 can absorb the impact force, and then the unmanned aerial vehicle can more stably fall on the surface of the flying platform 5, when the unmanned aerial vehicle needs to be folded, the bolt 11 is screwed, one end of the bolt 11 is separated from the inside of the threaded hole, then one end of the flying platform 5 is moved, the flying platform 5 is folded together through the hinge, one side of the base 1 is pushed, the base 1 can drive the telescopic column 18 to move, the telescopic column 18 slides in the telescopic groove formed in the fixed column 2, the base 1 is combined together, the subsequent transportation is convenient, the effect of prolonging the service life of the unmanned aerial vehicle is achieved, and the purpose of more convenient use is achieved.
The foregoing is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical scheme of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.
Claims (8)
1. The utility model provides a lightweight unmanned aerial vehicle flight platform, includes base (1), its characterized in that: the top of the base (1) is fixedly provided with a fixed column (2), the outer side of the fixed column (2) is fixedly provided with a rotary ring, a first bracket (3) is fixedly arranged on the outer side of the rotary ring, a second bracket (4) is rotatably connected on one side of the first bracket (3), the top of the base (1) is provided with a lifting frame (5), the bottom of the lifting frame (5) is fixedly provided with a connecting seat, the top of the second bracket (4) is rotationally connected with the bottom of the connecting seat, the outer side of the rotating ring is fixedly provided with an electric telescopic rod (6), a pushing seat is fixedly arranged at the extending end of the electric telescopic rod (6), one end of the pushing seat is rotatably connected with one side of the second bracket (4), a sliding rail (501) is fixedly arranged at one side of the bottom of the lifting frame (5), a sliding seat (7) is connected in the sliding way (501), one end of the first bracket (3) is rotatably connected to one side of the sliding seat (7), the top of the base (1) is connected with a movable seat (8) in a sliding way, a support column (9) is fixedly arranged in the movable seat (8), the other end of the second bracket (4) is rotationally connected with the top of the movable seat (8), screw holes are formed in the tops of the lifting frames (5), and bolts (11) are connected to the inner threads of the screw holes.
2. The lightweight unmanned aerial vehicle flight platform of claim 1, wherein: the outer side of the bolt (11) is provided with a mounting plate (10), and the top of the mounting plate (10) is fixedly provided with a platform base (12).
3. The lightweight unmanned aerial vehicle flight platform of claim 2, wherein: lifting grooves (13) are formed in the platform base (12), and lifting plates (14) are connected inside the lifting grooves (13) in a sliding mode.
4. A lightweight unmanned aerial vehicle flight platform according to claim 3, wherein: the bottom of the lifting plate (14) is fixedly provided with a shock absorber (15), and the bottom of the shock absorber (15) is fixedly arranged on the inner bottom wall of the lifting groove (13).
5. The lightweight unmanned aerial vehicle flight platform of claim 4, wherein: lifting columns (16) are fixedly arranged at the tops of the lifting plates (14), and platform bodies (17) are fixedly arranged at the tops of the lifting columns (16).
6. The lightweight unmanned aerial vehicle flight platform of claim 5, wherein: the number of the platform bodies (17) is two, and the two platform bodies (17) are rotationally connected through a hinge.
7. The lightweight unmanned aerial vehicle flight platform of claim 6, wherein: the telescopic slot is formed in one end of the fixed column (2), and the telescopic column (18) is connected inside the telescopic slot in a sliding mode.
8. The lightweight unmanned aerial vehicle flight platform of claim 7, wherein: the number of the bases (1) is two, and the other end of the telescopic column (18) is fixedly arranged on one side of the other base (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322066703.1U CN220518611U (en) | 2023-08-03 | 2023-08-03 | Lightweight unmanned aerial vehicle flight platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322066703.1U CN220518611U (en) | 2023-08-03 | 2023-08-03 | Lightweight unmanned aerial vehicle flight platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220518611U true CN220518611U (en) | 2024-02-23 |
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ID=89926146
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322066703.1U Active CN220518611U (en) | 2023-08-03 | 2023-08-03 | Lightweight unmanned aerial vehicle flight platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220518611U (en) |
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2023
- 2023-08-03 CN CN202322066703.1U patent/CN220518611U/en active Active
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