CN221114381U - Unmanned aerial vehicle flight buffer stop - Google Patents
Unmanned aerial vehicle flight buffer stop Download PDFInfo
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- CN221114381U CN221114381U CN202323076794.3U CN202323076794U CN221114381U CN 221114381 U CN221114381 U CN 221114381U CN 202323076794 U CN202323076794 U CN 202323076794U CN 221114381 U CN221114381 U CN 221114381U
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- strip
- aerial vehicle
- unmanned aerial
- collision
- clamping
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- 238000009434 installation Methods 0.000 abstract description 13
- 238000010521 absorption reaction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000000575 pesticide Substances 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle flight anti-collision device, and relates to the technical field of repairing bridge cracks. This unmanned aerial vehicle anticollision device that flies, including the unmanned aerial vehicle main part, one side of unmanned aerial vehicle main part is provided with the connecting strip, one side of connecting strip is provided with mounting mechanism, one side of connecting strip is provided with anticollision institution. This unmanned aerial vehicle anticollision device that flies, through setting up the crashproof strip, when needs crashproof to the wing, be connected with installation mechanism through the connecting block in the bottom of wing at first, be provided with the carrier bar at installation mechanism's top, be connected with the crashproof strip through the rack in the inside of carrier bar, the inside of carrier bar is connected with draw-in lever and spring through the draw-in groove simultaneously, carry out the joint to the rack through the draw-in lever, and make the crashproof strip receive pressure movement when receiving the collision through the spring, the rack slides in the inside of carrier bar, buffer the impact force, avoid the wing directly to receive the collision, the device is convenient for crashproof to the wing.
Description
Technical Field
The utility model belongs to the technical field of repairing bridge cracks, and particularly relates to an unmanned aerial vehicle flight anti-collision device.
Background
In recent years, the agricultural unmanned helicopter is increasingly widely applied in the field of domestic agricultural plant protection operation in recent years, and the agricultural unmanned helicopter has the advantages of light weight, flexible use and the like, so that the agricultural unmanned helicopter is not only suitable for plain areas with wide land features, but also suitable for pesticide spraying and other operations in various complicated areas such as mountain areas, hills and the like;
The device does not have an unmanned aerial vehicle energy-absorbing anti-collision structure when in use, so that the collision force is counteracted by the energy absorption of the protection frame and the spring in most of the prior unmanned aerial vehicle anti-collision, but the unmanned aerial vehicle can rebound for a distance after the collision is finished, the unmanned aerial vehicle flight state is easily unbalanced, the unmanned aerial vehicle is inconvenient to use, and the unmanned aerial vehicle flight anti-collision device is designed based on the defects of the prior art.
Disclosure of utility model
In order to solve the problems in the prior art, the utility model provides the unmanned aerial vehicle flight anti-collision device, which has the characteristics of energy absorption and collision prevention of an unmanned aerial vehicle.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the unmanned aerial vehicle flight anti-collision device comprises an unmanned aerial vehicle main body, wherein a connecting strip is arranged on one side of the unmanned aerial vehicle main body, a mounting mechanism is arranged on one side of the connecting strip, and an anti-collision mechanism is arranged on one side of the connecting strip;
The anti-collision mechanism comprises an anti-collision strip and a rack, wherein the anti-collision strip is arranged on one side of the unmanned aerial vehicle main body, and one side of the anti-collision strip is fixedly connected with the rack.
As an optimal technical scheme of the unmanned aerial vehicle flight anti-collision device, the anti-collision mechanism further comprises a clamping rod, a spring, a bearing strip and a clamping groove, wherein the clamping rod is arranged on one side of the rack, the spring is movably sleeved on one side of the clamping rod, the bearing strip is arranged on one side of the anti-collision strip, and the clamping groove is formed in one side of the bearing strip.
As an optimal technical scheme of the unmanned aerial vehicle flight anti-collision device, the bottom of the unmanned aerial vehicle main body is provided with the supporting legs, and one side of the connecting strip is fixedly connected with the connecting block.
As an optimal technical scheme of the unmanned aerial vehicle flight anti-collision device, the upper surface of the connecting block is fixedly connected with a bearing block, and the top of the bearing block is provided with a wing.
As an optimal technical scheme of the unmanned aerial vehicle flight anti-collision device, the installation mechanism comprises a clamping ring, an annular groove, a connecting rod, an arc-shaped strip and a supporting rod, wherein the clamping ring is movably clamped on the outer surface of the connecting block, the annular groove is formed in the outer surface of the connecting block, one side of the clamping ring is fixedly connected with the connecting rod, one side of the connecting rod is fixedly connected with the arc-shaped strip, and the upper surface of the arc-shaped strip is fixedly connected with the supporting rod.
As an optimal technical scheme of the unmanned aerial vehicle flight anti-collision device, the clamping rod is connected inside the clamping groove in a sliding mode, and the spring is movably clamped inside the clamping groove.
As an optimal technical scheme of the unmanned aerial vehicle flight anti-collision device, the clamping ring is movably clamped in the annular groove, and the supporting rod is fixedly connected to the lower surface of the bearing strip.
Compared with the prior art, the utility model has the beneficial effects that:
1. When the anti-collision device is used, the anti-collision strip is arranged, when an airfoil is required to be crashed, the bottom of the airfoil is connected with the installation mechanism through the connecting block, the top of the installation mechanism is provided with the bearing strip, the anti-collision strip is connected inside the bearing strip through the rack, meanwhile, the clamping rod and the spring are connected inside the bearing strip through the clamping groove, the clamping rod is clamped with the rack through the clamping rod, the clamping rod is pressed to move when the anti-collision strip is crashed through the spring, the rack slides inside the bearing strip, the impact force is buffered, the airfoil is prevented from being directly crashed, and the anti-collision device is convenient for crashing the airfoil;
2. When the anti-collision mechanism is required to be installed, the anti-collision mechanism is clamped in the annular groove at one side of the connecting block through the clamping ring, and the anti-collision mechanism is convenient to install through the connecting rod, the arc-shaped strip and the supporting rod at one side of the clamping ring.
Drawings
The accompanying drawings are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate the utility model and together with the embodiments of the utility model, serve to explain the utility model. In the drawings:
fig. 1 is a schematic view of a main body structure of an unmanned aerial vehicle according to the present utility model;
FIG. 2 is a schematic view of a connecting strip according to the present utility model;
FIG. 3 is a schematic view of a mounting mechanism according to the present utility model;
Fig. 4 is a schematic structural view of an anti-collision mechanism according to the present utility model.
In the figure: 1. an unmanned aerial vehicle main body; 101. supporting feet; 2. a connecting strip; 201. a connecting block; 202. a bearing block; 203. a wing; 3. a mounting mechanism; 301. a clasp; 302. an annular groove; 303. a connecting rod; 304. an arc-shaped strip; 305. a support rod; 4. an anti-collision mechanism; 401. a bumper strip; 402. a rack; 403. a clamping rod; 404. a spring; 405. a carrier strip; 406. a clamping groove.
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. 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 the following technical solutions: the unmanned aerial vehicle flight anti-collision device comprises an unmanned aerial vehicle main body 1, wherein a connecting strip 2 is arranged on one side of the unmanned aerial vehicle main body 1, a mounting mechanism 3 is arranged on one side of the connecting strip 2, and an anti-collision mechanism 4 is arranged on one side of the connecting strip 2;
The bottom of unmanned aerial vehicle main part 1 is provided with supporting legs 101, and one side fixedly connected with connecting block 201 of connecting strip 2.
The upper surface of connecting block 201 is fixedly connected with carrier block 202, and the top of carrier block 202 is provided with wing 203.
Further explanation is needed: the bottom at unmanned aerial vehicle main part 1 is provided with supporting legs 101, supports when being convenient for unmanned aerial vehicle main part 1 falls to the ground through setting up supporting legs 101, is provided with connecting strip 2 in the side of unmanned aerial vehicle main part 1, installs wing 203 through setting up connecting strip 2, is fixed with connecting block 201 in one side of connecting strip 2 simultaneously, installs installation mechanism 3 through connecting block 201, is convenient for install crashproof mechanism 4 through setting up installation mechanism 3, has crashproof effect through setting up crashproof mechanism 4.
Referring to fig. 4, the present utility model provides the following technical solutions:
the anti-collision mechanism 4, the anti-collision mechanism 4 includes crashproof strip 401 and rack 402, and crashproof strip 401 sets up in one side of unmanned aerial vehicle main part 1, and one side fixedly connected with rack 402 of crashproof strip 401.
The anti-collision mechanism 4 further comprises a clamping rod 403, a spring 404, a bearing strip 405 and a clamping groove 406, wherein the clamping rod 403 is arranged on one side of the rack 402, the spring 404 is movably sleeved on one side of the clamping rod 403, the bearing strip 405 is arranged on one side of the anti-collision strip 401, and the clamping groove 406 is formed in one side of the bearing strip 405.
The clamping rod 403 is connected inside the clamping groove 406 in a sliding manner, and the spring 404 is movably clamped inside the clamping groove 406.
Further explanation is needed: the bottom of wing 203 is connected with installation mechanism 3 through connecting block 201, be provided with and bear strip 405 at the top of installation mechanism 3, be connected with crashproof strip 401 through rack 402 in the inside of bearing strip 405, be connected with draw-in lever 403 and spring 404 through draw-in groove 406 simultaneously, carry out the joint through draw-in lever 403 to rack 402, and make crashproof strip 401 receive the pressure and remove when receiving the collision through spring 404 draw-in lever 403, rack 402 slides in the inside of bearing strip 405, impact force is buffered, avoid wing 203 to receive the collision directly.
Referring to fig. 2-4, the present utility model provides the following technical solutions:
The mounting mechanism 3 comprises a clamping ring 301, an annular groove 302, a connecting rod 303, an arc-shaped strip 304 and a supporting rod 305, wherein the clamping ring 301 is movably clamped on the outer surface of the connecting block 201, the annular groove 302 is formed in the outer surface of the connecting block 201, one side of the clamping ring 301 is fixedly connected with the connecting rod 303, one side of the connecting rod 303 is fixedly connected with the arc-shaped strip 304, and the upper surface of the arc-shaped strip 304 is fixedly connected with the supporting rod 305.
The snap ring 301 is movably clamped in the annular groove 302, and the supporting rod 305 is fixedly connected to the lower surface of the bearing strip 405.
Further explanation is needed: the anti-collision mechanism 4 is convenient to install through the connecting rod 303, the arc-shaped strip 304 and the supporting rod 305 on one side of the clamping ring 301, and the clamping ring 301 is clamped inside the annular groove 302 on one side of the connecting block 201.
Working principle: when the unmanned aerial vehicle flight anti-collision device is used, firstly, the supporting feet 101 are arranged at the bottom of the unmanned aerial vehicle main body 1, the unmanned aerial vehicle main body 1 is supported conveniently when falling to the ground by arranging the supporting feet 101, the connecting strips 2 are arranged on the side face of the unmanned aerial vehicle main body 1, the wings 203 are arranged by arranging the connecting strips 2, meanwhile, the connecting blocks 201 are fixed on one side of the connecting strips 2, the installation mechanism 3 is arranged by the connecting blocks 201, the anti-collision mechanism 4 is convenient to install by arranging the installation mechanism 3, and the anti-collision mechanism 4 has an anti-collision effect;
When the wing 203 needs to be crashproof, be connected with installation mechanism 3 through connecting block 201 at the bottom of wing 203 at first, be provided with carrier strip 405 at the top of installation mechanism 3, be connected with crashproof strip 401 through rack 402 in the inside of carrier strip 405, simultaneously the inside of carrier strip 405 is connected with draw-in lever 403 and spring 404 through draw-in groove 406, carry out the joint to rack 402 through draw-in lever 403, and make crashproof strip 401 receive the pressure and remove when receiving the collision through spring 404, rack 402 slides in the inside of carrier strip 405, cushion the impact force, avoid wing 203 directly to receive the collision, the device is convenient for carry out the anticollision to wing 203.
When the anti-collision mechanism 4 needs to be installed, firstly, the anti-collision mechanism 4 is installed conveniently through the connecting rod 303, the arc-shaped strip 304 and the supporting rod 305 on one side of the clamping ring 301 in the annular groove 302 on one side of the connecting block 201 in a clamping mode, and the anti-collision mechanism 4 is installed conveniently.
Finally, it should be noted that: the above is only a preferred embodiment of the present utility model, and the present utility model is not limited thereto, but it is to be understood that the present utility model is described in detail with reference to the foregoing embodiments, and modifications and equivalents of some of the technical features described in the foregoing embodiments may be made by those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.
Claims (7)
1. Unmanned aerial vehicle collision avoidance system that flies, including unmanned aerial vehicle main part (1), its characterized in that: one side of the unmanned aerial vehicle main body (1) is provided with a connecting strip (2), one side of the connecting strip (2) is provided with a mounting mechanism (3), and one side of the connecting strip (2) is provided with an anti-collision mechanism (4);
Anti-collision mechanism (4), anti-collision mechanism (4) include crashproof strip (401) and rack (402), crashproof strip (401) set up in one side of unmanned aerial vehicle main part (1), one side fixedly connected with rack (402) of crashproof strip (401).
2. The unmanned aerial vehicle flight collision avoidance device of claim 1, wherein: the anti-collision mechanism (4) further comprises a clamping rod (403), a spring (404), a bearing strip (405) and a clamping groove (406), wherein the clamping rod (403) is arranged on one side of the rack (402), the spring (404) is movably sleeved on one side of the clamping rod (403), the bearing strip (405) is arranged on one side of the anti-collision strip (401), and the clamping groove (406) is formed in one side of the bearing strip (405).
3. The unmanned aerial vehicle flight collision avoidance device of claim 1, wherein: the bottom of unmanned aerial vehicle main part (1) is provided with supporting legs (101), one side fixedly connected with connecting block (201) of connecting strip (2).
4. A unmanned aerial vehicle flight collision avoidance device as claimed in claim 3, wherein: the upper surface of connecting block (201) is fixedly connected with carrier block (202), the top of carrier block (202) is provided with wing (203).
5. The unmanned aerial vehicle flight collision avoidance device of claim 1, wherein: the mounting mechanism (3) comprises a clamping ring (301), an annular groove (302), a connecting rod (303), an arc-shaped strip (304) and a supporting rod (305), wherein the clamping ring (301) is movably clamped on the outer surface of the connecting block (201), the annular groove (302) is formed in the outer surface of the connecting block (201), one side of the clamping ring (301) is fixedly connected with the connecting rod (303), one side of the connecting rod (303) is fixedly connected with the arc-shaped strip (304), and the upper surface of the arc-shaped strip (304) is fixedly connected with the supporting rod (305).
6. The unmanned aerial vehicle flight collision avoidance device of claim 2, wherein: the clamping rod (403) is connected inside the clamping groove (406) in a sliding mode, and the spring (404) is movably clamped inside the clamping groove (406).
7. The unmanned aerial vehicle flight collision avoidance device of claim 5, wherein: the clamping ring (301) is movably clamped in the annular groove (302), and the supporting rod (305) is fixedly connected to the lower surface of the bearing strip (405).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323076794.3U CN221114381U (en) | 2023-11-15 | 2023-11-15 | Unmanned aerial vehicle flight buffer stop |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323076794.3U CN221114381U (en) | 2023-11-15 | 2023-11-15 | Unmanned aerial vehicle flight buffer stop |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221114381U true CN221114381U (en) | 2024-06-11 |
Family
ID=91342736
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323076794.3U Active CN221114381U (en) | 2023-11-15 | 2023-11-15 | Unmanned aerial vehicle flight buffer stop |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221114381U (en) |
-
2023
- 2023-11-15 CN CN202323076794.3U patent/CN221114381U/en active Active
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