CN220263129U - A prevent submerged device for unmanned aerial vehicle - Google Patents
A prevent submerged device for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN220263129U CN220263129U CN202322006192.4U CN202322006192U CN220263129U CN 220263129 U CN220263129 U CN 220263129U CN 202322006192 U CN202322006192 U CN 202322006192U CN 220263129 U CN220263129 U CN 220263129U
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- 238000007667 floating Methods 0.000 claims abstract description 71
- 238000009434 installation Methods 0.000 claims abstract description 7
- 238000012423 maintenance Methods 0.000 abstract description 2
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Abstract
The utility model discloses an anti-sinking device for an unmanned aerial vehicle, which relates to the technical field of anti-sinking devices of unmanned aerial vehicles, and comprises an unmanned aerial vehicle body for installation, and is characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein a connecting assembly is arranged on the unmanned aerial vehicle body, and a floating assembly is arranged on the connecting assembly; the connecting assembly comprises two groups of first fixing plates arranged on one side of the unmanned aerial vehicle body, the two groups of first fixing plates are symmetrically distributed about the central axis of the unmanned aerial vehicle body, the two groups of first fixing plates are respectively provided with a first clamping groove, the two groups of first fixing plates are respectively provided with a first fixing hole at the top, a first clamping block is arranged in the first clamping groove, and a first circular through hole is formed in the first clamping block. The utility model relates to an anti-sinking device for an unmanned aerial vehicle, which enables equipment to be capable of rapidly installing the anti-sinking device when in use, is convenient for subsequent maintenance, and greatly improves the use efficiency.
Description
Technical Field
The utility model relates to the technical field of anti-sinking devices of unmanned aerial vehicles, in particular to an anti-sinking device for an unmanned aerial vehicle.
Background
Unmanned aerial vehicles refer to aircraft without personnel, which are manipulated and operated by wireless remote control or a preset automated program. Unmanned aerial vehicles are typically composed of a number of components, including a body, a battery, a motor, sensors, a control system, and the like. They can be designed and manufactured according to different uses and requirements, with various shapes and sizes. Unmanned aerial vehicles's application is very extensive. In military terms, unmanned aerial vehicles are commonly used to detect, monitor and fight enemy targets. In the civil field, unmanned aerial vehicle can be used to aerial photography, geological exploration, disaster monitoring, agricultural spraying, cargo transportation etc. In addition, unmanned aerial vehicle can also be used for fields such as environmental protection, scientific research, amusement.
The existing unmanned aerial vehicle is not provided with an anti-sinking device generally, however, under certain special application scenes, such as marine rescue or water surface monitoring, some special unmanned aerial vehicles may be provided with the anti-sinking device, but are very complex to install in use, are very inconvenient to disassemble and maintain after use, greatly influence the use efficiency, bring very bad experiences to users, and therefore, a new solution is necessary to be provided.
The existing unmanned aerial vehicle anti-sinking device is very complex to install when in use, is inconvenient to detach and maintain after use, greatly influences the use efficiency, and therefore, we propose an anti-sinking device for an unmanned aerial vehicle.
Disclosure of Invention
The utility model mainly aims to provide an anti-sinking device for an unmanned aerial vehicle, which can effectively solve the problems in the background technology.
In order to achieve the above purpose, the technical scheme adopted by the utility model is as follows: the utility model provides an prevent submerged device for unmanned aerial vehicle, includes the unmanned aerial vehicle body that is used for the installation, be equipped with coupling assembling on the unmanned aerial vehicle body, be equipped with on the coupling assembling and float the subassembly, coupling assembling is used for floating the subassembly and is connected with the unmanned aerial vehicle body, floats the subassembly and prevents that the unmanned aerial vehicle body from sinking;
the connecting assembly comprises two groups of first fixing plates arranged on one side of the unmanned aerial vehicle body, the two groups of first fixing plates are symmetrically distributed on the other side of the unmanned aerial vehicle body, first clamping grooves are formed in one side of the first fixing plates, first fixing holes are formed in the tops of the two groups of first fixing plates, first clamping blocks are arranged in the first clamping grooves, first circular through holes are formed in the first clamping blocks, first springs are arranged in the first circular through holes, first fixing blocks are fixedly connected to one ends of the first springs far away from the first circular through holes, the first fixing blocks are matched with the first fixing holes, two groups of second fixing plates are arranged on the other side of the unmanned aerial vehicle body, the two groups of second fixing plates are symmetrically distributed on the other side of the unmanned aerial vehicle body, second clamping grooves are formed in one side of the second fixing plates, second fixing holes are formed in the tops of the two groups of the second fixing plates, second clamping blocks are arranged in the second clamping grooves, second circular through holes are formed in the second clamping grooves, first through holes are formed in the second clamping blocks, first springs are fixedly connected to the first fixing blocks, the first fixing blocks are fixedly arranged in the first circular through holes, the first fixing blocks are fixedly arranged in the first fixing blocks far away from the first circular through holes, the first fixing blocks are fixedly arranged in the first fixing blocks, and are fixedly arranged at the first fixing blocks, and are fixedly arranged in the first fixing blocks, and are fixedly arranged at first fixing blocks, and are fixedly in the first fixing blocks and are fixedly arranged at first fixing blocks and are opposite first fixing holes and are opposite to the first fixing holes and are fixedly through holes and are fixedly arranged in the first fixing holes and are respectively, and are respectively. The second clamping block is fixed in the second clamping groove.
Preferably, the floating assembly comprises a first floating plate and a second floating plate which are arranged at the bottom of the unmanned aerial vehicle body, two groups of first convex blocks are arranged on one side of the first floating plate and symmetrically distributed about the central axis of the first floating plate, two groups of first convex blocks are arranged on the other end of the first convex blocks, one side of the top of the first connecting plate is fixedly connected with one end of a first clamping block, the first floating plate and the second floating plate are used for providing buoyancy, the unmanned aerial vehicle body is prevented from sinking, the first convex blocks are used for connecting the first floating plate with the first connecting plate, and the first connecting plate is convenient to connect the first floating plate with the first clamping block.
Preferably, two groups of second protruding blocks are arranged on one side of the second floating plate, the two groups of second protruding blocks are symmetrically distributed about the central axis of the second floating plate, a second connecting plate is arranged at the other end of each second protruding block, one side of the top of each second connecting plate is fixedly connected with one end of each second clamping block, the second protruding blocks are used for connecting the second floating plate with the second connecting plate, and the second connecting plates are convenient to connect the second floating plate with the second clamping blocks.
Preferably, two sets of positioning jacks are formed in one side of the first floating plate, the two sets of positioning jacks are symmetrically distributed about the central axis of the first floating plate, and the two sets of positioning jacks are convenient for placing two sets of positioning inserting rods.
Preferably, two groups of positioning inserting rods are arranged on one side of the second floating plate, the two groups of positioning inserting rods are symmetrically distributed about the central axis of the second floating plate, and the two groups of positioning inserting rods are matched with the two groups of positioning inserting holes so as to conveniently and rapidly position the first floating plate and the second floating plate.
Preferably, the other ends of the two groups of positioning inserting rods extend into the positioning insertion holes, so that the first floating plate and the second floating plate can be conveniently installed.
Compared with the prior art, the utility model has the following beneficial effects:
according to the anti-sinking device, the two groups of positioning inserting rods are inserted into the positioning inserting holes at first, so that the first floating plate and the second floating plate can be positioned quickly, the two groups of first fixing blocks are pressed into the first fixing holes, the first clamping blocks are aligned with the first clamping grooves and pushed in, the first springs are used for fixing the first fixing blocks in the first fixing holes, the first clamping blocks are fixed in the first clamping grooves, the first floating plate is fixed through the first connecting plates, the two groups of second fixing blocks are pressed into the second fixing holes, the second clamping blocks are aligned with the second clamping grooves and pushed in, the second springs are used for fixing the second fixing blocks in the second fixing holes, the second clamping blocks are fixed in the second clamping grooves through the second connecting plates, and finally, the installation is completed, so that the anti-sinking device can be installed quickly, the subsequent maintenance is facilitated, and the use efficiency is greatly improved.
Drawings
FIG. 1 is a schematic view of the whole structure of an anti-sinking device for an unmanned aerial vehicle;
FIG. 2 is a schematic top cross-sectional view of an anti-sinking device for an unmanned aerial vehicle according to the present utility model;
FIG. 3 is a schematic cross-sectional view of FIG. 1 in accordance with the present utility model;
fig. 4 is a schematic cross-sectional view of fig. 1 in accordance with the present utility model.
In the figure: 1. an unmanned aerial vehicle body; 2. a first floating plate; 3. a second floating plate; 4. a first fixing plate; 5. a second fixing plate; 6. a first clamping groove; 7. a second clamping groove; 8. a first clamping block; 9. a second clamping block; 10. a first fixing hole; 11. a second fixing hole; 12. a first spring; 13. a second spring; 14. a first fixed block; 15. a second fixed block; 16. a first connection plate; 17. a second connecting plate; 18. a first bump; 19. a second bump; 20. positioning the jack; 21. positioning the inserted link.
Detailed Description
The utility model is further described in connection with the following detailed description, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the utility model easy to understand.
In the description of the present utility model, it should be noted that the directions or positional relationships indicated by the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific direction, be configured and operated in the specific direction, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "provided," "connected," and the like are to be construed broadly, and may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
Example 1
Referring to fig. 1-4, the anti-sinking device for an unmanned aerial vehicle of the present utility model includes an unmanned aerial vehicle body 1 for installation, a connection assembly is provided on the unmanned aerial vehicle body 1, a floating assembly is provided on the connection assembly, the connection assembly is used for 1 connection of the floating assembly and the unmanned aerial vehicle body, the floating assembly prevents the unmanned aerial vehicle body 1 from sinking;
the connecting component comprises two groups of first fixing plates 4 arranged on one side of the unmanned aerial vehicle body 1, the two groups of first fixing plates 4 are symmetrically distributed about the central axis of the unmanned aerial vehicle body 1, first clamping grooves 6 are formed in one side of the two groups of first fixing plates 4, first fixing holes 10 are formed in the tops of the two groups of first fixing plates 4, first clamping blocks 8 are arranged in the first clamping grooves 6, first circular through holes are formed in the first clamping blocks 8, first springs 12 are arranged in the first circular through holes, first fixing blocks 14 are fixedly connected to one ends of the first springs 12 far away from the first circular through holes, the first fixing blocks 14 are matched with the first fixing holes 10, two groups of second fixing plates 5 are arranged on the other side of the unmanned aerial vehicle body 1, the two groups of second fixing plates 5 are symmetrically distributed about the central axis of the unmanned aerial vehicle body 1, second clamping grooves 7 are formed in one side of the two groups of second fixing plates 5, second fixing holes 11 are formed in the tops of the two groups of second fixing plates 5, the second clamping groove 7 is internally provided with a second clamping block 9, the second clamping block 9 is provided with a second circular through hole, the second circular through hole is internally provided with a second spring 13, one end of the second spring 13 far away from the second circular through hole is fixedly connected with a second fixing block 15, the second fixing block 15 is matched with the second fixing hole 11, the first clamping groove 6 is used for fixing the first clamping block 8 on the first fixing plate 4, the second clamping groove 7 is used for fixing the second clamping block 9 on the second fixing plate 5, the floating assembly is fixed on the unmanned aerial vehicle body 1, the first circular through hole is used for installing a first spring 12, the second circular through hole is used for installing a second spring 13, the first spring 12 is used for fixing the first fixing block 14 in the first fixing hole 10, the first clamping block 8 is fixed in the first clamping groove 6, the second spring 13 is used for fixing the second fixing block 15 in the second fixing hole 11, so that the second clamping block 9 is fixed in the second clamping groove 7.
The floating assembly comprises a first floating plate 2 and a second floating plate 3, wherein the first floating plate 2 and the second floating plate 3 are arranged at the bottom of the unmanned aerial vehicle body 1, two groups of first convex blocks 18 are arranged on one side of the first floating plate 2 and symmetrically distributed relative to the central axis of the first floating plate 2, first connecting plates 16 are arranged at the other ends of the two groups of first convex blocks 18, one side of the top of each first connecting plate 16 is fixedly connected with one end of each first clamping block 8, the first floating plate 2 and the second floating plate 3 are used for providing buoyancy, the unmanned aerial vehicle body 1 is prevented from sinking, the first convex blocks 18 are used for connecting the first floating plate 2 with the first connecting plates 16, and the first connecting plates 16 are convenient to connect the first floating plate 2 with the first clamping blocks 8.
Two groups of second convex blocks 19 are arranged on one side of the second floating plate 3, the two groups of second convex blocks 19 are symmetrically distributed about the central axis of the second floating plate 3, second connecting plates 17 are arranged at the other ends of the two groups of second convex blocks 19, one side of the top of each second connecting plate 17 is fixedly connected with one end of each second clamping block 9, the second convex blocks 19 are used for connecting the second floating plate 3 with the second connecting plates 17, and the second connecting plates 17 are convenient for connecting the second floating plate 3 with the second clamping blocks 9.
Example 2
The embodiment is an improvement made on the basis of embodiment 1, and referring to fig. 2, two sets of positioning jacks 20 are provided on one side of the first floating plate 2, the two sets of positioning jacks 20 are symmetrically distributed about the central axis of the first floating plate 2, two sets of positioning inserting rods 21 are provided on one side of the second floating plate 3, the two sets of positioning inserting rods 21 are symmetrically distributed about the central axis of the second floating plate 3, the other ends of the two sets of positioning inserting rods 21 extend into the positioning jacks 20, the two sets of positioning inserting rods 21 are convenient for placing the two sets of positioning inserting rods 21, the two sets of positioning inserting rods 21 are matched with the two sets of positioning jacks 20 to facilitate rapid positioning of the first floating plate 2 and the second floating plate 3, and the first floating plate 2 and the second floating plate 3 are convenient for installation.
The working principle of the utility model is as follows: firstly, two groups of positioning inserting rods 21 are inserted into the positioning insertion holes 20, so that the first floating plate 2 and the second floating plate 3 can be positioned quickly, then two groups of first fixing blocks 14 are pressed into the first fixing holes 10, then the first clamping blocks 8 are aligned with the first clamping grooves 6 and pushed in, the first springs 12 are used for fixing the first fixing blocks 14 in the first fixing holes 10, the first clamping blocks 8 are fixed in the first clamping grooves 6, the first floating plate 2 is fixed through the first connecting plates 16, then two groups of second fixing blocks 15 are pressed into the second fixing holes 11, then the second clamping blocks 9 are aligned with the second clamping grooves 7 and pushed in, the second springs 13 are used for fixing the second fixing blocks 15 in the second fixing holes 11, so that the second clamping blocks 9 are fixed in the second clamping grooves 7, the second floating plate 3 is fixed through the second connecting plates 17, and finally the installation is completed.
The foregoing has shown and described the basic principles and main features of the present utility model and the advantages of the present utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present utility model, and various changes and modifications may be made without departing from the spirit and scope of the utility model, which is defined in the appended claims. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (6)
1. A prevent submerged device for unmanned aerial vehicle, including unmanned aerial vehicle body (1) that is used for the installation, its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein a connecting component is arranged on the unmanned aerial vehicle body, and a floating component is arranged on the connecting component;
the utility model discloses a unmanned aerial vehicle, including connecting subassembly, including setting up two sets of first fixed plates (4) in unmanned aerial vehicle body (1) one side, two sets of first fixed plate (4) are about unmanned aerial vehicle body (1) axis symmetric distribution, two sets of first fixed plate (4) one side has all been seted up first fixed orifices (10), two sets of first fixed plate (4) top has all been seted up first fixed orifices (10), be equipped with first fixture block (8) in first fixed plate (6), set up first circular through-hole on first fixture block (8), be equipped with first spring (12) in the first circular through-hole, first spring (12) are in the one end fixedly connected with first fixed block (14) that keep away from first circular through-hole, first fixed block (14) and first fixed orifices (10) phase-match, unmanned aerial vehicle body (1) opposite side is equipped with two sets of second fixed plates (5) first fixed orifices (10), two sets of second fixed plate (5) are about unmanned aerial vehicle body (1) symmetric distribution, two sets of second fixed plates (5) have been equipped with first circular through-hole (7) in the first fixed plate (8), two sets of second through-hole (7) have been seted up on second fixed orifices (9), the second spring (13) is fixedly connected with a second fixing block (15) at one end far away from the second circular through hole, and the second fixing block (15) is matched with the second fixing hole (11).
2. An anti-sinking device for an unmanned aerial vehicle according to claim 1, wherein: the floating assembly comprises a first floating plate (2) and a second floating plate (3) which are arranged at the bottom of an unmanned aerial vehicle body (1), two groups of first convex blocks (18) are arranged on one side of the first floating plate (2), the two groups of first convex blocks (18) are symmetrically distributed about the central axis of the first floating plate (2), a first connecting plate (16) is arranged at the other end of each first convex block (18), and one side of the top of each first connecting plate (16) is fixedly connected with one end of a first clamping block (8).
3. An anti-sinking device for an unmanned aerial vehicle according to claim 2, wherein: two groups of second convex blocks (19) are arranged on one side of the second floating plate (3), the two groups of second convex blocks (19) are symmetrically distributed about the central axis of the second floating plate (3), a second connecting plate (17) is arranged at the other end of each second convex block (19), and one side of the top of each second connecting plate (17) is fixedly connected with one end of each second clamping block (9).
4. A submerged preventing apparatus for an unmanned aerial vehicle according to claim 3, wherein: two groups of positioning jacks (20) are formed in one side of the first floating plate (2), and the two groups of positioning jacks (20) are symmetrically distributed relative to the central axis of the first floating plate (2).
5. An anti-submergence device for a drone as set forth in claim 4 wherein: two groups of positioning inserting rods (21) are arranged on one side of the second floating plate (3), and the two groups of positioning inserting rods (21) are symmetrically distributed relative to the central axis of the second floating plate (3).
6. The anti-submergence device for a drone of claim 5, wherein: the other ends of the two groups of positioning inserting rods (21) extend into the positioning inserting holes (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322006192.4U CN220263129U (en) | 2023-07-28 | 2023-07-28 | A prevent submerged device for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322006192.4U CN220263129U (en) | 2023-07-28 | 2023-07-28 | A prevent submerged device for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220263129U true CN220263129U (en) | 2023-12-29 |
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ID=89298030
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322006192.4U Active CN220263129U (en) | 2023-07-28 | 2023-07-28 | A prevent submerged device for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220263129U (en) |
-
2023
- 2023-07-28 CN CN202322006192.4U patent/CN220263129U/en active Active
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