CN221214656U - Unmanned aerial vehicle protects support - Google Patents

Unmanned aerial vehicle protects support Download PDF

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Publication number
CN221214656U
CN221214656U CN202322549541.7U CN202322549541U CN221214656U CN 221214656 U CN221214656 U CN 221214656U CN 202322549541 U CN202322549541 U CN 202322549541U CN 221214656 U CN221214656 U CN 221214656U
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CN
China
Prior art keywords
groove
fixedly connected
aerial vehicle
unmanned aerial
sliding
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CN202322549541.7U
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Chinese (zh)
Inventor
戴炳宇
洪宇
葛成林
王龙磊
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Fujian Minnan Aviation Technology Co ltd
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Fujian Minnan Aviation Technology Co ltd
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Priority to CN202322549541.7U priority Critical patent/CN221214656U/en
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Abstract

The utility model relates to the technical field of unmanned aerial vehicle protection brackets, in particular to an unmanned aerial vehicle protection bracket which comprises a mounting plate, wherein one side of the mounting plate is fixedly connected with a bearing column, the inside of the bearing column is provided with a hollow groove, the inner side wall of the hollow groove is slidably connected with a sliding plate, the bottom of the sliding plate is fixedly connected with a telescopic column, the inner bottom wall of the hollow groove is provided with a first sliding groove, the inner side wall of the first sliding groove is fixedly connected with a limiting plate, the outer wall of the telescopic column is provided with a second sliding groove, the inner top wall of the hollow groove is provided with a third sliding groove, the inside of the third sliding groove is slidably connected with a connecting block, the inside of the connecting block is fixedly connected with a shaft lever, and the outside of the shaft lever is rotatably connected with a rotating plate. According to the utility model, the unmanned aerial vehicle can be buffered, damped and protected, so that the use safety of the unmanned aerial vehicle is improved, the property loss of people is reduced, the use stability of the unmanned aerial vehicle is improved, and the unmanned aerial vehicle is conveniently protected by people.

Description

Unmanned aerial vehicle protects support
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle protection brackets, in particular to an unmanned aerial vehicle protection bracket.
Background
Unmanned plane is unmanned plane for short, is the unmanned plane that utilizes radio remote control equipment and self-contained program control device to operate, perhaps carries out autonomous operation by on-vehicle computer is complete or indirect, compares with unmanned plane, unmanned plane often more is fit for the task that is too "dull, dirty or dangerous", unmanned plane is used in many fields, has military unmanned plane, is used in survey and reconnaissance etc. aspects, has civil unmanned plane, is used in aspects such as sprinkling irrigation and disinfection of crops, and unmanned plane's creation technique constantly is innovating and advancing. In the prior art, the unmanned aerial vehicle can be impacted by the ground during landing, so that the internal mechanical parts of the unmanned aerial vehicle are damaged, the use safety of the unmanned aerial vehicle is reduced, people are inconvenient to use the unmanned aerial vehicle, and therefore, the unmanned aerial vehicle protection support is needed to be provided.
Disclosure of utility model
(One) solving the technical problems
Aiming at the defects of the prior art, the utility model aims to provide the unmanned aerial vehicle protection bracket which can buffer, absorb shock and protect the unmanned aerial vehicle.
(II) technical scheme
In order to achieve the above purpose, the utility model provides the following technical scheme, namely, an unmanned aerial vehicle protection bracket, which comprises the following steps: including the mounting panel, one side fixedly connected with spandrel post of mounting panel, the hollow space has been seted up to spandrel post's inside, the inside wall sliding connection of hollow space has the sliding plate, the flexible post of bottom fixedly connected with of sliding plate, first spout has been seted up to the interior bottom wall of hollow space, the inside wall fixedly connected with limiting plate of first spout.
The second spout has been seted up to the outer wall of flexible post, the third spout has been seted up to the interior roof of empty slot, the inside sliding connection of third spout has the connecting block, the inside fixedly connected with axostylus axostyle of connecting block, the outside of axostylus axostyle rotates and is connected with the rotor plate, can cushion shock attenuation protection to unmanned aerial vehicle, improves unmanned aerial vehicle's safety in utilization, reduces people's loss of property simultaneously, increases unmanned aerial vehicle's stability in use, and people of being convenient for protect unmanned aerial vehicle.
As the preferred scheme, be sliding connection between limiting plate and the second spout, the interior roof fixedly connected with damping spring of second spout is convenient for carry out slip shock attenuation to the telescopic column.
As the preferable scheme, the rotating plate is connected with the connecting block in a rotating way through the shaft rod, and one side of the connecting block is fixedly connected with a damping spring, so that the rotating plate can conveniently extrude the connecting block to slide.
As the preferred scheme, the mounting groove has been seted up to the inside of mounting panel, the inside sliding connection of mounting groove has the installation piece, the storage groove has been seted up to the inside of installation piece, the fourth spout has been seted up to the inside wall of storage groove, the inside sliding connection of fourth spout has the slider, one side fixedly connected with push pedal of slider, the bottom fixedly connected with fixture block of push pedal, the draw-in groove has been seted up to the interior bottom wall of mounting groove, the cavity has been seted up to the interior roof of mounting groove, the inside sliding connection of cavity has the extrusion piece, the fifth spout has been seted up to the inside wall fixedly connected with connecting rod of cavity, the top fixedly connected with slide bar of extrusion piece, the top fixedly connected with fixed disk of slide bar can carry out quick installation to the mounting panel.
As the preferred scheme, the width size of mounting groove is greater than the width size of installation piece, the top fixedly connected with reset spring of slider is convenient for install the inside at the mounting groove of installation piece.
As the preferable scheme, be the block between fixture block and the draw-in groove fixedly, for mutually perpendicular setting between extrusion piece and the installation piece, the extrusion piece of being convenient for carries out stable slip.
As the preferred scheme, the top fixedly connected with extension spring of extrusion piece is sliding connection between connecting rod and the fifth spout, is convenient for carry out slip spacing to the extrusion piece.
(III) beneficial effects
Compared with the prior art, the utility model provides the unmanned aerial vehicle protection bracket, which has the following beneficial effects:
1. According to the unmanned aerial vehicle, the mounting plate, the bearing post, the empty slot, the sliding plate, the telescopic post, the first sliding slot, the limiting plate, the second sliding slot, the third sliding slot, the connecting block, the shaft rod and the rotating plate are arranged, the unmanned aerial vehicle drives the bearing post to slide through the mounting plate, so that the telescopic post drives the fixed pad at the bottom to contact the ground, meanwhile, the telescopic post extrudes the sliding plate to slide in the empty slot, the telescopic post slides in the first sliding slot, the limiting plate slides in the second sliding slot, meanwhile, the limiting plate extrudes the damping spring to buffer and absorb shock, the sliding plate extrudes the rotating plate to rotate through the shaft rod, the rotating plate extrudes the connecting block to slide in the third sliding slot, meanwhile, the connecting block extrudes the damping spring to buffer and absorb shock, the unmanned aerial vehicle can be buffered and absorbed and protected, the use safety of the unmanned aerial vehicle is improved, the use stability of the unmanned aerial vehicle is improved, and people can conveniently protect the unmanned aerial vehicle.
2. According to the utility model, the mounting groove, the mounting block, the storage groove, the fourth sliding groove, the sliding block, the push plate, the clamping block, the clamping groove, the cavity, the extrusion block, the fifth sliding groove, the connecting rod, the sliding rod and the fixed disc are arranged, the fixed disc is pulled to enable the fixed disc to drive the sliding rod to slide in the mounting plate, the sliding rod drives the extrusion block to slide in the cavity, the connecting rod slides in the fifth sliding groove, the mounting block is inserted into the mounting groove, the mounting groove extrudes the clamping block to slide, the clamping block extrudes the push plate to slide, the sliding block is driven to slide in the fourth sliding groove by the push plate, the clamping block is reset through the telescopic spring, the clamping block and the clamping groove are clamped and fixed, and the fixed disc is loosened, so that the extrusion block is reset through the telescopic spring, and the mounting plate can be rapidly mounted, thereby saving a large amount of time and effort, improving the use rapidness of the protection bracket, and being convenient for people to use the protection bracket.
Drawings
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is a schematic diagram of a front cross-sectional structure of the present utility model;
FIG. 3 is an enlarged schematic view of the structure of FIG. 2A according to the present utility model;
FIG. 4 is an enlarged schematic view of the structure of FIG. 2B according to the present utility model;
fig. 5 is a schematic perspective view of a fixture block according to the present utility model.
In the figure: 1. a mounting plate; 2. a bearing column; 3. a hollow groove; 4. a sliding plate; 5. a telescopic column; 6. a first chute; 7. a limiting plate; 8. a second chute; 9. a third chute; 10. a connecting block; 11. a shaft lever; 12. a rotating plate; 13. a mounting groove; 14. a mounting block; 15. a storage groove; 16. a fourth chute; 17. a slide block; 18. a push plate; 19. a clamping block; 20. a clamping groove; 21. a cavity; 22. extruding a block; 23. a fifth chute; 24. a connecting rod; 25. a slide bar; 26. a fixed disk.
Detailed Description
Embodiments of the present utility model are described in further detail below with reference to the accompanying drawings and examples. The following examples are illustrative of the utility model but are not intended to limit the scope of the utility model.
In the description of the present utility model, unless otherwise indicated, the meaning of "a plurality" is two or more; the terms "upper," "lower," "left," "right," "inner," "outer," "front," "rear," "head," "tail," and the like are used as an orientation or positional relationship based on that shown in the drawings, merely to facilitate description of the utility model and to simplify the description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore should not be construed as limiting the utility model. Furthermore, the terms "first," "second," "third," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
Example 1
Referring to fig. 1-5, the embodiment provides a protection support for an unmanned aerial vehicle, which comprises a mounting plate 1, wherein one side of the mounting plate 1 is fixedly connected with a bearing column 2, a hollow groove 3 is formed in the bearing column 2, a sliding plate 4 is slidably connected to the inner side wall of the hollow groove 3, a telescopic column 5 is fixedly connected to the bottom of the sliding plate 4, a first sliding groove 6 is formed in the inner bottom wall of the hollow groove 3, and a limiting plate 7 is fixedly connected to the inner side wall of the first sliding groove 6.
The second spout 8 has been seted up to the outer wall of flexible post 5, third spout 9 has been seted up to the interior roof of empty slot 3, the inside sliding connection of third spout 9 has connecting block 10, the inside fixedly connected with axostylus axostyle 11 of connecting block 10, the outside rotation of axostylus axostyle 11 is connected with rotor plate 12, can cushion shock attenuation protection to unmanned aerial vehicle, improve unmanned aerial vehicle's safety in utilization, reduce people's loss of property simultaneously, increase unmanned aerial vehicle's stability in use, the people of being convenient for protect unmanned aerial vehicle.
The limiting plate 7 is in sliding connection with the second sliding groove 8, and the damping spring is fixedly connected to the inner top wall of the second sliding groove 8, so that sliding damping is conveniently carried out on the telescopic column 5.
The rotating plate 12 is connected with the connecting block 10 in a rotating way through the shaft rod 11, and a damping spring is fixedly connected to one side of the connecting block 10, so that the rotating plate 12 can conveniently extrude the connecting block 10 to slide.
Example 2
Referring to fig. 1-5, based on the same concept as that of the above embodiment 1, the present embodiment further proposes that a mounting groove 13 is formed in the mounting plate 1, a mounting block 14 is slidably connected in the mounting groove 13, a receiving groove 15 is formed in the mounting block 14, a fourth sliding groove 16 is formed in an inner side wall of the receiving groove 15, a sliding block 17 is slidably connected in the fourth sliding groove 16, a push plate 18 is fixedly connected to one side of the sliding block 17, a clamping block 19 is fixedly connected to the bottom of the push plate 18, a clamping groove 20 is formed in an inner bottom wall of the mounting groove 13, a cavity 21 is formed in an inner top wall of the mounting groove 13, an extrusion block 22 is slidably connected in the cavity 21, a fifth sliding groove 23 is formed in the extrusion block 22, a connecting rod 24 is fixedly connected to an inner side wall of the cavity 21, a sliding rod 25 is fixedly connected to a top end of the extrusion block 22, and a fixed disc 26 is fixedly connected to a top end of the sliding rod 25, so that the mounting plate 1 can be quickly mounted.
The width size of the mounting groove 13 is larger than that of the mounting block 14, and a reset spring is fixedly connected to the top of the sliding block 17, so that the mounting block 14 is conveniently mounted in the mounting groove 13.
The clamping block 19 and the clamping groove 20 are clamped and fixed, and the extrusion block 22 and the mounting block 14 are mutually perpendicular, so that the extrusion block 22 can stably slide.
The telescopic spring is fixedly connected to the top of the extrusion block 22, and the connecting rod 24 and the fifth sliding groove 23 are in sliding connection, so that the extrusion block 22 can be conveniently limited in a sliding manner.
The working principle of the utility model is as follows: when the unmanned aerial vehicle needs to be buffered, damping and protection, the unmanned aerial vehicle drives the bearing column 2 to slide through the mounting plate 1, thereby the fixed pad at the bottom of the telescopic column 5 is driven to contact the ground, meanwhile, the telescopic column 5 extrudes the sliding plate 4 to slide in the hollow groove 3, so that the telescopic column 5 slides in the first sliding groove 6, the limiting plate 7 slides in the second sliding groove 8, meanwhile, the limiting plate 7 extrudes the damping spring to buffer and absorb shock, the sliding plate 4 extrudes the rotating plate 12 to rotate through the shaft rod 11, the rotating plate 12 extrudes the connecting block 10 to slide in the third sliding groove 9, meanwhile, the connecting block 10 extrudes the damping spring to buffer and absorb shock, the unmanned aerial vehicle can be buffered, damped and protected, the use safety of the unmanned aerial vehicle is improved, the property loss of people is reduced, the use stability of the unmanned aerial vehicle is improved, and the unmanned aerial vehicle is protected conveniently;
When the mounting plate 1 needs to be rapidly mounted, the fixing disc 26 is pulled, the fixing disc 26 drives the sliding rod 25 to slide in the mounting plate 1, the sliding rod 25 drives the extrusion block 22 to slide in the cavity 21, meanwhile, the connecting rod 24 slides in the fifth sliding groove 23, the mounting block 14 is inserted into the mounting groove 13, the mounting groove 13 extrudes the clamping block 19 to slide, the clamping block 19 extrudes the push plate 18 to slide, the push plate 18 drives the sliding block 17 to slide in the fourth sliding groove 16, the clamping block 19 resets through the telescopic spring, the clamping block 19 and the clamping groove 20 are clamped and fixed, the fixing disc 26 is loosened, the extrusion block 22 resets through the telescopic spring, and the mounting plate 1 can be rapidly mounted, so that a large amount of time and effort are saved, the use rapidness of the protective bracket is improved, and people can conveniently use the protective bracket.
Finally, it should be noted that the above embodiments are only for illustrating the technical solution of the present utility model, and not for limiting the scope of the present utility model, and although the present utility model has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications or equivalent substitutions can be made to the technical solution of the present utility model without departing from the spirit and scope of the technical solution of the present utility model.

Claims (7)

1. The utility model provides an unmanned aerial vehicle protection support, includes mounting panel (1), its characterized in that: one side of the mounting plate (1) is fixedly connected with a bearing column (2), an empty groove (3) is formed in the bearing column (2), a sliding plate (4) is slidably connected to the inner side wall of the empty groove (3), a telescopic column (5) is fixedly connected to the bottom of the sliding plate (4), a first sliding groove (6) is formed in the inner bottom wall of the empty groove (3), and a limiting plate (7) is fixedly connected to the inner side wall of the first sliding groove (6);
the outer wall of flexible post (5) has seted up second spout (8), third spout (9) have been seted up to the interior roof of empty slot (3), the inside sliding connection of third spout (9) has connecting block (10), the inside fixedly connected with axostylus axostyle (11) of connecting block (10), the outside of axostylus axostyle (11) rotates and is connected with rotor plate (12).
2. The unmanned aerial vehicle protective bracket according to claim 1, wherein: the limiting plate (7) is in sliding connection with the second sliding groove (8), and the damping spring is fixedly connected with the inner top wall of the second sliding groove (8).
3. The unmanned aerial vehicle protective bracket according to claim 1, wherein: the rotating plate (12) is in rotating connection with the connecting block (10) through the shaft rod (11), and one side of the connecting block (10) is fixedly connected with a damping spring.
4. The unmanned aerial vehicle protective bracket according to claim 1, wherein: the inside of mounting panel (1) has been seted up mounting groove (13), the inside sliding connection of mounting groove (13) has installed piece (14), accomodate groove (15) have been seted up to the inside of installing piece (14), accomodate the inside wall of groove (15) and have been seted up fourth spout (16), the inside sliding connection of fourth spout (16) has slider (17), one side fixedly connected with push pedal (18) of slider (17), the bottom fixedly connected with fixture block (19) of push pedal (18), draw-in groove (20) have been seted up to the interior inner wall of mounting groove (13), cavity (21) have been seted up to the interior roof of mounting groove (13), the inside sliding connection of cavity (21) has extrusion piece (22), fifth spout (23) have been seted up to the inside wall fixedly connected with connecting rod (24) of cavity (21), the top fixedly connected with slide bar (25) of extrusion piece (22), the top fixedly connected with fixed disk (26) of slide bar (25).
5. The unmanned aerial vehicle protective bracket of claim 4, wherein: the width of the mounting groove (13) is larger than that of the mounting block (14), and a reset spring is fixedly connected to the top of the sliding block (17).
6. The unmanned aerial vehicle protective bracket of claim 4, wherein: the clamping block (19) and the clamping groove (20) are clamped and fixed, and the extrusion block (22) and the mounting block (14) are mutually perpendicular.
7. The unmanned aerial vehicle protective bracket of claim 4, wherein: the top of the extrusion block (22) is fixedly connected with a telescopic spring, and the connecting rod (24) is in sliding connection with the fifth sliding groove (23).
CN202322549541.7U 2023-09-20 2023-09-20 Unmanned aerial vehicle protects support Active CN221214656U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202322549541.7U CN221214656U (en) 2023-09-20 2023-09-20 Unmanned aerial vehicle protects support

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202322549541.7U CN221214656U (en) 2023-09-20 2023-09-20 Unmanned aerial vehicle protects support

Publications (1)

Publication Number Publication Date
CN221214656U true CN221214656U (en) 2024-06-25

Family

ID=91542601

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202322549541.7U Active CN221214656U (en) 2023-09-20 2023-09-20 Unmanned aerial vehicle protects support

Country Status (1)

Country Link
CN (1) CN221214656U (en)

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