CN212657457U - Unmanned aerial vehicle is antidetonation formula support for jammer - Google Patents
Unmanned aerial vehicle is antidetonation formula support for jammer Download PDFInfo
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- CN212657457U CN212657457U CN201922359729.9U CN201922359729U CN212657457U CN 212657457 U CN212657457 U CN 212657457U CN 201922359729 U CN201922359729 U CN 201922359729U CN 212657457 U CN212657457 U CN 212657457U
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Abstract
The utility model discloses an unmanned aerial vehicle interference utensils antidetonation formula support relates to unmanned aerial vehicle support equipment field, the camera includes a supporting plate, the bracing piece downside is provided with the pipe, be provided with damping spring in the pipe, the damping spring suit is at the bracing piece lower extreme, be provided with the clamp plate on the bracing piece, the clamp plate is located the damping spring upper surface, the pipe downside is provided with the base, the base right-hand member is provided with first bolt, first bolt left end runs through base and pipe and extends to the base left end, the backup pad upper surface is provided with the casing, both ends all are fixed with the connecting plate about the casing of telling, the connecting plate upper end is provided with the second bolt, second bolt lower extreme runs through connecting plate and backup pad, be provided with the sleeve in the casing, be provided with the spring in the sleeve. The utility model discloses the shock attenuation is effectual, improves and disturbs the precision, is convenient for adjust the height, and the dismouting of being convenient for is accomodate, and the practicality is strong.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle support equipment field especially relates to an unmanned aerial vehicle is antidetonation formula support for jammer.
Background
All current civil unmanned aerial vehicles all need use radio technology to realize functions such as location, remote control, image transmission. Of course, some special-purpose drones can determine their own position by methods such as terrain matching, image recognition and high-precision inertial navigation, and perform tasks autonomously, but the unmanned drone is not popular in the civil field. Now that the drone must use radio technology, the drone jammers can be used to interfere with the radio, thus reaching the goal of causing the drone to be out of control or to turn back. Traditional unmanned aerial vehicle interference ware support can not carry out the shock attenuation when placing, leads to disturbing making the precision to unmanned aerial vehicle and reduces, and personnel's of not being convenient for use, greatly reduced the practicality. Therefore, the problem is solved by providing the anti-seismic support for the unmanned aerial vehicle interference device.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the anti-seismic support for unmanned aerial vehicle interference unit that proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme: an anti-seismic support for an Unmanned Aerial Vehicle (UAV) jammer comprises a support plate, wherein lug plates are fixed on the lower surface of the support plate in a welded manner, a support rod is arranged between the lug plates, a screw rod is arranged in each lug plate, one end of the screw rod penetrates through each lug plate and the support rod, a round pipe is arranged on the lower side of each support rod, a damping spring is arranged in each round pipe, the damping spring is sleeved at the lower end of each support rod, a pressing plate is arranged on each support rod and is positioned on the upper surface of each damping spring, a base is arranged on the lower side of each round pipe, a first bolt is arranged at the right end of each base, the left end of each first bolt penetrates through each base and each round pipe and extends to the left end of each base, a shell is arranged on the upper surface of the support plate, the improved structure of the automobile seat is characterized in that a sleeve is arranged in the shell, a spring is arranged in the sleeve, a pressing rod is arranged on the upper surface of the spring, a connecting frame is fixed on the upper surface of the pressing rod, a limiting rod is fixed on the lower surface of the connecting frame, and one end of the limiting rod penetrates through the shell and the supporting plate and extends to the lower side of the supporting plate.
Preferably, the otic placode is provided with three pairs, three pairs the otic placode annular weld fixation is in the backup pad lower surface, and three pairs the contained angle between the otic placode is 60.
Preferably, the round tube is internally provided with a limiting ring, the damping spring is arranged on the limiting ring, and the lower end of the support rod penetrates through the damping spring and the limiting ring.
Preferably, the upper surface of the shell is provided with a through groove, the limiting rod is T-shaped, and the upper end of the limiting rod penetrates through the supporting plate and the shell and extends to the lower surface of the connecting frame.
Preferably, the upper surface of the support plate is provided with a threaded hole, the upper surface of the connecting plate is provided with a through hole, and the connecting plate is fixedly connected with the support plate through a second bolt and the threaded hole.
The utility model has the advantages that: be connected with outside unmanned aerial vehicle interference unit through the link, make the casing fixed through connecting plate and second bolt, the vibrations that make to receive through depression bar and spring can only reciprocate, through otic placode and screw rod, damping spring, structural component such as base and first bolt, the vibrations dispersion that makes to receive is to all around to realize improving the shock attenuation effect.
The utility model discloses the shock attenuation is effectual, improves and disturbs the precision, is convenient for adjust the height, and the dismouting of being convenient for is accomodate, and the practicality is strong, excellent in use effect.
Drawings
Fig. 1 is the utility model provides a front view of unmanned aerial vehicle is antidetonation formula support for jammer.
Fig. 2 is the utility model provides a top view of antidetonation formula support for unmanned aerial vehicle interferometer.
Reference numbers in the figures: the damping device comprises a sleeve 1, a spring 2, a supporting plate 3, an ear plate 4, a screw rod 5, a supporting rod 6, a round tube 7, a pressing plate 8, a damping spring 9, a first bolt 10, a base 11, a second bolt 12, a connecting plate 13, a shell 14, a limiting rod 15, a connecting frame 16 and a pressing rod 17.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Referring to fig. 1 and 2, an anti-vibration support for an Unmanned Aerial Vehicle (UAV) jammer comprises a support plate 3, wherein lug plates 4 are welded and fixed on the lower surface of the support plate 3, support rods 6 are arranged between the lug plates 4, screw rods 5 are arranged in the lug plates 4, one ends of the screw rods 5 penetrate through the lug plates 4 and the support rods 6, a round tube 7 is arranged on the lower side of the support rods 6, a damping spring 9 is arranged in the round tube 7, the damping spring 9 is sleeved at the lower end of the support rod 3, a pressing plate 8 is arranged on the support rod 3, the pressing plate 8 is positioned on the upper surface of the damping spring 9, a base 11 is arranged on the lower side of the round tube 7, a first bolt 10 is arranged at the right end of the base 11, the left end of the first bolt 10 penetrates through the base 11 and the round tube 7 and extends to the left end of the base 11, a shell 14 is arranged, be provided with sleeve 1 in the casing 14, be provided with spring 2 in the sleeve 1, 2 upper surfaces of spring are provided with depression bar 17, depression bar 17 upper surface is fixed with link 16, 16 lower fixed surface of link has gag lever post 15, gag lever post 15 one end runs through casing 14 and backup pad 3 and extends to 3 downside of backup pad, be connected with outside unmanned aerial vehicle interference ware through link 16, it is fixed to make casing 14 through connecting plate 13 and second bolt 12, the vibrations that make to receive through depression bar 17 and spring 2 can only reciprocate, through otic placode 4 and screw rod 5, damping spring 9, structural component such as base 11 and first bolt 10, the vibrations dispersion that make to receive is to all around, thereby realize improving the shock attenuation effect.
The ear plates 4 are provided with three pairs, the three pairs of ear plates 4 are welded and fixed on the lower surface of the supporting plate 3 in an annular mode, included angles among the three pairs of ear plates 4 are 60 degrees, and the effect of the design is improved when the supporting is carried out.
Be provided with the spacing ring in the pipe 7, damping spring 9 sets up on the spacing ring, and damping spring 9 and spacing ring are run through to 6 lower extremes of bracing piece, and this design realizes supporting damping spring 9, makes bracing piece 6 have buffer space simultaneously.
Through groove has been seted up to casing 14 upper surface, and gag lever post 15 is the T type, and 15 upper ends of gag lever post run through backup pad 3 and casing 14 and extend to link 16 lower surfaces, and this design has realized that link 16 can only reciprocate.
Threaded hole has been seted up to backup pad 3 upper surface, and the through-hole has been seted up to connecting plate 13 upper surface, and connecting plate 13 passes through second bolt 12 and threaded hole fixed connection with backup pad 3, and this design is convenient for fixed connection board 13, and then fixed casing 14.
The working principle is as follows: when the device is used, firstly, the base 11 and the round tube 7 are fixed through the first bolt 10, and the three bases 11 are positioned on the same plane, the support plate 3 is positioned at a proper height by rotating the support rod 6, then the upper end of the support rod 6 is fixed by the screw rod 5, so as to realize the height adjustment of the support plate 3, then a user connects the connecting frame 16 with an external unmanned aerial vehicle interference device, when external vibration is generated, the limiting rod 15 enables the connecting frame 16 to only move up and down through the compression rod 17 and the compression spring 2, the vibration is transmitted to the support plate 3 and is transmitted to the round tube 7 through the support rod 6, the support rod 6 and the compression spring 2 through the pressing plate 8, simultaneously, the vibration strength is dispersed to all directions through the inclination angle of the round tube 7 and then transmitted to the base 11, so as to realize the vibration reduction, the utility model discloses the shock absorption effect, the practicability is strong and the using effect is good.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (5)
1. The utility model provides an unmanned aerial vehicle is antidetonation formula support for jammer, includes backup pad (3), backup pad (3) lower surface welded fastening has otic placode (4), its characterized in that, be provided with bracing piece (6) between otic placode (4), be provided with screw rod (5) in otic placode (4), screw rod (5) one end runs through otic placode (4) and bracing piece (6), bracing piece (6) downside is provided with pipe (7), be provided with damping spring (9) in pipe (7), damping spring (9) suit is at bracing piece (6) lower extreme, be provided with clamp plate (8) on bracing piece (6), clamp plate (8) are located damping spring (9) upper surface, pipe (7) downside is provided with base (11), base (11) right-hand member is provided with first bolt (10), first bolt (10) left end runs through base (11) and pipe (7) and extends to base (11) left end, the utility model discloses a support plate, including backup pad (3), connecting plate (13) all are fixed with at both ends about the casing (14) of telling, connecting plate (13) upper end is provided with second bolt (12), second bolt (12) lower extreme runs through connecting plate (13) and backup pad (3), be provided with sleeve (1) in casing (14), be provided with spring (2) in sleeve (1), spring (2) upper surface is provided with depression bar (17), depression bar (17) upper surface fixed has link (16), link (16) lower fixed surface is with gag lever post (15), gag lever post (15) one end runs through casing (14) and backup pad (3) and extends to backup pad (3) downside.
2. The anti-seismic support for the unmanned aerial vehicle jammer according to claim 1, characterized in that the ear plates (4) are provided with three pairs, the three pairs of ear plates (4) are welded and fixed on the lower surface of the support plate (3) in an annular manner, and the included angles between the three pairs of ear plates (4) are 60 degrees.
3. The anti-seismic support for the unmanned aerial vehicle jammer according to claim 1, wherein a limit ring is arranged in the circular tube (7), the damping spring (9) is arranged on the limit ring, and the lower end of the support rod (6) penetrates through the damping spring (9) and the limit ring.
4. The anti-seismic support for the unmanned aerial vehicle jammer according to claim 1, wherein a through groove is formed in the upper surface of the shell (14), the limiting rod (15) is T-shaped, and the upper end of the limiting rod (15) penetrates through the support plate (3) and the shell (14) and extends to the lower surface of the connecting frame (16).
5. The anti-seismic support for the unmanned aerial vehicle jammer according to claim 1, wherein a threaded hole is formed in the upper surface of the support plate (3), a through hole is formed in the upper surface of the connecting plate (13), and the connecting plate (13) is fixedly connected with the support plate (3) through the second bolt (12) and the threaded hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922359729.9U CN212657457U (en) | 2019-12-25 | 2019-12-25 | Unmanned aerial vehicle is antidetonation formula support for jammer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922359729.9U CN212657457U (en) | 2019-12-25 | 2019-12-25 | Unmanned aerial vehicle is antidetonation formula support for jammer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212657457U true CN212657457U (en) | 2021-03-05 |
Family
ID=74766541
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922359729.9U Active CN212657457U (en) | 2019-12-25 | 2019-12-25 | Unmanned aerial vehicle is antidetonation formula support for jammer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212657457U (en) |
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2019
- 2019-12-25 CN CN201922359729.9U patent/CN212657457U/en active Active
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