CN215867082U - Radar support - Google Patents
Radar support Download PDFInfo
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- CN215867082U CN215867082U CN202121730041.8U CN202121730041U CN215867082U CN 215867082 U CN215867082 U CN 215867082U CN 202121730041 U CN202121730041 U CN 202121730041U CN 215867082 U CN215867082 U CN 215867082U
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Abstract
The utility model discloses a radar support and relates to the technical field of radar supports. The utility model comprises a base plate; the top of the bottom plate is fixedly connected with a U-shaped support frame; the middle part of the U-shaped supporting frame is fixedly connected with a central column; a support column is rotatably connected inside the central column; one end of the support column is fixedly connected with a first turbine; the other end of the supporting column is fixedly connected with a top plate; two ends of the top plate are fixedly connected with side plates; the two side plates are rotatably connected with a rotating rod relative to the inner wall; the circumferential side surface of the rotating rod is fixedly connected with a connecting seat; the top of the connecting seat is fixedly connected with a supporting rod; the edge of the top end of the supporting rod is fixedly connected with a limiting block; a radar antenna seat is fixedly connected between the top of the supporting rod and the limiting block through a nut; the inside rotation of support column is connected with the pivot. According to the utility model, the first worm and the first turbine are driven by the first servo motor to be in meshing transmission with each other, so that the radar antenna base is driven to rotate, different angles can be conveniently adjusted, and the effects of more stable, quicker and more convenient steering of the radar antenna are achieved.
Description
Technical Field
The utility model belongs to the technical field of radar supports, and particularly relates to a radar support.
Background
Radar, which, in order to achieve "radio detection and ranging", finds objects and determines their spatial position by means of radio. Therefore, radar is also referred to as "radiolocation". Radars are electronic devices that detect objects using electromagnetic waves. The radar emits electromagnetic waves to irradiate the target and receives the echo of the target, so that information such as the distance from the target to an electromagnetic wave emission point, the distance change rate, the azimuth and the height is obtained.
Current radar support and radar are generally all through bolt fixed connection, and support itself also is fixed structure simultaneously, and the flexibility is relatively poor in daily use, can't adjust detection angle according to actual need in real time, use very inconvenient.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a radar support, which solves the problem of poor radar angle adjustment and flexibility by matching a bottom plate, a U-shaped support frame, a central column, a support column, a rotating rod and a radar antenna base.
In order to solve the technical problems, the utility model is realized by the following technical scheme:
the utility model relates to a radar bracket, which comprises a bottom plate; the top of the bottom plate is fixedly connected with a U-shaped support frame; the middle part of the U-shaped supporting frame is fixedly connected with a central column; a support column is rotatably connected inside the central column; one end of the supporting column is fixedly connected with a first turbine; the other end of the supporting column is fixedly connected with a top plate; two ends of the top plate are fixedly connected with side plates; the two side plates are rotatably connected with a rotating rod relative to the inner wall; the circumferential side surface of the rotating rod is fixedly connected with a connecting seat; the top of the connecting seat is fixedly connected with a supporting rod; the edge of the top end of the supporting rod is fixedly connected with a limiting block; a radar antenna seat is fixedly connected between the top of the supporting rod and the limiting block through a nut; a first bevel gear is fixedly connected to the circumferential side surface of the rotating rod and positioned on one side of the connecting seat; the inside rotation of support column is connected with the pivot.
Furthermore, connecting blocks are fixedly connected to two sides of the U-shaped supporting frame; the opposite inner walls of the two connecting blocks are fixedly connected with connecting lugs; the opposite inner walls of the two connecting lugs are respectively and rotatably connected with a first worm and a second worm.
Furthermore, a first servo motor is fixedly connected to one side edge of the bottom plate through a bolt; the rotating shaft end of the first servo motor is fixedly connected with one end of the first worm; the first worm and the first worm wheel are in meshing transmission with each other; a second servo motor is fixedly installed on the edge of one side, far away from the U-shaped support frame, of the bottom plate through a bolt; and the rotating shaft end of the second servo motor is fixedly connected with one end of the second worm.
Further, the central column is of a hollow structure; the top of the central column is provided with a first through hole matched with the support column.
Furthermore, a second through hole matched with the rotating shaft is formed in the middle of the top end of the top plate.
Further, a second bevel gear is fixedly connected to the top end of the rotating shaft; the second bevel gear and the first bevel gear are in meshing transmission with each other; a second turbine is fixedly connected to the bottom end of the rotating shaft and close to the bottom of the first turbine; the first worm wheel and the second worm are in meshing transmission with each other.
The utility model has the following beneficial effects:
1. according to the utility model, the bottom plate, the U-shaped support frame, the central column, the support column, the radar antenna pedestal and the first servo motor are matched, and the first worm and the first turbine are driven by the first servo motor to be in meshing transmission with each other, so that the support column and the radar antenna pedestal are driven to rotate, and different angles can be conveniently adjusted, thereby achieving the effects of more stable, quicker and more convenient steering of the radar antenna.
2. According to the utility model, the bottom plate, the U-shaped support frame, the central column, the support column, the rotating rod, the radar antenna pedestal and the second servo motor are matched, the second worm and the second worm wheel are driven by the second servo motor to be in meshing transmission with each other, so that the rotating shaft is driven to rotate, and the second bevel gear and the first bevel gear are in meshing transmission with each other, so that the reciprocating motion of the radar antenna pedestal is conveniently adjusted, the radar can be quantitatively adjusted, the high-precision adjustment of the position of the radar is realized, the operation is convenient, and the practicability is strong.
Of course, it is not necessary for any product in which the utility model is practiced to achieve all of the above-described advantages at the same time.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to the drawings without creative efforts.
FIG. 1 is a schematic structural view of a radar mount according to the present invention;
FIG. 2 is a cross-sectional view of a structural schematic diagram of a radar mount;
FIG. 3 is a schematic structural view of a base plate;
FIG. 4 is a schematic structural diagram of a support column;
FIG. 5 is a schematic structural view of the rotary rod;
FIG. 6 is a schematic structural view of the spindle;
in the drawings, the components represented by the respective reference numerals are listed below:
1-bottom plate, 2-U-shaped support frame, 3-center column, 4-support column, 5-rotating rod, 6-radar antenna seat, 7-rotating shaft, 8-first worm, 9-second worm, 10-first servo motor, 11-second servo motor, 201-connecting block, 202-connecting lug, 301-first through hole, 401-first turbine, 402-top plate, 403-side plate, 404-second through hole, 501-connecting seat, 502-support rod, 503-limiting block, 504-first bevel gear, 701-second bevel gear and 702-second turbine.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1 to 6, the present invention is a radar mount, including a base plate 1; the top of the bottom plate 1 is fixedly connected with a U-shaped support frame 2; the middle part of the U-shaped supporting frame 2 is fixedly connected with a central column 3; a support column 4 is rotatably connected inside the central column 3; one end of the support column 4 is fixedly connected with a first turbine 401; the other end of the support column 4 is fixedly connected with a top plate 402; two ends of the top plate 402 are fixedly connected with side plates 403; the two side plates 403 are rotatably connected with a rotating rod 5 relative to the inner wall; the peripheral side surface of the rotating rod 5 is fixedly connected with a connecting seat 501; the top of the connecting seat 501 is fixedly connected with a supporting rod 502; the edge of the top end of the support rod 502 is fixedly connected with a limit block 503; a radar antenna seat 6 is fixedly connected between the top of the support rod 502 and the limiting block 503 through a nut; a first bevel gear 504 is fixedly connected to the 5-circumference side surface of the rotating rod and positioned at one side of the connecting seat 501; a rotating shaft 7 is rotatably connected inside the supporting column 3; a first servo motor 10 is fixedly connected to one side edge of the bottom plate 1 through a bolt; the rotating shaft end of the first servo motor 10 is fixedly connected with one end of the first worm 8; the first worm 8 and the first worm wheel 401 are in meshing transmission with each other; a second servo motor 11 is fixedly installed on the edge of one side, far away from the U-shaped support frame 2, of the bottom plate 1 through bolts; the rotating shaft end of the second servo motor 11 is fixedly connected with one end of the second worm 9; the first worm 8 is driven by the first servo motor 10 to rotate, so that the first worm 8 and the first turbine 401 are in meshing transmission with each other, the support column 4, the top plate 402 and the side plate 403 are driven to rotate, and the effect that the radar antenna pedestal 6 is more stable, faster and more convenient to steer is achieved; then, the second worm 9 is driven to rotate by the second servo motor 11, so that the second worm 9 and the second worm wheel 702 are in meshing transmission with each other, the second bevel gear 701 and the first bevel gear 504 are in meshing transmission with each other, the rotating rod 5 is driven to rotate, parameters such as an adjusting angle, a distance and a position can be directly read, the radar can be quantitatively adjusted, and high-precision adjustment of the position of the radar is achieved.
Wherein, the two sides of the U-shaped supporting frame 2 are fixedly connected with connecting blocks 201; the opposite inner walls of the two connecting blocks 201 are fixedly connected with connecting lugs 202; the opposite inner walls of the two connecting lugs 202 are respectively connected with a first worm 8 and a second worm 9 in a rotating way; the connecting block 201 and the connecting lug 202 are convenient for fixing the first worm 8 and the second worm 9 and prevent the first worm and the second worm from shifting during rotation.
Wherein, the central column 3 is a hollow structure; the top of the central column 3 is provided with a first through hole 301 matched with the support column 4; the first through hole 301 is found offset when the column 3 is rotated.
Wherein, the middle part of the top end of the top plate 402 is provided with a second through hole 404 matched with the rotating shaft 7; the second through hole 404 facilitates the deviation of the rotating shaft 7 during rotation, thereby greatly enhancing the stability of the rotation of the radar antenna pedestal 6.
Wherein, the top end of the rotating shaft 7 is fixedly connected with a second bevel gear 701; the second bevel gear 701 and the first bevel gear 504 are in meshing transmission with each other; a second turbine 702 is fixedly connected to the bottom end of the rotating shaft 7 and close to the bottom of the first turbine 401; the first worm wheel 702 and the second worm 9 are in meshed transmission with each other; the first bevel gear 701 and the second bevel gear 501 are in meshing transmission with each other, so that the angle of the radar antenna pedestal 6 can be conveniently adjusted, and information can be conveniently collected.
One specific application of this embodiment is: when the radar antenna pedestal is used, the first worm 8 is driven to rotate by the first servo motor 10, so that the first worm 8 and the first turbine 401 are in meshing transmission with each other, the supporting column 4, the top plate 402 and the side plate 403 are driven to rotate, and the effect that the radar antenna pedestal 6 is more stable, faster and more convenient to steer is achieved; then, the second worm 9 is driven to rotate by the second servo motor 11, so that the second worm 9 and the second worm wheel 702 are in meshing transmission with each other, the second bevel gear 701 and the first bevel gear 504 are in meshing transmission with each other, the rotating rod 5 is driven to rotate, parameters such as an adjusting angle, a distance and a position can be directly read, the radar can be quantitatively adjusted, and high-precision adjustment of the position of the radar is achieved.
In the description herein, references to the description of "one embodiment," "an example," "a specific example" or the like are intended to mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the utility model. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The preferred embodiments of the utility model disclosed above are intended to be illustrative only. The preferred embodiments are not intended to be exhaustive or to limit the utility model to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the utility model and the practical application, to thereby enable others skilled in the art to best utilize the utility model. The utility model is limited only by the claims and their full scope and equivalents.
Claims (6)
1. A radar support comprises a bottom plate (1),
the method is characterized in that:
the top of the bottom plate (1) is fixedly connected with a U-shaped support frame (2); the middle part of the U-shaped supporting frame (2) is fixedly connected with a central column (3); a support column (4) is rotatably connected inside the central column (3);
one end of the supporting column (4) is fixedly connected with a first turbine (401); the other end of the supporting column (4) is fixedly connected with a top plate (402); two ends of the top plate (402) are fixedly connected with side plates (403); the two side plates (403) are rotatably connected with a rotating rod (5) relative to the inner wall;
the peripheral side surface of the rotating rod (5) is fixedly connected with a connecting seat (501); the top of the connecting seat (501) is fixedly connected with a supporting rod (502); the edge of the top end of the support rod (502) is fixedly connected with a limit block (503); a radar antenna seat (6) is fixedly connected between the top of the supporting rod (502) and the limiting block (503) through a nut; a first bevel gear (504) is fixedly connected to the circumferential side surface of the rotating rod (5) and positioned on one side of the connecting seat (501);
the supporting column (4) is internally and rotatably connected with a rotating shaft (7).
2. A radar stand according to claim 1, characterized in that the U-shaped supporting frame (2) is fixedly connected with connecting blocks (201) at two sides; the opposite inner walls of the two connecting blocks (201) are fixedly connected with connecting lugs (202); the two connecting lugs (202) are respectively connected with a first worm (8) and a second worm (9) in a rotating way relative to the inner wall.
3. The radar support according to claim 2, characterized in that a first servo motor (10) is fixedly connected to one side edge of the bottom plate (1) through a bolt; the rotating shaft end of the first servo motor (10) is fixedly connected with one end of the first worm (8); the first worm (8) and the first worm wheel (401) are in meshed transmission with each other; a second servo motor (11) is fixedly installed on the edge of one side, far away from the U-shaped support frame (2), of the bottom plate (1) through a bolt; and the rotating shaft end of the second servo motor (11) is fixedly connected with one end of the second worm (9).
4. A radar stand according to claim 1, characterised in that the central column (3) is of a "hollow" construction; the top of the central column (3) is provided with a first through hole (301) matched with the support column (4).
5. The radar bracket as recited in claim 1, wherein a second through hole (404) is formed in a middle portion of a top end of the top plate (402) and is matched with the rotating shaft (7).
6. The radar support according to claim 5, wherein a second bevel gear (701) is fixedly connected to the top end of the rotating shaft (7); the second bevel gear (701) and the first bevel gear (504) are in meshing transmission with each other; a second turbine (702) is fixedly connected to the bottom end of the rotating shaft (7) and close to the bottom of the first turbine (401); the second worm wheel (702) and the second worm (9) are in meshed transmission with each other.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121730041.8U CN215867082U (en) | 2021-07-28 | 2021-07-28 | Radar support |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121730041.8U CN215867082U (en) | 2021-07-28 | 2021-07-28 | Radar support |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215867082U true CN215867082U (en) | 2022-02-18 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121730041.8U Active CN215867082U (en) | 2021-07-28 | 2021-07-28 | Radar support |
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| Country | Link |
|---|---|
| CN (1) | CN215867082U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115195624A (en) * | 2022-09-06 | 2022-10-18 | 之江实验室 | Adjustable laser radar installing support |
-
2021
- 2021-07-28 CN CN202121730041.8U patent/CN215867082U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115195624A (en) * | 2022-09-06 | 2022-10-18 | 之江实验室 | Adjustable laser radar installing support |
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