CN210864031U - Radar test structure with automatic every single move function - Google Patents
Radar test structure with automatic every single move function Download PDFInfo
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- CN210864031U CN210864031U CN201921314409.5U CN201921314409U CN210864031U CN 210864031 U CN210864031 U CN 210864031U CN 201921314409 U CN201921314409 U CN 201921314409U CN 210864031 U CN210864031 U CN 210864031U
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Abstract
The utility model discloses a radar test structure with automatic every single move function, a serial communication port, include: a radar array plane (1); the driving motor (3) is arranged on one side of the radar array surface (1), is mechanically connected with the radar array surface (1), and is used for driving the radar array surface (1) to rotate so as to form a set pitch angle with the horizontal plane; and the instrument panel (4) with 360 degrees is arranged on the other side of the radar array surface (1) and is mechanically connected with the radar array surface (1). Driving motor (3) drive radar array face (1) and rotate according to setting for the angle through the cylinder pole that sets up on radar array face adapter (6) fixed, and simultaneously, the rotation of radar array face (1) also drives 360 degrees panel boards (4) through radar array face adapter (6) and rotates for confirm and the calibration sets for the angle of pitch.
Description
Technical Field
The utility model relates to a radar test structure especially relates to a radar test structure with automatic every single move function.
Background
In the debugging and testing process of the foundation radar in the prior art, the pitching angle of the radar is required to be easy to adjust, the locking is firm, and no backlash exists in the rotating process; meanwhile, the portable multifunctional chair is easy to disassemble and assemble, portable and portable; at present, most of radar test structures are manual test platforms, and no radar test automatic pitching debugging structure with an automatic pitching adjusting structure exists.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
The utility model provides a radar test structure with automatic every single move function to at least part solves the problem that the radar can not the automatic adjustment pitch angle among the prior art.
(II) technical scheme
According to the utility model discloses an aspect provides a radar test structure with automatic every single move function, a serial communication port, include: a radar array face 1; the driving motor 3 is arranged on one side of the radar array surface 1, is mechanically connected with the radar array surface 1, and is used for driving the radar array surface 1 to rotate so as to form a set pitch angle with a horizontal plane; and a radar test support 2 for supporting radar array face 1 and driving motor 3, and then fix radar array face 1 and driving motor 3 on the horizontal plane, radar test support 2 includes a left side board, a right side board and a bottom plate, wherein, the both ends of bottom plate are located to left side board and right side board branch, and the top respectively has a recess.
The driving motor 3 is further provided with a cylindrical rod, the tail end of the cylindrical rod is mechanically connected with the radar front 1 through a radar front adapter 6, and the body part of the cylindrical rod is embedded in a groove in the top end of the left side plate of the radar test support 2 and used for fixing the radar front 1 on the radar test support 2.
In a further scheme, the radar structure further comprises a 360-degree instrument panel 4 for confirming and calibrating a set pitch angle, wherein one disc surface of the 360-degree instrument panel 4 is mechanically connected with the radar front 1 through a radar front adapter 6, the other disc surface is provided with a cylindrical rod, and the body part of the cylindrical rod is embedded and clamped in a groove on the right side plate of the radar test support 2 and used for fixing the radar front 1 on the radar test support 2.
In a further scheme, the radar test structure further comprises an instrument pointer 5 horizontally arranged at the top end of the right side plate of the radar test support 2 and used for indicating the rotating pitch angle of the radar array surface 1 together with the 360-degree instrument panel 4.
In a further scheme, the radar structure further includes an antenna support rod 7 disposed at a top end of the radar front 1, where the antenna support rod 7 and the radar front 1 are located on the same plane; two test antennas 10 respectively arranged at two ends of the antenna support rod 7; and a laser pen light calibrating device 8, set up in the top of radar array face 1, laser pen light calibrating device 8 includes two laser beam locating holes and a laser pen 9, sets up on laser pen light calibrating device 8.
(III) advantageous effects
According to the above technical scheme, the utility model provides a pair of radar test structure with automatic every single move function, driving motor sets up the cylinder pole on the adapter of radar array face through fixed, drives the radar array face and rotates according to setting for the angle, and then drives the rotation that the antenna carries out the same angle through the antenna support pole, and simultaneously, the rotation of radar array face also drives 360 degrees panel boards through the adapter of radar array face and rotates for confirm with the angle of pitch of calibration setting.
Drawings
Fig. 1 is a schematic diagram of a radar test structure with an automatic pitch function according to an embodiment of the present invention.
Fig. 2 is a schematic illustration of the radar front of the structure shown in fig. 1.
Fig. 3 is a schematic diagram of a radar front adapter of the structure shown in fig. 1.
Fig. 4 is a schematic view of a driving motor of the structure shown in fig. 1.
Fig. 5 is a schematic view of the 360 degree instrument panel and gauge pointer of the configuration of fig. 1.
Fig. 6 is a diagram illustrating the effect of adjusting the elevation angle shown in fig. 1.
[ description of reference ]
1-radar array surface, 2-radar test bracket, 3-driving motor, 4-360 degree instrument panel,
5-meter pointer, 6-radar array adapter, 7-antenna support rod,
8-laser pen light calibration device, 9-laser pen, 10-test antenna
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in detail with reference to the accompanying drawings.
In the present invention, "disposed on" or "attached to" is used to include direct contact relationships with a single or multiple components. Furthermore, the use of ordinal numbers such as "first," "second," "first," or "second," etc., in the description and in the claims to modify a claimed element, does not by itself connote any preceding ordinal number, nor is the order in which a particular element is presented or the order in which it is manufactured, but are used merely to distinguish one element having a certain name from another element having a same name.
The utility model provides a radar test structure with automatic every single move function, driving motor locates the cylinder pole in the radar array face adapter through the spiral shell, drives the radar array face and rotates according to setting for the angle, and then drives the antenna through antenna support pole and carry out the rotation of the same angle, and simultaneously, the rotation of radar array face also drives 360 degrees panel boards through radar array face adapter and rotates for confirm and calibrate the angle of pitch of setting for.
Fig. 1 is a schematic diagram of a radar test structure with an automatic pitching function according to an embodiment of the present invention, as shown in fig. 1, including:
a radar array face 1; the driving motor 3 is arranged on one side of the radar array surface 1, is mechanically connected with the radar array surface 1 and is used for driving the radar array surface 1 to rotate so as to form a set pitch angle with the horizontal plane; and a radar test support 2 for support radar array face 1 and driving motor 3, and then fix radar array face 1 and driving motor 3 on the horizontal plane, radar test support 2 includes a left side board, a right side board and a bottom plate, wherein, the both ends of bottom plate are located to left side board and right side board branch, and the top respectively has a recess, in this embodiment, left side board and right side board are respectively through fix with screw on the bottom plate, simultaneously, still set up a set-square respectively in the junction of left side board and bottom plate and right side board and bottom plate for the fixed effect of reinforcing.
The driving motor 3 is further provided with a cylindrical rod, the tail end of the cylindrical rod is mechanically connected with the radar front face 1 through a radar front face adapter 6, the body part of the cylindrical rod is embedded in a groove in the top end of a left side plate of the radar test support 2 and used for fixing the radar front face 1 on the radar test support 2, in the embodiment, a plurality of screw holes are formed in the left side plate, and the driving motor 3 is screwed on the left side plate through the screw holes.
In the exemplary embodiment of the present invention, the radar test structure further includes a 360-degree dashboard 4 for confirming and calibrating the set pitch angle, wherein a panel of the 360-degree dashboard 4 is mechanically connected to the radar front 1 through a radar front adapter 6, and another panel is configured with a cylindrical rod, the cylindrical rod is embedded in a groove on the right side plate of the radar test support 2 for fixing the radar front 1 on the radar test support 2, and a meter pointer 5 is horizontally arranged on the top end of the right side plate of the radar test support 2 for indicating the pitch angle of the rotation of the radar front 1 together with the 360-degree dashboard 4, in this embodiment, a plurality of screw holes are provided on the right side plate, the meter pointer 5 is fixed on the right side plate through the screw holes, when the driving motor 3 drives the radar front 1 to rotate according to the set pitch angle, the rotation of the radar array face 1 also drives the 360-degree instrument panel 4 to rotate through the radar array face adapter 6, and the instrument pointer 5 can point to the corresponding angle marked on the 360-degree instrument panel 4.
In addition, the radar structure further comprises an antenna support rod 7 arranged at the top end of the radar front 1, and the antenna support rod 7 and the radar front 1 are located on the same plane; two test antennas 10 respectively arranged at two ends of the antenna support rod 7; and a laser pen light calibrating device 8, set up in the top of radar array face 1, laser pen light calibrating device 8 includes two laser beam locating holes and a laser pen 9, sets up on laser pen light calibrating device 8.
In this embodiment, antenna support 7 passes through the screw fixation on radar front 1, and two test antennas 10 pass through the screw fixation on antenna support 7, when driving motor 3 drove radar front 1 and rotate according to setting for the angle, antenna support 7 and test antenna 10 also rotated the same angle along with radar front 1.
Simultaneously, laser pen light calibrating device 8 also passes through the screw fixation on radar array face 1, laser pen 9 passes through the screw fixation on laser pen light calibrating device 8, when driving motor 3 drives radar array face 1 and rotates according to setting for the angle, laser pen light calibrating device 8 also rotates the same angle along with radar array face 1, and then drive laser pen 9 and rotate the same angle, laser pen 9 is beaten the light beam through two laser beam locating holes of laser calibrating device 8, shine the target of being surveyed, help test antenna 10's test work.
Fig. 2 is a schematic view of the radar array plane with the structure shown in fig. 1, as shown in fig. 2, in this embodiment, the radar array plane 1 is a square, the left and right sides of the radar array plane are respectively provided with an accommodating port for accommodating the radar array plane adapter 6, and the outer side of the accommodating port is further provided with a plurality of screw holes for fixing the radar array plane adapter 6 to the accommodating ports.
Fig. 3 is a schematic diagram of the radar front adapter of the structure shown in fig. 1, as shown in fig. 3, the radar front adapter 6 includes a rectangular rod, two ends of the rectangular rod are respectively provided with a rectangular block, the rectangular block is provided with a screw hole, the two rectangular blocks can penetrate into the upper and lower ends of the receiving opening of the radar front 1, and simultaneously, the rectangular rod can be fixed in the receiving opening by screws, in addition, the rectangular rod body is also fixedly provided with a disc, and the disc is provided with a plurality of screw holes.
Fig. 4 is a schematic diagram of the driving motor with the structure shown in fig. 1, as shown in fig. 4, a disc is further configured at the tail end of the cylindrical rod of the driving motor 3, a plurality of screw holes are formed in the disc, the radar front adapter 6 located on the left side plate of the radar test support 2 is fixed with the disc through screws, no backlash is guaranteed in the rotating process, and meanwhile, the cylindrical rod body is embedded and clamped in a groove in the top end of the left side plate of the radar test support 2 and used for fixing the radar front 1 on the radar test support 2.
Fig. 5 is a schematic diagram of the 360-degree instrument panel and the instrument pointer of the structure shown in fig. 1, as shown in fig. 5, a radar front adapter 6 located on the right side plate of the radar test support 2 is fixed with a disc surface of the 360-degree instrument panel 4 through screws, and another disc surface is configured with a cylindrical rod, the cylindrical rod is embedded and clamped in a groove on the right side plate of the radar test support 2 for fixing the radar front 1 on the radar test support 2, meanwhile, a plurality of screw holes are arranged on the right side plate, the instrument pointer 5 is fixed on the right side plate through the screw holes, when the radar front 1 is perpendicular to the horizontal plane, the instrument pointer 5 points to the zero scale of the 360-degree instrument panel 4, and when the driving motor 3 drives the radar front 1 to rotate according to a set angle, the rotation of the radar front 1 also drives the 360-degree instrument panel 4 to rotate through the radar adapter 6, the gauge pointer 5 may then point to the corresponding angle marked on the 360 degrees dashboard 4.
Fig. 6 is an elevation angle adjustment effect diagram shown in fig. 1, and driving motor 3 drives radar array 1 to rotate according to a set angle through a cylindrical rod screwed in radar array adapter 6, and the rotation of radar array 1 also drives 360-degree instrument panel 4 to rotate through radar array adapter 6 for confirming and calibrating the set pitch angle, and simultaneously, antenna support rod 7 also drives test antenna 10 to rotate by a corresponding angle.
In addition, be fixed in laser pen light calibrating device on radar array face 1 and also can rotate the same angle along with radar array face 1, and then drive laser pen 9 and rotate the same angle, laser pen 9 is beaten the light beam through two laser beam locating holes of laser calibrating device 8, shines the target of being surveyed, assists the test operation of test antenna 10.
The above-mentioned embodiments, further detailed description of the objects, technical solutions and advantages of the present invention, it should be understood that the above-mentioned embodiments are only specific embodiments of the present invention, and are not intended to limit the present invention, and any modifications, equivalent substitutions, improvements, etc. made within the spirit and principle of the present invention should be included in the scope of the present invention.
Claims (7)
1. A radar test structure with an automatic pitch function, comprising:
a radar array plane (1);
and the driving motor (3) is arranged on one side of the radar array surface (1), is mechanically connected with the radar array surface (1) and is used for driving the radar array surface (1) to rotate so as to form a set pitch angle with the horizontal plane.
2. The structure of claim 1, further comprising a radar test support (2) for supporting the radar front (1) and the driving motor (3) to fix the radar front (1) and the driving motor (3) on a horizontal plane, wherein the radar test support (2) comprises a left side plate, a right side plate and a bottom plate, wherein the left side plate and the right side plate are respectively disposed at two ends of the bottom plate, and the top ends of the left side plate and the right side plate are respectively provided with a groove.
3. The structure according to claim 2, characterized in that the drive motor (3) is further provided with a cylindrical rod, the end of which is mechanically connected with the radar front (1) through a radar front adapter (6), and the cylindrical rod is embedded in a groove at the top end of the left side plate of the radar test bracket (2) for fixing the radar front (1) on the radar test bracket (2).
4. The structure according to claim 2, characterized in that it further comprises a 360-degree dashboard (4), one of said 360-degree dashboard (4) being mechanically connected to said radar front (1) by means of a radar front adapter (6), the other being provided with a cylindrical rod, the body of said cylindrical rod being engaged in a recess in the right side plate of said radar test mount (2) for fixing said radar front (1) to said radar test mount (2).
5. The structure according to claim 4, characterized by further comprising a meter pointer (5) horizontally arranged at the top end of the right side plate of the radar test support (2) and used for indicating the pitch angle of the rotation of the radar front surface (1) together with the 360-degree instrument panel (4).
6. The structure of claim 1, further comprising:
the antenna support rod (7) is arranged at the top end of the radar array surface (1), and the antenna support rod (7) and the radar array surface (1) are positioned on the same plane;
and the two test antennas (10) are respectively arranged at two ends of the antenna supporting rod (7).
7. The structure of claim 1, further comprising:
the laser pen light calibration device (8) is arranged at the top end of the radar array surface (1), and the laser pen light calibration device (8) comprises two laser beam positioning holes;
a laser pen (9) arranged on the laser pen light calibration device (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921314409.5U CN210864031U (en) | 2019-08-13 | 2019-08-13 | Radar test structure with automatic every single move function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921314409.5U CN210864031U (en) | 2019-08-13 | 2019-08-13 | Radar test structure with automatic every single move function |
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| Publication Number | Publication Date |
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| CN210864031U true CN210864031U (en) | 2020-06-26 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201921314409.5U Active CN210864031U (en) | 2019-08-13 | 2019-08-13 | Radar test structure with automatic every single move function |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110346770A (en) * | 2019-08-13 | 2019-10-18 | 中国科学院电子学研究所 | A kind of radar test structure with automatic pitching function |
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2019
- 2019-08-13 CN CN201921314409.5U patent/CN210864031U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110346770A (en) * | 2019-08-13 | 2019-10-18 | 中国科学院电子学研究所 | A kind of radar test structure with automatic pitching function |
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