Radar array plane skeleton

Abstract

The utility model discloses a radar array plane skeleton, which relates to the technical field of skeleton structures and comprises a plurality of frames, a plurality of bolt assemblies and a plurality of mounting assemblies. The plurality of mounting assemblies are respectively arranged on the plurality of frames, the plurality of mounting assemblies are sequentially connected from top to bottom, and any two adjacent mounting assemblies are detachably connected through a bolt assembly. And one mounting assembly and one frame jointly form a skeleton unit. When the radar array plane framework needs to be transported, an operator can unscrew the plurality of bolt assemblies, so that the plurality of framework units are separated from one another, the operator can separately convey the plurality of framework units, and the radar array plane framework is more convenient to transport and carry. When the radar array plane framework needs to be assembled, due to the fact that the framework units are detachably connected, the radar array plane framework can adapt to different installation sites and requirements more easily, and the installation flexibility of the radar array plane framework is improved.

Description

Technical Field

[0001] This utility model relates to the field of skeleton structure technology, and in particular to a radar array skeleton. Background Technology

[0002] A radar array frame is a structural framework used to support a radar array. Its main function is to provide support for various electronic components, such as antenna assemblies, ensuring these components are in the correct position and relative relationships. This guarantees the shape and structural stability of the radar array, thereby ensuring the normal operation of the radar system. In existing technologies, radar array frames are large and heavy structural frameworks, which makes them susceptible to space and weight limitations during transportation, thus hindering the ease of transport and installation. Utility Model Content

[0003] This invention aims to solve at least one of the technical problems existing in the prior art. To this end, this invention proposes a radar array frame that improves the ease of transportation and installation of the radar array frame.

[0004] According to an embodiment of the present invention, a radar array frame includes multiple frames, multiple bolt assemblies, and multiple mounting assemblies. The multiple mounting assemblies are respectively disposed on the multiple frames, and are connected sequentially from top to bottom. Any two adjacent mounting assemblies are detachably connected via the bolt assemblies.

[0005] It has at least the following beneficial effects:

[0006] Multiple mounting components are mounted on multiple frames, forming multiple skeleton units. Each mounting component and frame together constitutes a skeleton unit. The mounting components are connected sequentially from top to bottom, resulting in a top-to-bottom distribution of the frames and skeleton units. Any two adjacent mounting components are detachably connected via bolts, allowing for a detachable connection between two frames and skeleton units. When transporting the radar array skeleton, operators can loosen the bolts to separate the mounting components and skeleton units, enabling separate transport of each unit. This reduces the overall volume and weight of the radar array skeleton, making transportation and handling more convenient, especially in situations with limited space and weight. To assemble the radar array skeleton, operators arrange the skeleton units sequentially and then connect the mounting components of adjacent units using bolts, completing the assembly. Because multiple skeleton units can be detachably connected, this radar array skeleton can be more easily adapted to different installation sites and requirements, thus improving the installation flexibility of the radar array skeleton.

[0007] According to the radar array frame of this utility model embodiment, the mounting assembly includes multiple mounting seats, all of which are disposed on the frame. The multiple mounting seats on any two adjacent frames are respectively disposed correspondingly, and two adjacent mounting seats in the vertical direction are connected by the bolt assembly.

[0008] According to an embodiment of the present invention, the radar array frame includes three first mounting plates, three second mounting plates, two first connecting arms, two second connecting arms, and two connecting vertical rods. The three first mounting plates are arranged in a triangular pattern. One end of each of the two first connecting arms is connected to one of the first mounting plates, and the other end of each of the two first connecting arms is connected to the other two first mounting plates. The openings of the two first connecting arms forming an included angle face forward. Similarly, the three second mounting plates are arranged in a triangular pattern. One end of each of the two second connecting arms is connected to one of the second mounting plates, and the other end of each of the two second connecting arms is connected to the other two first mounting plates. Two second mounting plates are connected, and the openings of the two second connecting arms form an angle facing forward. The upper ends of the two connecting vertical rods are respectively connected to the other two first mounting plates, and the lower ends of the two connecting vertical rods are respectively connected to the other two second mounting plates. The front sides of the two connecting vertical rods are used for antenna assembly installation. All three first mounting plates are connected to the upper end of the frame, and all three second mounting plates are connected to the lower end of the frame. The three first mounting plates are respectively arranged correspondingly to the three second mounting plates so that the first mounting plates and second mounting plates on adjacent frames can be connected by the bolt assembly.

[0009] According to the radar array skeleton of this utility model embodiment, the first mounting plate has a plurality of first mounting holes, and the second mounting plate has a plurality of second mounting holes, all of which are used for the bolt assembly to pass through.

[0010] According to the radar array frame of this utility model embodiment, the mounting assembly further includes multiple connecting crossbars, each of which is simultaneously connected to multiple mounting bases, and the front sides of each of the multiple connecting crossbars are used for mounting antenna components.

[0011] According to the radar array frame of this utility model embodiment, each of the multiple frames is provided with a first auxiliary mounting bracket on both the left and right sides, and the multiple first auxiliary mounting brackets are used to connect to the support structure on the ground.

[0012] According to an embodiment of the present invention, the radar array frame further includes a second auxiliary mounting bracket, which is disposed on the rear side of one of the frames and is used to connect with a support structure on the ground.

[0013] According to an embodiment of the present invention, the radar array frame includes multiple quadrangular pyramidal grid frames.

[0014] Additional aspects and advantages of this invention will be set forth in part in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention. Attached Figure Description

[0015] The present invention will be further described below with reference to the accompanying drawings and embodiments, wherein:

[0016] Figure 1 This is a schematic diagram of the radar array frame structure according to an embodiment of the present invention;

[0017] Figure 2 for Figure 1 A magnified view of a section at point A in the middle;

[0018] Figure 3 This is a schematic diagram of the disassembled radar array frame according to an embodiment of the present invention;

[0019] Figure 4 This is a schematic diagram of the structure of one of the frames and mounting components in the radar array skeleton of this utility model embodiment;

[0020] Figure 5 This is a structural schematic diagram of one of the frames and mounting components in the radar array skeleton of this utility model embodiment from another perspective;

[0021] Figure 6 This is a schematic diagram of the structure of the mounting components in the radar array frame according to an embodiment of the present invention;

[0022] Figure 7 This is a schematic diagram of the mounting base in the radar array frame of this utility model embodiment;

[0023] Figure 8 This is a schematic diagram of the structure of the radar array frame tilted according to an embodiment of the present invention;

[0024] Icon labels:

[0025] Frame 100; First auxiliary mounting bracket 110; Second auxiliary mounting bracket 120;

[0026] Mounting component 200; mounting base 210; first mounting plate 211; second mounting plate 212; first connecting arm 213; second connecting arm 214; connecting vertical rod 215; connecting horizontal rod 220. Detailed Implementation

[0027] In the description of this utility model, it should be understood that the directional descriptions, such as up, down, front, back, left, right, etc., indicate the directional or positional relationship based on the directional or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.

[0028] In the description of this utility model, the use of "first" and "second" is only for the purpose of distinguishing technical features and should not be construed as indicating or implying relative importance or implicitly indicating the number of technical features or the order of the technical features.

[0029] In the description of this utility model, unless otherwise explicitly defined, terms such as "setting," "installation," and "connection" should be interpreted broadly, and those skilled in the art can reasonably determine the specific meaning of the above terms in this utility model in conjunction with the specific content of the technical solution.

[0030] refer to Figure 1 , Figure 3 and Figure 6 This utility model discloses a radar array frame, including multiple frames 100, multiple bolt assemblies and multiple mounting assemblies 200.

[0031] Multiple mounting components 200 are respectively mounted on multiple frames 100. The multiple mounting components 200 are connected sequentially from top to bottom. Any two adjacent mounting components 200 are detachably connected by bolt assemblies.

[0032] It is understood that multiple mounting components 200 are respectively mounted on multiple frames 100, so that the multiple frames 100 and multiple mounting components 200 respectively form multiple skeleton units, that is, one mounting component 200 and one frame 100 together form a skeleton unit. The multiple mounting components 200 are connected sequentially from top to bottom, so that the multiple frames 100 are distributed from top to bottom, thus resulting in multiple skeleton units distributed from top to bottom. Furthermore, any two adjacent mounting components 200 are detachably connected by bolt assemblies, so that two frames 100 can be detachably connected via the mounting components 200, thus resulting in a detachable connection between two skeleton units. When the radar array skeleton needs to be transported, the operator can loosen the multiple bolt assemblies, so that the multiple mounting components 200 are separated from each other, thus separating the multiple skeleton units from each other. This allows the operator to transport multiple skeleton units separately, reducing the overall volume and weight of the radar array skeleton during transport. This makes the radar array skeleton more convenient during transportation and handling, especially in situations where transportation space and weight are limited. When assembling the radar array frame, operators can arrange multiple frame units sequentially, and then connect the mounting components 200 of adjacent frame units together using bolt assemblies to complete the assembly of the radar array frame. Because multiple frame units can be detachably connected, this makes the radar array frame more adaptable to different installation sites and requirements, improving the flexibility of its installation.

[0033] refer to Figures 4 to 7The mounting assembly 200 includes multiple mounting seats 210, all of which are disposed on the frame 100. The mounting seats 210 on any two adjacent frames 100 are respectively disposed correspondingly, and adjacent mounting seats 210 in the vertical direction are connected by bolt assemblies. It can be understood that the mounting assembly 200 includes multiple mounting seats 210, all of which are disposed on the frame 100, meaning that multiple mounting seats 210 are evenly distributed along the left-right direction on each of the multiple frames 100. In this embodiment of the present invention, there are a total of four frames 100 and four mounting assemblies 200, that is, a total of four skeleton units. For ease of explanation, the four frames 100 are defined from top to bottom as the first frame 100, the second frame 100, the third frame 100, and the fourth frame 100. Understandably, when assembling the radar array frame, the operator can first install the lowermost fourth frame 100 onto the support structure on the ground using its multiple mounting seats 210. Then, the operator can move the third frame 100 and its multiple mounting seats 210 together onto the fourth frame 100, so that the multiple mounting seats 210 on the third frame 100 correspond one-to-one with the multiple mounting seats 210 on the fourth frame 100. Then, the corresponding two mounting seats 210 on the fourth frame 100 and the third frame 100 are connected together using bolt assemblies, thus completing the installation of the fourth frame 100 and the third frame 100.

[0034] After the third frame 100 is installed, the operator can move the second frame 100 and its multiple mounting seats 210 onto the third frame 100, so that the mounting seats 210 on the second frame 100 correspond one-to-one with the mounting seats 210 on the third frame 100. Then, the corresponding mounting seats 210 on the third frame 100 and the second frame 100 are connected together using bolt assemblies, thus completing the installation of the third frame 100 and the second frame 100. After the second frame 100 is installed, the operator can move the first frame 100 and its multiple mounting seats 210 onto the second frame 100, so that the mounting seats 210 on the first frame 100 correspond one-to-one with the mounting seats 210 on the second frame 100. Then, the corresponding mounting seats 210 on the first frame 100 and the second frame 100 are connected together using bolt assemblies, thus completing the installation of the first frame 100 and the second frame 100, and thus completing the assembly of the radar array skeleton. In this embodiment of the invention, the radar array frame may also include a greater number of frames 100 and mounting components 200, which will not be described further here.

[0035] refer to Figures 2 to 7The mounting base 210 includes three first mounting plates 211, three second mounting plates 212, two first connecting arms 213, two second connecting arms 214, and two connecting vertical rods 215. The three first mounting plates 211 are arranged in a triangle. One end of each of the two first connecting arms 213 is connected to one of the first mounting plates 211, and the other end of each of the two first connecting arms 213 is connected to the other two first mounting plates 211 respectively. The openings of the two first connecting arms 213 at an included angle face forward. The three second mounting plates 212 are also arranged in a triangle. One end of each of the two second connecting arms 214 is connected to one of the second mounting plates 212, and the other end of each of the two second connecting arms 214 is connected to the other two first mounting plates 212 respectively. Two mounting plates 212 are connected, and the openings of the two second connecting arms 214 form an angle facing forward. The upper ends of the two connecting vertical rods 215 are respectively connected to the other two first mounting plates 211, and the lower ends of the two connecting vertical rods 215 are respectively connected to the other two second mounting plates 212. The front sides of the two connecting vertical rods 215 are used for antenna assembly installation. The three first mounting plates 211 are all connected to the upper end of the frame 100, and the three second mounting plates 212 are all connected to the lower end of the frame 100. The three first mounting plates 211 are respectively set to correspond to the three second mounting plates 212 so that the first mounting plates 211 and the second mounting plates 212 on two adjacent frames 100 can be connected by bolt assemblies.

[0036] In this embodiment of the invention, the bolt assembly includes multiple fastening bolts and multiple nuts, wherein the fastening bolts are threadedly connected to the nuts. A first mounting plate 211 has multiple first mounting holes, and a second mounting plate 212 has multiple second mounting holes; both the first and second mounting holes are for the bolt assembly to pass through.

[0037] Understandably, reference Figure 1 and Figure 2The frame 100 is provided with multiple mounting seats 210, and each mounting seat 210 includes three first mounting plates 211 and three second mounting plates 212, so that the upper end of the frame 100 is connected to multiple first mounting plates 211 and the lower end of the frame 100 is connected to multiple second mounting plates 212. When assembling the radar array skeleton, the operator can first install the lowermost fourth frame 100 onto the support structure on the ground through the multiple second mounting plates 212 on its lower end. Then, the operator can move the third frame 100 onto the fourth frame 100, so that the multiple second mounting plates 212 on the lower end of the third frame 100 are respectively aligned with the multiple first mounting plates 211 on the upper end of the fourth frame 100, so that the multiple second mounting holes on the second mounting plates 212 can be aligned with the multiple first mounting holes on the first mounting plates 211. The operator then passes the fastening bolts through the second and first mounting holes and tightens the nuts on the fastening bolts, thus securing the second mounting plate 212 and the first mounting plate 211 together. Repeating the steps of placing the fastening bolts and tightening the nuts secures the multiple second mounting plates 212 on the lower end of the third frame 100 to the multiple first mounting plates 211 on the upper end of the fourth frame 100, completing the installation of the third and fourth frames 100. The installation process for the second and first frames 100 is similar and will not be described further here. In this embodiment of the invention, the mounting assembly 200 includes three mounting bases 210.

[0038] In this embodiment of the invention, since the three first mounting plates 211 and the three second mounting plates 212 are all triangularly distributed, the structural stability of the mounting base 210 can be effectively improved, preventing the mounting base 210 from shaking during use. In this embodiment of the invention, after the radar array frame is assembled, the operator needs to install the antenna assembly on the radar array frame. Specifically, the operator can install the antenna assembly on the front side of the connecting vertical rod 215, that is, the front side of the connecting vertical rod 215 is the mounting surface for installing the antenna assembly. As one embodiment of the invention, the upper end of the connecting vertical rod 215 is welded to the first mounting plate 211, and the lower end of the connecting vertical rod 215 is welded to the second mounting plate 212. (Reference) Figures 4 to 6The mounting assembly 200 also includes multiple connecting crossbars 220, each of which is simultaneously connected to multiple mounting bases 210. The front surfaces of the connecting crossbars 220 are all used for mounting the antenna assembly. It is understood that the multiple mounting bases 210 are connected by the multiple connecting crossbars 220, and the front surfaces of the connecting crossbars 220 also serve as mounting surfaces for the antenna assembly. In other words, the front surfaces of the multiple connecting crossbars 220 and the multiple connecting vertical bars 215 together form the front surface of the radar array frame, allowing operators to mount the antenna assembly on the front surface of the radar array frame. As one embodiment of this invention, the connecting crossbars 220 are welded to the connecting vertical bars 215.

[0039] refer to Figure 5 Each of the multiple frames 100 has a first auxiliary mounting bracket 110 on both its left and right sides, and all of the first auxiliary mounting brackets 110 are used to connect to the support structure on the ground. The radar array frame also includes a second auxiliary mounting bracket 120, which is located on the rear side of one of the frames 100 and is used to connect to the support structure on the ground. It should be noted that, according to... Figure 8 In this embodiment of the invention, the radar array frame is mounted on a support structure on the ground. The support structure not only supports and fixes the radar array frame, ensuring its stable connection to the ground, but also adjusts its attitude, allowing it to be tilted. Multiple frames 100 have first auxiliary mounting brackets 110 on both sides. These brackets connect to the support structure on the ground, enabling the frames 100 to be mounted on the support structure, ensuring a stable connection between the radar array frame and the ground. In this embodiment, a second auxiliary mounting bracket 120 is located on the rear side of one of the frames 100 in the middle position and connects to the support structure on the ground, allowing the radar array frame to be stably connected to the ground in an tilted posture.

[0040] refer to Figure 1 , Figure 4 and Figure 5The frame 100 includes multiple quadrangular pyramidal space frames. In this embodiment of the invention, the quadrangular pyramidal space frame is a common space frame structure, including an upper chord, a lower chord, web members, and multiple bolted ball joints, which will not be further elaborated here. In this embodiment of the invention, the first mounting plate 211 and the second mounting plate 212 are both connected to the corresponding bolted ball joints. It can be understood that the radar array frame is composed of multiple frames 100, and each of the multiple frames 100 is composed of multiple quadrangular pyramidal space frames. The quadrangular pyramidal space frame is a spatial load-bearing structure, which enables the radar array frame to have better load-bearing capacity and deformation resistance, and can effectively resist the effects of natural forces such as wind and earthquakes. As an embodiment of the invention, the quadrangular pyramidal space frame is made of aluminum alloy material. Aluminum alloy quadrangular pyramidal space frames have stronger corrosion resistance, enabling the radar array frame to be erected in harsh environments such as the field. On the other hand, the aluminum alloy quadrangular pyramidal grid frame not only ensures the strength of the radar array frame, but also significantly reduces the overall weight of the radar array frame, further improving the ease of transportation of the radar array frame.

[0041] The technical features of the above embodiments can be combined in any way. For the sake of brevity, not all possible combinations of the technical features in the above embodiments are described. However, as long as there is no contradiction in the combination of these technical features, they should be considered to be within the scope of this specification.

[0042] Of course, this utility model is not limited to the above-described embodiments. Those skilled in the art can make equivalent modifications or substitutions without departing from the spirit of this utility model. All such equivalent modifications or substitutions are included within the scope defined by the claims of this application.

Claims

1. A radar array frame, characterized in that, include: Multiple frames (100); Multiple bolt assemblies; Multiple mounting components (200) are respectively disposed on multiple frames (100), and the multiple mounting components (200) are connected sequentially from top to bottom. Any two adjacent mounting components (200) are detachably connected by bolts.

2. The radar array frame according to claim 1, characterized in that: The mounting assembly (200) includes a plurality of mounting seats (210), all of which are disposed on the frame (100). The plurality of mounting seats (210) on any two adjacent frames (100) are respectively disposed, and the two adjacent mounting seats (210) in the vertical direction are connected by the bolt assembly.

3. The radar array frame according to claim 2, characterized in that: The mounting base (210) includes three first mounting plates (211), three second mounting plates (212), two first connecting arms (213), two second connecting arms (214), and two connecting vertical rods (215). The three first mounting plates (211) are arranged in a triangle. One end of each of the two first connecting arms (213) is connected to one of the first mounting plates (211), and the other end of each of the two first connecting arms (213) is connected to the other two first mounting plates (211). The openings of the two first connecting arms (213) at an included angle face forward. The three second mounting plates (212) are arranged in a triangle. One end of each of the two second connecting arms (214) is connected to one of the second mounting plates (212), and the other end of each of the two second connecting arms (214) is connected to the other two second mounting plates (212). (212) Connection, the openings of the two second connecting arms (214) forming an angle face forward, the upper ends of the two connecting vertical rods (215) are respectively connected to the other two first mounting plates (211), the lower ends of the two connecting vertical rods (215) are respectively connected to the other two second mounting plates (212), the front sides of the two connecting vertical rods (215) are used for antenna assembly installation, the three first mounting plates (211) are all connected to the upper end of the frame (100), the three second mounting plates (212) are all connected to the lower end of the frame (100), the three first mounting plates (211) are respectively corresponding to the three second mounting plates (212) so that the first mounting plates (211) and the second mounting plates (212) on the two adjacent frames (100) can be connected by the bolt assembly.

4. The radar array frame according to claim 3, characterized in that: The first mounting plate (211) has a plurality of first mounting holes, and the second mounting plate (212) has a plurality of second mounting holes. Both the plurality of first mounting holes and the plurality of second mounting holes are used for the bolt assembly to pass through.

5. The radar array frame according to claim 2, characterized in that: The mounting assembly (200) also includes multiple connecting crossbars (220), each of which is simultaneously connected to multiple mounting bases (210), and the front sides of each of the multiple connecting crossbars (220) are used for mounting the antenna assembly.

6. The radar array frame according to claim 1, characterized in that: Each of the multiple frames (100) is provided with a first auxiliary mounting bracket (110) on both the left and right sides, and the multiple first auxiliary mounting brackets (110) are used to connect to the support structure on the ground.

7. The radar array frame according to claim 1, characterized in that: It also includes a second auxiliary mounting bracket (120), which is located on the rear side of one of the frames (100) and is used to connect to a support structure on the ground.

8. The radar array frame according to claim 1, characterized in that: The frame (100) includes multiple quadrangular pyramidal space frames.

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