Multifunctional satellite communication equipment

Abstract

The utility model discloses a multifunctional satellite communication device, which comprises a satellite communication main body, a fixing seat and a plurality of supporting columns, one end of each supporting column is expanded outwards to form an insertion part with a conical structure, the supporting columns are sleeved with impact sleeves, the fixing seat is arranged in the supporting columns, and the fixing seat is arranged in the supporting columns. A connecting groove is formed in one end face of the fixing base, a plurality of connecting blocks are slidably installed in the connecting groove, supporting arms are installed on the connecting blocks, sleeves are installed at the ends, away from the connecting blocks, of the supporting arms, and the supporting columns are sleeved with the sleeves. According to the utility model, the structure is simple, the satellite communication main body can be installed among the plurality of supporting columns through the sleeves, so that the satellite communication main body can move up and down along the supporting columns so as to change the installation height, and the plurality of external supporting columns can play a role in intercepting and protecting the internal satellite communication main body; and the situation that an external worker collides with the satellite communication main body is reduced.

Description

Technical Field

[0001] This utility model relates to the field of communication technology, specifically to a multifunctional satellite communication device. Background Technology

[0002] Satellite communication equipment, especially equipment mounted on communication satellites, is a key component for realizing satellite communication.

[0003] When existing satellite communication equipment is used outdoors, it is mounted on a bracket. However, most of these brackets are placed directly on the ground, making it impossible to adjust the height of the satellite communication equipment and providing insufficient protection. This means that staff may accidentally touch the equipment while it is in use on the ground, which could easily change the angle of the satellite communication equipment and affect the communication quality. Utility Model Content

[0004] The technical problem to be solved by this utility model is to provide a multifunctional satellite communication device that can adjust its height and form a protective fence around the satellite communication device through external support columns, so as to solve the problems mentioned in the background art.

[0005] This utility model is achieved through the following technical solution: a multifunctional satellite communication device, including a satellite communication main body, a fixed base, and multiple support columns. One end of each support column expands outward to form a conical insertion part. Each support column is fitted with an impact sleeve. The multiple support columns are distributed in a ring structure. The fixed base is located inside the multiple support columns. One end face of the fixed base is provided with a connecting groove. Multiple connecting blocks are slidably installed in the connecting groove. Each connecting block is equipped with a support arm. The end of each support arm away from the connecting block is equipped with a sleeve, which is fitted onto the support column. A hydraulic damping gimbal is installed at the other end of the fixed base. The other end of the hydraulic damping gimbal is fixedly connected to the satellite communication main body.

[0006] As a preferred technical solution, the outer ring surface of the sleeve is provided with screw holes, and each screw hole is threaded with a hand-tightening bolt. One end of each hand-tightening bolt is set to abut against the support column, and the inner diameter of the sleeve matches the diameter of the support column.

[0007] As a preferred technical solution, positioning grooves are provided on both the inner and outer ring surfaces of the connecting groove, and positioning parts are formed by protrusions on both sides of the connecting block. The positioning parts are slidably disposed in the positioning grooves, and a rubber layer is installed on the inner wall surface of the connecting groove. The rubber layer is in frictional contact with the connecting block.

[0008] As a preferred technical solution, the outer ring surface of the impact sleeve is recessed to form a handheld groove with an annular structure.

[0009] As a preferred technical solution, the end of the support arm furthest from the sleeve is bent upwards.

[0010] As a preferred technical solution, one end of the impact sleeve is arranged to abut against the end face of the insertion part.

[0011] The beneficial effects of this utility model are: the utility model has a simple structure, and the impact sleeve can more efficiently insert the support column into the soil and adapt to uneven ground. The satellite communication body can be installed between multiple support columns through the sleeve, so that the satellite communication body can move up and down along the support columns to change its installation height. In addition, the multiple external support columns can intercept and protect the internal satellite communication body, reducing the possibility of external personnel hitting the satellite communication body. Attached Figure Description

[0012] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0013] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0014] Figure 2 This is a bottom view of the present invention;

[0015] Figure 3 This is a top view of the present invention.

[0016] The components include: 1. Satellite communication main body; 2. Support column; 3. Insertion part; 4. Impact sleeve; 5. Hand-held groove; 6. Sleeve; 7. Hand-tightening bolt; 8. Support arm; 9. Fixing seat; 10. Connecting groove; 11. Connecting block. Detailed Implementation

[0017] The embodiments of this utility model are described in detail below. Examples of these embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain this utility model, and should not be construed as limiting this utility model.

[0018] All features disclosed in this specification, or all steps in all disclosed methods or processes, may be combined in any way, except for mutually exclusive features and / or steps.

[0019] Any feature disclosed in this specification (including any appended claims, abstract, and drawings) may be replaced by other equivalent or similar features for a similar purpose, unless specifically stated otherwise. That is, unless specifically stated otherwise, each feature is merely one example of a series of equivalent or similar features.

[0020] like Figure 1 , Figure 2 and Figure 3 As shown, this utility model discloses a multifunctional satellite communication device, comprising a satellite communication main body 1, a fixed base 9, and multiple support columns 2. One end of each support column 2 expands outward to form a conical insertion portion 3. Each support column 2 is fitted with an impact sleeve 4. The multiple support columns 2 are arranged in a ring structure. The fixed base 9 is disposed inside the multiple support columns 2. One end face of the fixed base 9 has a connecting groove 10, in which multiple connecting blocks 11 are slidably installed. Each connecting block 11 is fitted with a support arm 8. The end of each support arm 8 away from the connecting block 11 is fitted with a sleeve 6, which is fitted onto the support column 2. A hydraulic damping gimbal is installed at the other end of the fixed base 9, and the other end of the hydraulic damping gimbal is fixedly connected to the satellite communication main body 1. The angle of the satellite communication main body can be adjusted by the hydraulic damping gimbal, thereby improving signal reception.

[0021] In this embodiment, screw holes are provided on the outer ring surface of the sleeve 6, and hand-tightening bolts 7 are threaded into the screw holes. One end of the hand-tightening bolts 7 is set to abut against the support column 2, and the inner diameter of the sleeve 6 matches the diameter of the support column 2.

[0022] In this embodiment, positioning grooves are provided on both the inner and outer ring surfaces of the connecting groove 10. Positioning parts are formed by protrusions on both sides of the connecting block 11. The positioning parts are slidably disposed in the positioning grooves. A rubber layer is installed on the inner wall surface of the connecting groove 10. The rubber layer is in frictional contact with the connecting block 11, thereby enabling the rotating support arm to be positioned by friction.

[0023] In this embodiment, the outer ring surface of the impact sleeve 4 is recessed to form a ring-shaped handheld groove 5.

[0024] In this embodiment, the end of the support arm 8 away from the sleeve 6 is bent upwards, which can lift the fixing base and the satellite communication body upwards, thereby increasing the distance between the satellite communication equipment and the support arm and increasing the adjustment angle of the satellite communication body.

[0025] In this embodiment, one end of the impact sleeve 4 is arranged to abut against the end face of the insertion part 3, so that the impact sleeve can impact the insertion part downward and press the insertion part into the soil.

[0026] When using, first insert the support column independently into the soil. During the insertion process, hold it in the hand slot of the impact sleeve, lift the impact sleeve upward, and quickly push the impact sleeve downward so that the impact sleeve can impact the insertion part, so that the insertion part can be efficiently inserted into the soil, increasing the installation efficiency.

[0027] After the support column is installed, the support arm can rotate along the connecting groove until the sleeve is positioned opposite the support column, so that the sleeve can be smoothly fitted onto the outside of the support column and can move up and down along the support column to change the installation height of the satellite communication body. The adjustment method can prevent the satellite communication body from contacting or covering the plants on the ground, and the moved sleeve can be positioned on the support column by hand-tightening the bolts.

[0028] The satellite communication unit is equipped with multiple support pillars on its exterior, which form a protective fence to reduce the chance of external personnel bumping into the satellite communication unit.

[0029] The above description is merely a specific embodiment of this utility model, but the protection scope of this utility model is not limited thereto. Any changes or substitutions conceived without inventive effort should be included within the protection scope of this utility model. Therefore, the protection scope of this utility model should be determined by the scope defined in the claims.

Claims

1. A multi-functional satellite communication device, characterized in that: The system includes a satellite communication main body (1), a fixed base (9), and multiple support columns (2). One end of each support column (2) is expanded outward to form a conical insertion part (3). Each support column (2) is fitted with an impact sleeve (4). The multiple support columns (2) are arranged in a ring structure. The fixed base (9) is located inside the multiple support columns (2). One end face of the fixed base (9) is provided with a connecting groove (10). Multiple connecting blocks (11) are slidably installed in the connecting groove (10). Each connecting block (11) is equipped with a support arm (8). Each end of the support arm (8) away from the connecting block (11) is equipped with a sleeve (6). Each sleeve (6) is fitted onto the support column (2). The other end of the fixed base (9) is equipped with a hydraulic damping gimbal. The other end of the hydraulic damping gimbal is fixedly connected to the satellite communication main body (1).

2. The multi-functional satellite communication equipment according to claim 1, characterized in that: Screw holes are provided on the outer ring surface of the sleeve (6), and hand-tightening bolts (7) are threaded into the screw holes. One end of the hand-tightening bolts (7) is set to abut against the support column (2). The inner diameter of the sleeve (6) matches the diameter of the support column (2).

3. The multi-functional satellite communication equipment according to claim 1, characterized in that: The inner and outer ring surfaces of the connecting groove (10) are provided with positioning grooves. Both sides of the connecting block (11) protrude to form positioning parts. The positioning parts are slidably disposed in the positioning grooves. A rubber layer is installed on the inner wall surface of the connecting groove (10). The rubber layer is in frictional contact with the connecting block (11).

4. The multi-functional satellite communication equipment according to claim 1, characterized in that: The outer ring surface of the impact sleeve (4) is recessed to form a ring-shaped handheld groove (5).

5. The multi-functional satellite communication equipment according to claim 1, characterized in that: The end of the support arm (8) away from the sleeve (6) is bent upward.

6. The multi-functional satellite communication equipment according to claim 1, characterized in that: One end of the impact sleeve (4) is set to abut against the end face of the insertion part (3).

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