Satellite terminal adjusting support

By designing a satellite terminal adjustment bracket with a driving structure, using an asynchronous motor to drive the rack and threaded rod, multi-angle adjustment of the terminal orientation is achieved, solving the problem that the terminal is difficult to adjust in harsh environments in the prior art, and improving signal stability Sex and installation flexibility.

CN222351955UActive Publication Date: 2025-01-14HEILONGJIANG TIANXING TONGLIAN TECH CO LTD
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Patent Information

Application Number
CN202421310867.2
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-06-11
Publication Date
2025-01-14
Estimated Expiration
2034-06-11

AI Technical Summary

Technical Problem

The existing satellite terminals are difficult to adjust their orientation in harsh environments, resulting in unstable signal reception and transmission, and are inconvenient to adjust after installation.

Method used

A satellite terminal adjustment bracket including an adjustment bracket, a mounting frame, and a driving structure is designed. The rack and threaded rod are driven by an asynchronous motor to realize the rotation of the connecting ring and the support plate, allowing the orientation of the satellite terminal to be adjusted from multiple angles.

Benefits of technology

It improves the signal reception and transmission stability of satellite terminals in harsh environments, enhances the flexibility of installation and use, and facilitates adjustment and adjustment of terminal orientation.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to a satellite terminal adjusting support, which belongs to the technical field of satellite terminal adjusting supports and comprises an adjusting support, a mounting frame is arranged on the adjusting support, a satellite terminal is arranged on the mounting frame, and an adjusting structure and a driving structure are arranged on the adjusting support. According to the satellite terminal adjusting support, by arranging the adjusting structure and the driving structure, an asynchronous motor in the driving assembly is used as a driving source, and the connecting ring is controlled to rotate through mechanical transmission, so that the connecting ring drives a satellite terminal on the top of the mounting table to turn over through the supporting plate, and a locking bolt in the mounting table can be rotated; the fixed connection between the mounting table and the steering part is removed, so that a worker can conveniently rotate the mounting table to move the satellite terminal, the orientation of the satellite terminal can be adjusted after the satellite terminal adjusting support is flexibly installed, and then the satellite terminal can be conveniently installed and used.
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Description

Technical Field

[0001] The utility model relates to the technical field of satellite terminal adjustment brackets, in particular to a satellite terminal adjustment bracket. Background Art

[0002] In the mobile satellite communication system, the user segment needs to access the mobile satellite communication network through the ground segment for mobile communication. The communication terminal representing the user segment can have different forms, such as handheld terminals or vehicle-mounted terminals. The function of the user terminal is to enable the terminal user to set and obtain the communication status and complete the communication by installing a wireless transceiver antenna. For mobile satellite communication networks with different frequency bands, one of the manifestations is that the user terminals use different frequencies. User terminals that communicate using different frequency bands have different communication functions and design methods.

[0003] In the current existing technology, the satellite terminal needs to be installed on a mounting bracket, and the mounting bracket is installed on the ground through piles and embedded parts. In harsh environments, it is necessary to adjust the orientation of the satellite terminal to improve the stability of signal reception and transmission. However, the existing satellite terminal can only be pre-adjusted in terms of orientation and then installed in a designated position, which makes it inconvenient to adjust the orientation of the satellite terminal after installation. Therefore, a satellite terminal adjustment bracket is proposed to solve the above problem. Utility Model Content

[0004] In view of the shortcomings of the prior art, the utility model provides a satellite terminal adjustment bracket, which has the advantage of flexible installation and solves the problem of needing to adjust the orientation of the satellite terminal in harsh environments, thereby improving the stability of signal reception and transmission. However, the prior art can only pre-debug the orientation of the satellite terminal and then install it at a specified position, which makes it inconvenient to adjust the orientation of the satellite terminal after installation.

[0005] To achieve the above object, the utility model provides the following technical solutions: a satellite terminal adjustment bracket, comprising an adjustment bracket, a mounting frame is arranged on the adjustment bracket, a satellite terminal is arranged on the mounting frame, and an adjustment structure and a driving structure are arranged on the adjustment bracket;

[0006] The adjustment structure includes a connecting column rotatably installed between the front and rear side walls of the inner cavity of the adjustment bracket, a connecting ring is fixedly installed on the outer surface of the connecting column, a support plate is fixedly installed on the right side of the connecting ring, a steering member is fixedly installed on the top of the support plate, a mounting platform is fixedly installed on the outer surface of the steering member, the top of the mounting platform is fixedly connected to the mounting frame, a drive box is fixedly installed on the adjustment bracket, and the drive structure is arranged inside the drive box.

[0007] Furthermore, the driving structure includes a rack slidably installed inside the driving box, the outer surface of the rack is meshed with the outer surface of the connecting ring, the rear side wall of the inner cavity of the driving box is provided with a supporting assembly for supporting the movement of the rack, and the interior of the driving box is provided with a driving assembly for controlling the left and right movement of the rack.

[0008] Furthermore, the installation frame is located on the top of the adjustment bracket, the bottom of the adjustment bracket is fixedly installed with piles and embedded parts, and the satellite terminal is fixedly installed on the installation frame.

[0009] Furthermore, the steering member includes a round cake bin and a bearing, the inner circumferential wall of the bearing is fixedly connected to the outer circumferential wall of the round cake bin, and twenty-four fixing grooves are opened inside the round cake bin and are symmetrically distributed at the center of the round cake bin.

[0010] Furthermore, the mounting platform includes a columnar housing and a locking bolt, wherein the locking bolt is threadedly mounted on the columnar housing, the inner circumferential wall of the columnar housing is fixedly connected to the outer circumferential wall of the bearing, and one end of the locking bolt penetrates and extends to the interior of the fixing groove.

[0011] Furthermore, the drive box includes a protective chamber and a protective door, the protective chamber is fixedly mounted on the adjustment bracket, the protective door is hinged to the front side of the protective chamber, and the drive structure is arranged inside the protective chamber.

[0012] Furthermore, the support assembly includes a limit bar and a limit slot, the limit bar is fixedly mounted on the rear side wall of the inner cavity of the drive box, the limit slot is opened on the back side of the rack, and the inner wall of the limit slot is slidably connected to the outer surface of the limit bar.

[0013] Furthermore, the driving assembly includes a threaded rod and an asynchronous motor, the output shaft of the asynchronous motor is fixedly connected to one end of the threaded rod, the asynchronous motor is fixedly mounted on the inner bottom wall of the driving box, and the rack is threadedly mounted on the outer surface of the threaded rod.

[0014] Compared with the prior art, the technical solution of this application has the following beneficial effects:

[0015] The satellite terminal adjustment bracket is provided with an adjustment structure and a drive structure, so that the asynchronous motor in the drive assembly is used as a drive source and the rotation of the connecting ring is controlled by mechanical transmission, so that the connecting ring drives the satellite terminal on the top of the mounting platform to flip through the support plate, and the locking bolt in the mounting platform can be rotated to release the fixed connection between the mounting platform and the steering member, so that it is convenient for workers to rotate the mounting platform to move the satellite terminal, so that after the satellite terminal adjustment bracket is flexibly installed, the direction of the satellite terminal can be adjusted, thereby facilitating the installation and use of the satellite terminal, thereby enhancing the practicality of the satellite terminal adjustment bracket. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 It is a schematic diagram of the structure of the utility model;

[0017] Figure 2 This is a schematic diagram of the structure of the utility model Figure 1 A in the enlarged view;

[0018] Figure 3 It is a three-dimensional schematic diagram of the structural mounting platform and mounting bracket of the utility model.

[0019] In the figure: 1. adjustment bracket; 2. mounting frame; 3. satellite terminal; 41. connecting column; 42. connecting ring; 43. support plate; 44. steering member; 45. mounting platform; 46. drive box; 47. rack; 48. support assembly; 49. drive assembly. DETAILED DESCRIPTION

[0020] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0021] See also Figure 1-3 In this embodiment, a satellite terminal adjustment bracket includes an adjustment bracket 1, a mounting frame 2 is arranged on the adjustment bracket 1, a satellite terminal 3 is arranged on the mounting frame 2, an adjustment structure and a driving structure are arranged on the adjustment bracket 1, the mounting frame 2 is located at the top of the adjustment bracket 1, piles and embedded parts are fixedly installed at the bottom of the adjustment bracket 1, and the satellite terminal 3 is fixedly installed on the mounting frame 2.

[0022] In the implementation of this example, the adjustment structure includes a connecting column 41 rotatably installed between the front and rear side walls of the inner cavity of the adjustment bracket 1, a connecting ring 42 is fixedly installed on the outer surface of the connecting column 41, a support plate 43 is fixedly installed on the right side of the connecting ring 42, a steering member 44 is fixedly installed on the top of the support plate 43, and a mounting platform 45 is fixedly installed on the outer surface of the steering member 44. The steering member 44 includes a round cake bin and a bearing, the inner circumferential wall of the bearing is fixedly connected to the outer circumferential wall of the round cake bin, twenty-four fixed grooves are opened inside the round cake bin and are symmetrically distributed at the center of the round cake bin, so as to support the rotation of the mounting platform 45, and the top of the mounting platform 45 is fixedly connected to the mounting frame 2, a drive box 46 is fixedly installed on the adjustment bracket 1, and a drive structure is arranged inside the drive box 46, so as to control the flipping of the connecting ring 42 and the support plate 43, and the drive box 46 includes a protective bin and a protective door, the protective bin is fixedly installed on the adjustment bracket 1, the protective door is hinged to the front of the protective bin, and the drive structure is arranged inside the protective bin, so as to open the drive box 46 and inspect and maintain the drive structure.

[0023] Among them, the mounting platform 45 includes a columnar warehouse body and a locking bolt, the locking bolt is threadedly installed on the columnar warehouse body, the inner circumferential wall of the columnar warehouse body is fixedly connected to the outer circumferential wall of the bearing, and one end of the locking bolt passes through and extends to the inside of the fixing groove, which is convenient for rotating the columnar warehouse body and adjusting the orientation of the satellite terminal 3, and the locking bolt can be rotated and inserted into the fixing groove to achieve the angle of fixing the satellite terminal 3.

[0024] By adopting the above technical solution, it is possible to utilize the driving structure to control the rotation of the connecting ring 42, thereby controlling the connecting column 41 and driving the support plate 43 to flip, thereby controlling the mounting frame 2 and the satellite terminal 3 to flip, and the locking bolt in the mounting platform 45 can be rotated to release the position fixation of the mounting platform 45 and the steering member 44, and then the columnar warehouse body in the mounting platform 45 can be rotated, thereby realizing multi-angle adjustment of the orientation of the satellite terminal 3 on the mounting frame 2, thereby facilitating the flexible installation of the satellite terminal adjustment bracket, and then adjusting the orientation of the satellite terminal 3.

[0025] In the present embodiment, the driving structure includes a rack 47 slidably mounted inside a driving box 46, the outer surface of the rack 47 meshes with the outer surface of the connecting ring 42, so that the movable rack 47 can drive the connecting ring 42 to rotate, and a support assembly 48 for supporting the movement of the rack 47 is provided on the rear side wall of the inner cavity of the driving box 46, the support assembly 48 includes a limit bar and a limit groove, the limit bar is fixedly mounted on the rear side wall of the inner cavity of the driving box 46, the limit groove is provided on the back side of the rack 47, the inner wall of the limit groove is slidably connected to the outer surface of the limit bar, so as to limit the rack 47 to move left and right only on the outer surface of the limit bar, and a driving assembly 49 for controlling the left and right movement of the rack 47 is provided inside the driving box 46.

[0026] Among them, the driving component 49 includes a threaded rod and an asynchronous motor, the output shaft of the asynchronous motor is fixedly connected to one end of the threaded rod, the asynchronous motor is fixedly installed on the inner bottom wall of the driving box 46, and the rack 47 is threadedly installed on the outer surface of the threaded rod, so that the asynchronous motor drives the threaded rod to rotate and realizes the control of the rack 47 to move left and right.

[0027] By adopting the above technical solution, the asynchronous motor in the internal drive component 49 of the start-up drive box 46 is realized, so that the asynchronous motor drives the threaded rod to rotate, thereby controlling the rack 47 threadedly connected to the outer surface of the threaded rod to move to the right on the outer surface of the limit bar, and then the moving rack 47 drives the connecting ring 42 meshing with it to rotate.

[0028] The working principle of the above embodiment is:

[0029] When the satellite terminal adjustment bracket is in use, the asynchronous motor in the driving component 49 inside the driving box 46 is started, so that the asynchronous motor drives the threaded rod to rotate, thereby controlling the rack 47 threadedly connected to the outer surface of the threaded rod to move to the right on the outer surface of the limit bar, and then the moving rack 47 drives the connecting ring 42 engaged with it to rotate, thereby controlling the connecting column 41 and driving the support plate 43 to flip, thereby controlling the installation frame 2 and the satellite terminal 3 to flip, and the locking bolt in the mounting platform 45 can be rotated, thereby releasing the position fixation of the mounting platform 45 and the steering member 44, and then the columnar warehouse in the mounting platform 45 can be rotated, thereby realizing multi-angle adjustment of the orientation of the satellite terminal 3 on the mounting frame 2, thereby facilitating the flexible installation of the satellite terminal adjustment bracket, and then adjusting the orientation of the satellite terminal 3.

[0030] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device. In the absence of further restrictions, the elements defined by the sentence "comprise a ..." do not exclude the existence of other identical elements in the process, method, article or device including the elements.

[0031] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A satellite terminal adjustment bracket, comprising an adjustment bracket (1), characterized in that: The adjusting bracket (1) is provided with a mounting frame (2), the mounting frame (2) is provided with a satellite terminal (3), and the adjusting bracket (1) is provided with an adjusting structure and a driving structure; The adjustment structure comprises a connecting column (41) rotatably mounted between the front and rear side walls of the inner cavity of the adjustment bracket (1); a connecting ring (42) is fixedly mounted on the outer surface of the connecting column (41); a supporting plate (43) is fixedly mounted on the right side of the connecting ring (42); a steering member (44) is fixedly mounted on the top of the supporting plate (43); a mounting platform (45) is fixedly mounted on the outer surface of the steering member (44); the top of the mounting platform (45) is fixedly connected to the mounting frame (2); a driving box (46) is fixedly mounted on the adjustment bracket (1); and the driving structure is arranged inside the driving box (46).

2. The satellite terminal adjustment bracket according to claim 1, characterized in that: The driving structure comprises a rack (47) slidably mounted inside a driving box (46), the outer surface of the rack (47) meshing with the outer surface of a connecting ring (42), a supporting assembly (48) for supporting the movement of the rack (47) is arranged on the rear side wall of the inner cavity of the driving box (46), and a driving assembly (49) for controlling the left and right movement of the rack (47) is arranged inside the driving box (46).

3. The satellite terminal adjustment bracket according to claim 1, characterized in that: The installation frame (2) is located on the top of the adjustment bracket (1), a pile and an embedded part are fixedly installed on the bottom of the adjustment bracket (1), and the satellite terminal (3) is fixedly installed on the installation frame (2).

4. The satellite terminal adjustment bracket according to claim 1, characterized in that: The steering member (44) comprises a round cake bin and a bearing, the inner peripheral wall of the bearing is fixedly connected to the outer peripheral wall of the round cake bin, and twenty-four fixing grooves are provided inside the round cake bin and are symmetrically distributed at the center of the round cake bin.

5. The satellite terminal adjustment bracket according to claim 4, characterized in that: The mounting platform (45) comprises a columnar housing and a locking bolt, wherein the locking bolt is threadedly mounted on the columnar housing, the inner peripheral wall of the columnar housing is fixedly connected to the outer peripheral wall of the bearing, and one end of the locking bolt penetrates and extends into the interior of the fixing groove.

6. The satellite terminal adjustment bracket according to claim 1, characterized in that: The drive box (46) comprises a protection chamber and a protection door, the protection chamber is fixedly mounted on the adjustment bracket (1), the protection door is hinged to the front side of the protection chamber, and the drive structure is arranged inside the protection chamber.

7. The satellite terminal adjustment bracket according to claim 2, characterized in that: The support assembly (48) comprises a limit bar and a limit slot, wherein the limit bar is fixedly mounted on the rear side wall of the inner cavity of the drive box (46), the limit slot is opened on the back side of the rack (47), and the inner wall of the limit slot is slidably connected to the outer surface of the limit bar.

8. The satellite terminal adjustment bracket according to claim 2, characterized in that: The driving assembly (49) comprises a threaded rod and an asynchronous motor, wherein the output shaft of the asynchronous motor is fixedly connected to one end of the threaded rod, the asynchronous motor is fixedly mounted on the inner bottom wall of the driving box (46), and the rack (47) is threadedly mounted on the outer surface of the threaded rod.