Oscillator for satellite antenna

By designing a satellite antenna oscillator including vertical tube, first branch, second branch, support arm, through hole and vertical groove, the existing satellite antenna cannot meet the lightweight requirements and poor performance, and the effect of improving antenna performance and receiving multi-frequency signals is achieved, while reducing costs and labor.

CN222654329UActive Publication Date: 2025-03-21SUZHOU JUNCHANG COMM TECH CO LTD
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Patent Information

Application Number
CN202421512594.X
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-06-28
Publication Date
2025-03-21
Estimated Expiration
2034-06-28

AI Technical Summary

Technical Problem

Existing satellite antennas cannot meet the lightweight requirements and have poor performance.

Method used

A vibrator for satellite antennas is designed, including vertical tubes, first branches, second branches, support arms, through holes and vertical grooves. Through the coordination of these structures, the antenna performance can be improved, multi-frequency signals can be accepted, and the overall structure is small, reducing costs and labor.

Benefits of technology

Through the coordination of the first and second branches and vertical tubes, the performance of the antenna is improved, allowing it to accept multi-frequency signals, with a small overall structure, reducing cost and labor.

✦ Generated by Eureka AI based on patent content.

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    Figure CN222654329U_ABST
Patent Text Reader

Abstract

The satellite antenna oscillator comprises a vertical cylinder, a pair of first branches are arranged on the outer wall of the top end of the vertical cylinder in a left-right symmetry mode, a pair of second branches are arranged on the outer wall of the top end of the vertical cylinder in a front-back symmetry mode, a supporting arm is arranged on the inner wall of the top end of the vertical cylinder in a protruding mode, and a through hole is formed in the supporting arm in a concave mode; vertical grooves are concavely formed in the vertical cylinder on the two sides of the through hole and penetrate through the inner wall and the outer wall of the vertical cylinder. According to the oscillator, the antenna performance is improved through cooperation of the first branch knot, the second branch knot and the vertical cylinder, multi-frequency signals can be received, the overall structure is small, and cost and labor are reduced.
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Description

Technical Field

[0001] The present application relates to the field of electronic components, and in particular to an oscillator for a satellite antenna. Background Art

[0002] Existing satellite antennas cannot meet the lightweight requirements and have poor performance. Utility Model Content

[0003] The utility model aims to provide a vibrator for a satellite antenna to overcome the deficiencies in the prior art.

[0004] In order to achieve the above purpose, the utility model provides the following technical solutions:

[0005] An embodiment of the present application discloses a vibrator for a satellite antenna, which is characterized in that it includes a vertical tube, a pair of first branches are symmetrically provided on the outer wall of the top end of the vertical tube, a pair of second branches are symmetrically provided on the outer wall of the top end of the vertical tube, a support arm is convexly provided on the inner wall of the top end of the vertical tube, a through hole is recessed on the support arm, vertical grooves are recessed on the vertical tube on both sides of the through hole, and the vertical grooves penetrate the inner and outer walls of the vertical tube.

[0006] Preferably, in the above-mentioned vibrator for satellite antenna, the inner diameter of the vertical tube is 1.9 mm~1.95 mm.

[0007] Preferably, in the above-mentioned vibrator for satellite antenna, the distance between two opposite ends of a pair of the first branches is 9.93 mm to 9.97 mm, and the width of the first branches is 0.6 mm to 0.63 mm.

[0008] Preferably, in the above-mentioned vibrator for a satellite antenna, the distance between two opposite ends of a pair of the second branches is 6.92 mm to 6.96 mm, and the width of the second branch is 0.6 mm to 0.63 mm.

[0009] Preferably, in the above-mentioned vibrator for satellite antenna, the through hole is coaxially arranged with the vertical tube.

[0010] Preferably, in the above-mentioned vibrator for satellite antenna, a base is fixed to the bottom end of the vertical tube, a cavity connected to the vertical tube is provided in the base, the cross-section of the cavity is stepped, and the diameter of the cavity increases from top to bottom.

[0011] Compared with the prior art, the advantages of the utility model are:

[0012] The antenna performance is improved through the cooperation of the first branch, the second branch and the vertical tube, and multi-frequency signals can be received. The overall structure is small, and the cost and labor are reduced. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments recorded in the present application. For ordinary technicians in this field, it is easy to obtain other drawings based on these drawings without creative work.

[0014] Figure 1 The figure is a three-dimensional diagram of a vibrator for a satellite antenna in a specific embodiment of the utility model;

[0015] Figure 2 The figure shows a top view of a vibrator for a satellite antenna in a specific embodiment of the utility model;

[0016] Figure 3 Shown is a schematic structural diagram of a vibrator for a satellite antenna in a specific embodiment of the utility model. DETAILED DESCRIPTION

[0017] The following will be combined with the drawings in the embodiments of the utility model to describe the technical solutions in the embodiments of the utility model in detail. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments of 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.

[0018] Ginseng Figures 1 to 3 As shown, the vibrator for the satellite antenna in this embodiment includes a vertical tube 1, a pair of first branches 3 are symmetrically provided on the outer wall of the top end of the vertical tube 1, a pair of second branches 4 are symmetrically provided on the outer wall of the top end of the vertical tube 1, a support arm 5 is convexly provided on the inner wall of the top end of the vertical tube 1, a through hole 6 is recessed on the support arm 5, and vertical grooves 7 are recessed on the vertical tube 1 on both sides of the through hole 6, and the vertical grooves 7 pass through the inner and outer walls of the vertical tube 1.

[0019] Furthermore, the inner diameter of the vertical tube 1 is 1.9 mm to 1.95 mm.

[0020] Furthermore, the distance between the two opposite ends of a pair of first branches 3 is 9.93 mm to 9.97 mm, and the width of the first branches 3 is 0.6 mm to 0.63 mm.

[0021] Furthermore, the distance between the two opposite ends of a pair of second branches 4 is 6.92 mm to 6.96 mm, and the width of the second branches 4 is 0.6 mm to 0.63 mm.

[0022] Furthermore, the through hole 6 is coaxially arranged with the vertical tube 1, and the coaxiality during assembly is ensured by the through hole. With the cooperation of the vertical groove, the installation is convenient while ensuring the overall performance of the antenna.

[0023] Furthermore, a base 2 is fixed to the bottom end of the vertical tube 1, and a cavity 8 communicating with the vertical tube 1 is provided in the base 2. The cross section of the cavity 8 is stepped, and the diameter of the cavity 8 increases from top to bottom.

[0024] In this technical solution, the antenna performance is improved through the cooperation of the first branch, the second branch and the vertical tube, and multi-frequency signals can be received. The overall structure is small, and the cost and labor are reduced.

[0025] 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.

[0026] The above is only a specific implementation method of the present application. It should be pointed out that for ordinary technicians in this technical field, several improvements and modifications can be made without departing from the principles of the present application. These improvements and modifications should also be regarded as the scope of protection of the present application.

Claims

1. A vibrator for a satellite antenna, characterized in that: It includes a vertical tube, a pair of first branches are symmetrically arranged on the outer wall of the top end of the vertical tube, a pair of second branches are symmetrically arranged on the outer wall of the top end of the vertical tube, a support arm is convexly arranged on the inner wall of the top end of the vertical tube, a through hole is recessed on the support arm, vertical grooves are recessed on the vertical tube on both sides of the through hole, and the vertical grooves run through the inner and outer walls of the vertical tube.

2. A satellite antenna vibrator according to claim 1, characterized in that: The inner diameter of the vertical cylinder is 1.9 mm to 1.95 mm.

3. The vibrator for a satellite antenna according to claim 1, characterized in that: The distance between the two opposite ends of a pair of the first branches is 9.93 mm to 9.97 mm, and the width of the first branches is 0.6 mm to 0.63 mm.

4. The satellite antenna vibrator according to claim 1, characterized in that: The distance between the two opposite ends of a pair of the second branches is 6.92 mm to 6.96 mm, and the width of the second branches is 0.6 mm to 0.63 mm.

5. The satellite antenna vibrator according to claim 1, characterized in that: The through hole is coaxially arranged with the vertical cylinder.

6. The vibrator for a satellite antenna according to claim 1, characterized in that: A base is fixed at the bottom end of the vertical cylinder, and a cavity connected to the vertical cylinder is arranged in the base. The cross section of the cavity is stepped, and the diameter of the cavity increases from top to bottom.