一种一体化无人值守卫星通信终端

By integrating insect repellent components, auxiliary components, and locking components into the unattended satellite communication terminal, the problem of insects corroding the circuits in harsh environments has been solved, thereby improving signal stability and ease of maintenance.

CN224521057UActive Publication Date: 2026-07-17
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Patent Information

Application Number
CN202521713264.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Priority Date
2024-08-13
Filing Date
2025-08-13
Publication Date
2026-07-17
Estimated Expiration
2035-08-13

AI Technical Summary

Technical Problem

Existing unattended satellite communication terminals are susceptible to corrosion by pests in harsh environments, leading to signal interruptions, and lack effective protective measures.

Method used

An integrated unattended satellite communication terminal was designed, which includes an insect repellent component, an auxiliary component, and a locking component. The insect repellent component prevents insect corrosion by releasing insect repellent liquid, the auxiliary component improves stability, and the locking component facilitates disassembly and installation, enabling regular maintenance.

Benefits of technology

It effectively prevents pests from corroding the circuits, simplifies the maintenance process, reduces signal interruptions, and improves the reliability and ease of maintenance of the equipment.

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Abstract

本实用新型公开了一种一体化无人值守卫星通信终端,涉及卫星通信终端技术领域。本实用新型包括安装基座,所述安装基座上分别设有驱虫组件、辅助组件和卡合组件,所述驱虫组件用于释放一定量的驱虫液以对卫星通信终端本体的线路通过驱虫液的气味进行驱虫,辅助组件用于提升驱虫组件运作的稳定性防止驱虫组件出现歪斜。本实用新型通过与滑槽滑动的滑珠以及与限位槽滑动的限位块相配合,便于提升滑杆移动的稳定性,同时通过主半卡环与副半卡环相卡合便于将储液箱整体与卫星通信终端本体相安装,且便于将储液箱与卫星通信终端本体相拆卸,利于将储液箱内部的所有驱虫液进行更换,便于在对卫星通信终端本体进行定期维护时来定期对驱虫液进行更换。
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Claims

1. An integrated unattended satellite communication terminal comprising a mounting base (1), characterized in that, The mounting base (1) is provided with an insect repellent component (2), an auxiliary component (3), and a locking component (4). The insect repellent component (2) is used to release a certain amount of insect repellent liquid to repel insects from the lines of the satellite communication terminal body (5) through the smell of the insect repellent liquid. The auxiliary component (3) is used to improve the stability of the operation of the insect repellent component (2) and prevent the insect repellent component (2) from tilting. The locking component (4) is used to lock the insect repellent component (2) to the satellite communication terminal body (5) and facilitate the disassembly of the insect repellent component (2) from the satellite communication terminal body (5). The top of the mounting base (1) is connected to the satellite communication terminal body (5).

2. The integrated unattended satellite terminal of claim 1, wherein The insect repellent assembly (2) includes a fixed cylinder (21), a liquid storage tank (22), a baffle (24), a contraction spring (27), and an inlet pipe (29). The fixed cylinder (21) is placed at the top of the mounting base (1). The liquid storage tank (22) is located at the top of the fixed cylinder (21). A sliding rod (23) is slidably connected to one side of the liquid storage tank (22). The baffle (24) is located at the bottom of the sliding rod (23). A sealing gasket (25) is connected to the bottom of the baffle (24). A pressure block (26) is connected to one end of the sliding rod (23). The contraction spring (27) is sleeved on the surface of the sliding rod (23). Several leakage holes (28) are opened on the surface of the fixed cylinder (21). An inlet pipe (29) is connected to one side of the liquid storage tank (22).

3. The integrated unattended satellite terminal of claim 2, wherein The two ends of the contraction spring (27) are respectively connected to one end of the pressure block (26) and one side of the liquid storage tank (22).

4. The integrated unattended satellite terminal of claim 2, wherein, One end of the inlet pipe (29) is threaded with a sealing cap.

5. The integrated unattended satellite terminal of claim 2, wherein, The auxiliary component (3) includes two slides (31), a connecting plate (33), and a limiting block (35). The two slides (31) are both located inside the bottom of the liquid storage tank (22). Sliding balls (32) are slidably connected to the inner sides of the two slides (31). The tops of the two sliding balls (32) are connected to the bottom of the baffle (24). The connecting plate (33) is located inside the liquid storage tank (22). Two limiting grooves (34) are provided inside the connecting plate (33). The inner side of the limiting block (35) is connected to the surface of the slide rod (23). The surface of the limiting block (35) is slidably connected to the inner sides of the two limiting grooves (34).

6. An integrated unattended satellite terminal according to claim 5, wherein, The engaging assembly (4) includes two connecting rods (41) and two secondary half-locking rings (43). One of the connecting rods (41) is located on the surface of the fixed cylinder (21), and the other connecting rod (41) is located on the back of the liquid storage tank (22). One end of each of the two connecting rods (41) is connected to a primary half-locking ring (42). The two secondary half-locking rings (43) are engaged with the two primary half-locking rings (42) respectively, and the inner sides of the two secondary half-locking rings (43) are connected to the surface of the satellite communication terminal body (5).