Satellite internet terminal wiring locking mechanism

Abstract

The utility model discloses a satellite internet terminal wiring locking mechanism which comprises a base, a plurality of pressing structures are arranged at the top end of the base, each pressing structure comprises a positioning seat, a movable frame, a rotating handle and a linkage arm, the positioning seats are installed on the upper surface of the base at equal intervals, the movable frames are rotatably installed on the outer walls of the positioning seats, and the rotating handles are installed on the movable frames. A linkage arm is rotatably installed on the inner wall of one side of the movable frame, a rotating handle is rotatably installed at the end, away from the movable frame, of the linkage arm, the bottom of the rotating handle is rotatably connected with the outer wall of the positioning base, side connecting bases are arranged on the outer walls of the two sides of the base, positioning holes are formed in the centers of the interiors of the side connecting bases, and the two ends of the positioning holes extend to the exteriors of the side connecting bases. According to the utility model, not only is the locking effect of the wiring locking mechanism on the satellite internet terminal lead wire ensured, but also the purpose of easily manually locking the satellite internet terminal lead wire is achieved, and the convenience of the wiring locking mechanism in use is improved.

Description

Technical Field

[0001] This utility model relates to the field of spacecraft docking technology, specifically a satellite internet terminal wiring locking mechanism. Background Technology

[0002] With the rapid development of satellite internet technology, the demand for data transmission between satellite terminals and satellites is increasing. In the process of satellite communication, the stability and reliability of the wiring are crucial to ensuring communication quality. Therefore, it is particularly important to develop a wiring locking mechanism for satellite internet terminals.

[0003] Referring to CN213878911U, a wiring locking mechanism for electrical components includes a housing. A box is fixedly connected to the inner wall of the housing. A set of through holes is provided on both the upper and bottom surfaces of the box. A fixing plate is fixedly connected to the inner wall of the box. Two sliding grooves are provided on the inner side wall of the box. A slider adapted to the groove is engaged inside each groove. A clamping plate is fixedly connected to the side of the two sliders that are close to each other. Two threaded holes are provided on the back of the clamping plate. This wiring locking mechanism for electrical components, by setting... The device includes a motor that drives a connecting rod to rotate. This rotation of the connecting rod, in turn, causes the first pulley to rotate via a belt. The threaded rod then moves a clamping plate, which clamps the wires to prevent them from being pulled off by external forces, thus preventing short circuits and fires. While this wiring locking mechanism is generally effective, it is not ideal for multi-point locking of the leads, making it difficult to achieve the desired locking effect and frequently causing problems for users. Utility Model Content

[0004] The purpose of this utility model is to provide a satellite internet terminal wiring locking mechanism to solve the problem that although the wiring locking mechanism proposed in the background art can be well applied, it is usually not convenient to perform multi-point locking of the lead wire, so that the locking effect of the wiring locking mechanism on the lead wire is still difficult to achieve the expected result.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a satellite internet terminal wiring locking mechanism, including a base, with a plurality of pressing structures at the top of the base. Each pressing structure includes a positioning seat, a movable frame, a rotating handle, and a linkage arm. The upper surface of the base is equipped with equally spaced positioning seats. A movable frame is rotatably mounted on the outer wall of the positioning seats. A linkage arm is rotatably mounted on the inner wall of one side of the movable frame. A rotating handle is rotatably mounted on the end of the linkage arm away from the movable frame. The bottom of the rotating handle is rotatably connected to the outer wall of the positioning seat.

[0006] Preferably, side connecting seats are provided on the outer walls of both sides of the base, and a positioning hole is provided at the center of the side connecting seat. Both ends of the positioning hole extend to the outside of the side connecting seat. The positioning hole is provided to bolt and install the wiring locking mechanism.

[0007] Preferably, the clamping structure includes an upper connecting seat and an upper hexagonal nut. An upper connecting seat is provided on one side of the top of the movable frame, and an upper hexagonal nut is provided at the center of the top of the upper connecting seat. The upper hexagonal nut is provided to accommodate the threaded rod.

[0008] Preferably, the clamping structure includes a lower seat and a lower hexagonal nut. The lower seat is provided at the end of the movable frame away from the upper connecting seat, and the lower hexagonal nut is provided at the center of the bottom end of the lower seat. The lower hexagonal nut is provided to accommodate the threaded rod.

[0009] Preferably, the clamping structure includes a threaded rod and a pressure head. The threaded rod is installed on the internal threads of the upper and lower hexagonal nuts. The pressure head is installed at the bottom end of the threaded rod. The pressure head is used to clamp and lock the lead wire connected to the satellite internet terminal.

[0010] Preferably, the clamping structure includes a circular hole, and several circular holes are provided on both sides of the bottom of the positioning seat. The circular holes are provided so that the positioning seat can be bolted to the top of the base by means of bolts.

[0011] Compared with the prior art, the beneficial effects of this utility model are: the satellite internet terminal wiring locking mechanism not only ensures the locking effect of the satellite internet terminal lead wire when the wiring locking mechanism is used, but also achieves the purpose of easy manual locking of the satellite internet terminal lead wire, and improves the convenience of using the wiring locking mechanism;

[0012] (1) By setting several clamping structures at the top of the base, the lead wire connected to the satellite Internet terminal is passed through the top of the base and the lead wire is aligned below the pressure head. The lead wire can be clamped and locked at multiple points by multiple clamping structures, thereby ensuring the locking effect of the wiring locking mechanism on the lead wire of the satellite Internet terminal when it is used.

[0013] (2) By turning the threaded rod, the threaded rod rotates and slides down inside the upper and lower hexagonal nuts, so that the threaded rod drives the pressure head to move downward, and the pressure head can press and lock the lead wire connected to the satellite Internet terminal to the top of the base, thereby achieving the purpose of easily locking the lead wire of the satellite Internet terminal manually.

[0014] (3) By rotating the handle, the movable frame is slightly rotated on the outer wall of the positioning seat via the linkage arm, thereby increasing the distance between the pressure head and the base, making it easier to thread the lead wire connected to the satellite Internet terminal through the top of the base, thus improving the convenience of using the wiring locking mechanism. Attached Figure Description

[0015] Figure 1 This is a three-dimensional structural diagram of the present invention;

[0016] Figure 2 This is an enlarged schematic diagram of the clamping structure of this utility model;

[0017] Figure 3 This is a schematic diagram of the right side structure of the positioning seat of this utility model;

[0018] Figure 4 This is a schematic diagram of the positioning seat structure of this utility model from below.

[0019] In the diagram: 1. Base; 2. Side connecting seat; 3. Positioning hole; 4. Clamping structure; 401. Positioning seat; 402. Movable frame; 403. Rotary handle; 404. Linkage arm; 405. Upper connecting seat; 406. Upper hexagonal nut; 407. Lower seat body; 408. Lower hexagonal nut; 409. Threaded rod; 410. Pressure head; 411. Round hole. Detailed Implementation

[0020] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present utility model without creative effort are within the scope of protection of the present utility model.

[0021] Please see Figure 1-4 An embodiment of this utility model provides a satellite internet terminal wiring locking mechanism, including a base 1, with side connecting seats 2 provided on the outer walls of both sides of the base 1, and a positioning hole 3 provided at the center of the side connecting seat 2, with both ends of the positioning hole 3 extending to the outside of the side connecting seat 2.

[0022] In use, the positioning hole 3 is provided to bolt and install the wiring locking mechanism;

[0023] The top of the base 1 is provided with several clamping structures 4. The clamping structure 4 includes an upper connecting seat 405 and an upper hexagonal nut 406. The upper connecting seat 405 is provided on one side of the top of the movable frame 402, and the upper hexagonal nut 406 is provided at the center of the top of the upper connecting seat 405.

[0024] In use, the upper hexagonal nut 406 is used to install the threaded rod 409;

[0025] The clamping structure 4 includes a lower seat 407 and a lower hexagonal nut 408. The lower seat 407 is provided at the end of the movable frame 402 away from the upper connecting seat 405, and the lower hexagonal nut 408 is provided at the center of the bottom end of the lower seat 407.

[0026] In use, the threaded rod 409 is installed by setting the lower hexagonal nut 408;

[0027] The clamping structure 4 includes a threaded rod 409 and a pressure head 410. The threaded rod 409 is installed on the internal threads of the upper hexagonal nut 406 and the lower hexagonal nut 408. The pressure head 410 is installed at the bottom end of the threaded rod 409.

[0028] When in use, the pressure head 410 is set to clamp and lock the lead wire connected to the satellite internet terminal.

[0029] The clamping structure 4 includes a circular hole 411, and several circular holes 411 are provided on both sides of the bottom of the positioning seat 401;

[0030] In use, the round hole 411 is provided so that the positioning seat 401 can be bolted to the top of the base 1 with the help of bolts;

[0031] The clamping structure 4 includes a positioning seat 401, a movable frame 402, a rotating handle 403, and a linkage arm 404. The upper surface of the base 1 is equipped with equally spaced positioning seats 401. The movable frame 402 is rotatably mounted on the outer wall of the positioning seat 401. The linkage arm 404 is rotatably mounted on the inner wall of one side of the movable frame 402. The rotating handle 403 is rotatably mounted on the end of the linkage arm 404 away from the movable frame 402. The bottom of the rotating handle 403 is rotatably connected to the outer wall of the positioning seat 401.

[0032] In this embodiment, the wiring locking mechanism is first attached to the satellite internet terminal by means of a bolt that passes through the positioning hole 3 and is screwed into the threaded hole on the side of the satellite internet terminal interface. Then, by turning the threaded rod 409, it rotates and slides downwards within the upper hexagonal nut 406 and lower hexagonal nut 408, causing the threaded rod 409 to move the pressure head 410 downwards. The pressure head 410 then presses and locks the lead wire connected to the satellite internet terminal to the top of the base 1, facilitating manual locking of the satellite internet terminal lead wire. Finally, by rotating the handle 403, the wiring locking mechanism is secured to the satellite internet terminal. The linkage arm 404 drives the movable frame 402 to rotate slightly on the outer wall of the positioning seat 401, thereby increasing the distance between the pressure head 410 and the base 1. This makes it easier to thread the lead wire connected to the satellite internet terminal through the top of the base 1, improving the convenience of using the wiring locking mechanism. Finally, several pressing structures 4 are set at the top of the base 1. The lead wire connected to the satellite internet terminal is threaded through the top of the base 1 and aligned with the pressure head 410. The multiple pressing structures 4 can then perform multi-point pressing and locking of the lead wire to ensure the locking effect of the wiring locking mechanism on the lead wire of the satellite internet terminal, thus completing the use of the wiring locking mechanism.

[0033] It should be noted that, in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such process, method, article, or apparatus.

[0034] Although the present invention has been described above with reference to embodiments, various modifications can be made and components can be replaced with equivalents without departing from the scope of the present invention. In particular, as long as there is no structural conflict, the features in the embodiments disclosed in this invention can be combined with each other in any way. The lack of an exhaustive description of these combinations in this specification is merely for the sake of brevity and resource conservation. Therefore, the present invention is not limited to the specific embodiments disclosed herein, but includes all technical solutions falling within the scope of the claims.

Claims

1. A satellite internet terminal wiring lock mechanism, characterized by: The utility model provides a kind of pressing structure, including base (1), the top of the base (1) is provided with several compression structures (4), the compression structure (4) includes positioning seat (401), movable frame (402), handle (403) and linkage arm (404), the upper surface of the base (1) is installed with equidistant positioning seat (401), movable frame (402) is rotatably installed on the outer wall of positioning seat (401), linkage arm (404) is rotatably installed on the inner wall of one side of movable frame (402), handle (403) is rotatably installed on the end of linkage arm (404) away from movable frame (402), the bottom of handle (403) is rotatably connected with the outer wall of positioning seat (401).

2. The satellite internet terminal wiring lock mechanism of claim 1, wherein: The outer wall of the both sides of the base (1) is provided with side connecting seat (2), the center position inside side connecting seat (2) is provided with positioning hole (3), both ends of positioning hole (3) extend to the outside of side connecting seat (2).

3. The satellite internet terminal wiring lock mechanism of claim 1, wherein: The compression structure (4) includes upper connecting seat (405) and upper hexagon nut (406), one side of the top of movable frame (402) is provided with upper connecting seat (405), the center position of the top of upper connecting seat (405) is provided with upper hexagon nut (406).

4. The satellite internet terminal wiring lock mechanism of claim 3, wherein: The compression structure (4) includes lower seat body (407) and lower hexagon nut (408), the end of movable frame (402) away from upper connecting seat (405) is provided with lower seat body (407), the center position of the bottom of lower seat body (407) is provided with lower hexagon nut (408).

5. The satellite internet terminal wiring lock mechanism of claim 4, wherein: The compression structure (4) includes threaded rod (409) and pressure head (410), the inside of upper hexagon nut (406) and lower hexagon nut (408) is screw-threaded with threaded rod (409), the bottom of threaded rod (409) is installed with pressure head (410).

6. The satellite Internet terminal wiring lock mechanism of claim 1, wherein: The compression structure (4) includes round hole (411), the both sides of the bottom of positioning seat (401) are provided with several round holes (411).

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