Maritime satellite communication terminal

Abstract

The utility model discloses a maritime satellite communication terminal, which relates to the technical field of communication equipment and comprises a fixed plate, a box body is fixedly arranged on the fixed plate, an I-shaped block is arranged on the box body in a sliding manner, a flexible pad is arranged on the I-shaped block, a maritime satellite communication terminal body is fixedly arranged on the flexible pad, and a square frame is fixedly arranged at the bottom of the maritime satellite communication terminal body. Through cooperative use of the square frame, the limiting blocks, the sliding grooves, the rectangular blocks, the trapezoidal grooves, the threaded rods, the rotary knobs, the stand columns, the cross-shaped grooves, the limiting rods, the sliding plates, the first springs and the square holes, when the maritime satellite communication terminal body is installed, the maritime satellite communication terminal body can be rapidly installed and disassembled, fixation is firm, and the service life of the maritime satellite communication terminal body is prolonged. And through cooperative use of a second spring and a damping rod, during offshore operation, the satellite communication terminal body can be effectively damped, and the satellite communication terminal can effectively cope with an offshore working environment with more stormy waves.

Description

TECHNICAL FIELD

[0001] The utility model relates to communication equipment field especially relates to a maritime satellite communication terminal. BACKGROUND

[0002] At present, with the continuous progress of China's science and technology and the continuous development of communication industry, communication technology is applied to various industries, in the aspect of maritime affairs, in order to smooth communication, satellite communication terminal device is often used.

[0003] The existing maritime satellite communication terminal is difficult to install quickly, is very troublesome when detecting and maintaining, cannot satisfy people's use demand, and does not have the effect of buffering and shock absorption, stability is poor, and it is difficult to effectively cope with the working environment of more wind and wave on the sea. UTILIT Y MODEL CONTENT

[0004] The utility model aims at solving the shortcomings in the prior art and provides a maritime satellite communication terminal.

[0005] In order to solve the problems in the prior art, the utility model adopts the following technical scheme:

[0006] A maritime satellite communication terminal, including fixed plate, the fixed plate is equipped with box body, the box body is equipped with the I shape piece, the I shape piece is equipped with flexible pad, the flexible pad is equipped with maritime satellite communication terminal body, the maritime satellite communication terminal body bottom is equipped with square frame, the I shape piece is equipped with limit block, the I shape piece is equipped with the sliding slot, the sliding slot is equipped with the rectangle, the rectangle is equipped with trapezoidal groove, the rectangle front side is equipped with threaded rod, the threaded rod other end is equipped with knob, the I shape piece is equipped with stand, the limit block is equipped with cross slot, the stand top and cross slot sliding connection, a pair of the limit rod is equipped in the cross slot, a pair of the limit rod both sides are equipped with slide, the slide and cross slot sliding connection, the slide one side is equipped with first spring, the first spring other end is equipped with cross slot fixed connection, the square frame is equipped with a pair of square holes.

[0007] Preferably, a plurality of second springs are fixedly arranged in the box body, and the other ends of the second springs are fixedly connected with the bottom of the I-shaped block.

[0008] Preferably, the square frame penetrates the flexible pad, the square frame is located at the bottom center of the maritime satellite communication terminal body, the limit block is attached to the inside of the square frame, the top of the limit block is arc-shaped, and the I-shaped block penetrates the box body.

[0009] Preferably, one pair of said limiting rods is symmetrically arranged, and one end of the limiting rod in the cross-shaped slot is a right-angled triangle.

[0010] Preferably, the top of the column is inclined from the center to both sides, and the front side of the bottom of the column is inclined to the rear side.

[0011] Preferably, the threaded rod penetrates the sliding groove, and the oblong block is attached to the inner wall of the sliding groove.

[0012] Preferably, the column penetrates the sliding groove, and the limiting rods both penetrate the cross-shaped slot.

[0013] Preferably, a plurality of said second springs are arranged in a rectangular array, and the damping rods are respectively located at the centers of the second springs.

[0014] Compared with the prior art, the utility model has the beneficial effects that:

[0015] 1. In the utility model, through the cooperation of the square frame, the limiting block, the sliding groove, the oblong block, the trapezoidal slot, the threaded rod, the knob, the column, the cross-shaped slot, the limiting rod, the sliding plate, the first spring and the square hole, when the marine satellite communication terminal body is installed, not only can the installation and disassembly be quickly achieved, but also the installation and disassembly can be firmly fixed, and the troubles caused by the inspection and maintenance can be reduced.

[0016] 2. In the utility model, through the cooperation of the second spring and the damping rod, when the marine operation is carried out, the satellite communication terminal body can be effectively damped, the marine working environment with more wind and waves can be effectively coped with, and the influence of the wind and waves can be reduced. DRAWINGS

[0017] The drawings described herein are used to provide further understanding of the utility model and constitute a part of the application. The schematic embodiments of the utility model and the description thereof are used to explain the utility model, and do not constitute an improper limitation on the utility model. In the drawings:

[0018] Figure 1 It is a front view structural schematic diagram of the utility model;

[0019] Figure 2 It is a box cross-section structural schematic diagram of the utility model;

[0020] Figure 3 It is a sliding groove cross-section structural schematic diagram of the utility model;

[0021] Figure 4 It is a limiting block cross-section structural schematic diagram of the utility model;

[0022] Figure 5 It is a square frame cross-section structural schematic diagram of the utility model;

[0023] In the figure, the serial numbers are as follows: 1, fixed plate; 11, box body; 12, I-shaped block; 13, flexible pad; 14, maritime satellite communication terminal body; 15, square frame; 16, limiting block; 17, sliding groove; 18, rectangular block; 19, trapezoidal groove; 111, threaded rod; 112, knob; 113, vertical column; 114, cross groove; 115, limiting rod; 116, sliding plate; 117, first spring; 118, square hole; 2, second spring; 21, damping rod. DETAILED DESCRIPTION

[0024] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments of the present application.

[0025] Embodiment 1: The embodiment provides a maritime satellite communication terminal, which is described below with reference to Figures 1-5 , and specifically includes a fixed plate 1, the fixed plate 1 is fixedly provided with a box body 11, the box body 11 is slidably provided with an I-shaped block 12, the I-shaped block 12 is provided with a flexible pad 13, the flexible pad 13 is fixedly provided with a maritime satellite communication terminal body 14, the maritime satellite communication terminal body 14 is fixedly provided with a square frame 15 at the bottom, the I-shaped block 12 is fixedly provided with a limiting block 16, the I-shaped block 12 is provided with a sliding groove 17, the sliding groove 17 is slidably provided with a rectangular block 18, the rectangular block 18 is provided with a trapezoidal groove 19, the rectangular block 18 is rotatably provided with a threaded rod 111 at the front side, the threaded rod 111 is fixedly provided with a knob 112 at the other end, the I-shaped block 12 is slidably provided with a vertical column 113, the limiting block 16 is provided with a cross groove 114, the vertical column 113 is slidably connected with the cross groove 114 at the top, a pair of limiting rods 115 are slidably arranged in the cross groove 114, the pair of limiting rods 115 are fixedly provided with a sliding plate 116 at both sides, the sliding plate 116 is slidably connected with the cross groove 114, the sliding plate 116 is fixedly provided with a first spring 117 at one side, the first spring 117 is fixedly connected with the cross groove 114 at the other end, and the square frame 15 is provided with a square hole 118;

[0026] The square frame 15 penetrates the flexible pad 13, the square frame 15 is located at the center of the bottom of the maritime satellite communication terminal body 14, the limiting block 16 is attached to the inside of the square frame 15, the top of the limiting block 16 is arc-shaped at four edges, the I-shaped block 12 penetrates the box body 11, the pair of limiting rods 115 are symmetrically arranged, the limiting rods 115 are right-angled triangular at one end in the cross groove 114, the vertical column 113 is inclined from the center to both sides at the top, the vertical column 113 is inclined from the front side to the rear side at the bottom, the threaded rod 111 penetrates the sliding groove 17, the rectangular block 18 is attached to the inner wall of the sliding groove 17, the vertical column 113 penetrates the sliding groove 17, and the limiting rods 115 all penetrate the cross groove 114.

[0027] In the specific implementation process, as Figure 3 and Figure 4As shown, align the limiting block 16 with the square frame 15, insert the limiting block 16 into the square frame 15, and make the flexible pad 13 adhere to the surface of the I-shaped block 12. The flexible pad 13 protects the marine satellite communication terminal body 14 from colliding with the I-shaped block 12. The knob 112 drives the threaded rod 111 to rotate. The threaded rod 111 moves backward through the trapezoidal slot 19 on the rectangular block 18. The inclined surface on the trapezoidal slot 19 extrudes the inclined surface at the bottom of the stand column 113, driving the stand column 113 to move upward. The stand column 113 moves upward through the two inclined surfaces at the top to extrude the right triangle surface at the end of the limiting rod 115. The limiting rod 115 is pushed out of the cross slot 114 and inserted into the square hole 118. The limiting rod 115 drives the sliding plate 116 to move and extrude the first spring 117. The limiting rod 115 is inserted into the square hole 118 to limit the square frame 15. The installation of the marine satellite communication terminal body 14 is completed. When disassembly is required, the knob 112 is rotated in the opposite direction. The knob 112 drives the rectangular block 18 to move forward through the threaded rod 111. The extrusion of the trapezoidal slot 19 on the bottom of the stand column 113 is cancelled. The stand column 113 cancels the extrusion on the limiting rod 115 downward. The first spring 117 pushes the limiting rod 115 out of the square hole 118 through the sliding plate 116 and retracts into the cross slot 114, cancelling the limitation on the square frame 15. The marine satellite communication terminal body 14 can be removed. Through the cooperation of the square frame 15, the limiting block 16, the sliding slot 17, the rectangular block 18, the trapezoidal slot 19, the threaded rod 111, the knob 112, the stand column 113, the cross slot 114, the limiting rod 115, the sliding plate 116, the first spring 117 and the square hole 118, the marine satellite communication terminal body 14 can be quickly installed and disassembled, and firmly fixed during installation.

[0028] In example 1, there is also the problem of poor stability without the function of buffering and shock absorption. Therefore, based on example 1, this example further includes:

[0029] A plurality of second springs 2 are fixedly arranged in the box body 11. The other ends of the second springs 2 are fixedly connected with the bottom of the I-shaped block 12. A plurality of damping rods 21 are fixedly arranged in the box body 11. The piston rod ends of the damping rods 21 are fixedly connected with the bottom of the I-shaped block 12. The plurality of second springs 2 are arranged in a rectangular array. The damping rods 21 are respectively located at the centers of the second springs 2.

[0030] In the specific implementation process, for example, Figure 2As shown, the vibration makes the I-shaped block 12 swing up and down, the I-shaped block 12 compresses or stretches the second spring 2 at the bottom, the kinetic energy generated by the vibration is absorbed through the deformation of the second spring 2, and the damping rod 21 makes the deformed second spring 2 deform more slowly and smoothly, and through the cooperation of the second spring 2 and the damping rod 21, the satellite communication terminal body can be effectively damped during offshore operation, and the offshore working environment with more wind and waves can be effectively coped with.

[0031] Specifically, the working principle and operation method of the utility model are as follows:

[0032] Step one, when installing the marine satellite communication terminal body 14, align the limiting block 16 with the square frame 15, insert the limiting block 16 into the square frame 15, make the flexible pad 13 adhere to the surface of the I-shaped block 12, and the flexible pad 13 protects the marine satellite communication terminal body 14 so that it will not collide with the I-shaped block 12, rotate the knob 112, the knob 112 drives the threaded rod 111 to rotate, the threaded rod 111 moves backward through the trapezoidal groove 19 on the rectangular block 18, the inclined surface on the trapezoidal groove 19 extrudes the inclined surface at the bottom of the stand column 113, drives the stand column 113 to move upward, the stand column 113 extrudes the right triangle surface at the end of the limiting rod 115 through the two inclined surfaces at the top, pushes the limiting rod 115 to move outward from the cross groove 114 and inserts it into the square hole 118, the limiting rod 115 drives the sliding plate 116 to move and extrude the first spring 117, limits the square frame 15 by inserting the limiting rod 115 into the square hole 118, and completes the installation of the marine satellite communication terminal body 14, when disassembly is needed, rotate the knob 112 in the opposite direction, the knob 112 drives the rectangular block 18 to move forward through the threaded rod 111, cancels the extrusion of the trapezoidal groove 19 on the bottom of the stand column 113, the stand column 113 cancels the extrusion of the limiting rod 115 downward, the first spring 117 pushes the limiting rod 115 out of the square hole 118 through the sliding plate 116 and retracts it into the cross groove 114, cancels the limiting of the square frame 15, and then the marine satellite communication terminal body 14 can be removed;

[0033] Step two, when the impact of wind and waves causes vibration, the vibration makes the I-shaped block 12 swing up and down, the I-shaped block 12 compresses or stretches the second spring 2 at the bottom, the kinetic energy generated by the vibration is absorbed through the deformation of the second spring 2, and the damping rod 21 makes the deformed second spring 2 deform more slowly and smoothly;

[0034] The above is only a preferred specific embodiment of the utility model, but the protection scope of the utility model is not limited to this, any skilled person in the art can make equivalent replacement or change according to the technical scheme and the utility model concept of the utility model within the technical range disclosed by the utility model, which should be covered in the protection scope of the utility model.

Claims

1. A maritime satellite communication terminal, comprising a fixing plate (1), characterized in that: The fixing plate (1) is fixed with a box body (11), the box body (11) is slidably provided with an I-shaped block (12), the I-shaped block (12) is provided with a flexible pad (13), the flexible pad (13) is fixed with a maritime satellite communication terminal body (14), the bottom of the maritime satellite communication terminal body (14) is fixed with a square frame (15), the I-shaped block (12) is fixed with a limit block (16), a sliding groove (17) is provided in the I-shaped block (12), a rectangular block (18) is slidably provided in the sliding groove (17), a trapezoidal groove (19) is provided on the rectangular block (18), a threaded rod (111) is rotatably provided on the front side of the rectangular block (18), and the threaded rod (111) is rotatably provided on the front side of the rectangular block (18). 1) A knob (112) is fixedly provided at the other end, a column (113) is slidably provided on the I-shaped block (12), a cross slot (114) is provided in the limit block (16), the top of the column (113) is slidably connected to the cross slot (114), a pair of limit rods (115) are slidably provided in the cross slot (114), a slide plate (116) is fixed on both sides of the pair of limit rods (115), the slide plate (116) is slidably connected to the cross slot (114), a first spring (117) is fixed on one side of the slide plate (116), the other end of the first spring (117) is fixedly connected to the cross slot (114), and a pair of square holes (118) are provided in the square frame (15).

2. A maritime satellite communication terminal according to claim 1, characterized in that: A plurality of second springs (2) are fixedly provided in the box body (11), and the other ends of the second springs (2) are fixedly connected to the bottom of the I-shaped block (12). A plurality of damping rods (21) are fixedly provided in the box body (11), and the piston rod ends of the damping rods (21) are fixedly connected to the bottom of the I-shaped block (12).

3. A maritime satellite communication terminal according to claim 1, characterized in that: The square frame (15) passes through the flexible pad (13), the square frame (15) is located at the bottom center of the maritime satellite communication terminal body (14), the limit block (16) is fitted with the inside of the square frame (15), the top four sides of the limit block (16) are arc-shaped, and the I-shaped block 12 passes through the box body 11.

4. A maritime satellite communication terminal according to claim 1, characterized in that: A pair of the limiting rods (115) are symmetrically arranged, and one end of the limiting rod (115) in the cross slot (114) is a right triangle.

5. The maritime satellite communication terminal according to claim 1, characterized in that: The top of the column (113) is inclined from the center to both sides, and the bottom of the column (113) is inclined from the front side to the rear side.

6. A maritime satellite communication terminal according to claim 1, characterized in that: The threaded rod (111) passes through the slide groove (17), and the rectangular block (18) fits in contact with the inner wall of the slide groove (17).

7. The maritime satellite communication terminal according to claim 1, characterized in that: The upright column (113) passes through the slide groove (17), and the limiting rods (115) all pass through the cross groove (114).

8. A maritime satellite communication terminal according to claim 2, characterized in that: The plurality of second springs (2) are distributed in a rectangular row, and the damping rods (21) are respectively located at the center of the second springs (2).

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