Portable satellite communication station all-in-one machine

Abstract

The utility model discloses a portable satellite communication portable station integrated machine belongs to portable communication equipment field, including satellite station main part, the side surface fixedly connected with mounting seat of satellite station main part, the bottom detachably connected with bottom plate of mounting seat, the bottom of bottom plate is equipped with the mounting hole of side surface center, the inside of bottom plate is provided with the abutting component that carries out quick docking installation and stable of mounting seat, through the cooperation of above -mentioned each device, when installing satellite station main part, only need to insert mounting seat bottom end in mounting hole, and after aligning with annular chamber, two group bottom plate is straightened out, the docking ring is inserted into annular chamber at this moment, makes docking ring and mounting seat keep stable on bottom plate, through the self weight of satellite station main part and the docking ring to two group bottom plate generates the downward pressure, maintains satellite station main part barycenter stable while avoiding its generation displacement and the condition of separation.

Description

Technical Field

[0001] This utility model relates to the field of portable communication equipment technology, specifically a lightweight portable satellite communication station integrated machine. Background Technology

[0002] Satellite communication is communication between radio communication stations on Earth using satellites as relays. A satellite communication system consists of two parts: a satellite and an earth station. In addition, the characteristics of satellite communication are: communication can be carried out between any two points within the coverage area of ​​the satellite's radio waves; it is not easily affected by land disasters; it can be activated simply by setting up an earth station circuit; and it can be received from multiple locations simultaneously.

[0003] Upon investigation, a Chinese utility model patent discloses a lightweight portable satellite communication station integrated unit (publication number: CN220964883U). By loosening the bidirectional lead screw, the bidirectional lead screw, under the reset action of the torsion spring, drives the clamping block to insert into the positioning groove to fix the insertion rod. Through the above settings, the satellite communication integrated unit is more convenient to remove for installation and use, as well as to disassemble and load it onto a vehicle.

[0004] Although the aforementioned patent uses a positioning structure to fix the satellite communication station, the satellite communication equipment itself is large in size, and its irregular shape makes the positioning and calibration efficiency during assembly poor. Using only clips to fix its mounting column still results in an unstable center of gravity that is prone to tipping over, affecting the normal use of the integrated communication device.

[0005] Therefore, this utility model provides a lightweight portable satellite communication station integrated machine to solve the above problems. Utility Model Content

[0006] (a) Technical problems to be solved This invention provides a lightweight portable satellite communication station integrated device, which aims to solve the problems mentioned in the background art.

[0007] (II) Technical Solution To achieve the above objectives, this utility model provides the following technical solution: a lightweight portable satellite communication station, comprising a satellite station body, a mounting base fixedly connected to the side of the satellite station body, a base plate detachably connected to the bottom of the mounting base, an installation hole provided at the center of the side of the base plate, and an anti-locking component provided inside the base plate for quick docking and stable installation of the mounting base.

[0008] As a preferred technical solution of this application, the number of base plates is set to two sets, and the internal configuration of the two sets of base plates is exactly the same. The two sets of base plates are mirror images of each other on the left and right sides of the mounting base, and the two sets of base plates are connected by hinges.

[0009] As a preferred technical solution of this application, the clamping assembly includes an annular cavity, which is formed on the arc-shaped inner wall of the mounting hole. A mating ring is fixedly installed on the bottom outer wall of the mounting base. A push rod is slidably installed on the inner wall of the base plate. A spring is fixedly connected to the end of the push rod. A crossbar is fixedly connected to the side wall of the push rod. A stop block is fixedly installed on the lower surface of the crossbar. A locking block is slidably installed on the inner wall of the base plate. A trapezoidal block is fixedly installed on the upper surface of the locking block. A locking groove is formed on the upper surface of the mating ring. A protrusion is fixedly installed on the arc-shaped inner wall of the mounting hole. A groove is formed on the bottom arc-shaped outer wall of the mounting base.

[0010] As a preferred technical solution of this application, the inner diameter of the mounting hole is adapted to the outer diameter of the bottom end of the mounting base, and the outer diameter of the mating ring is the same as the inner diameter of the annular cavity, the thickness of the mating ring is less than the thickness of the annular cavity, and the mating ring is disposed inside the annular cavity.

[0011] As a preferred technical solution of this application, the push rods installed in the two sets of base plates are staggered in the horizontal direction, and a rectangular cavity adapted to the width of the crossbeam is opened on the inner wall of the base plate.

[0012] As a preferred technical solution of this application, the size of the card block is adapted to the trapezoidal block, and a sliding groove adapted to the card block is provided on the inner wall of the base plate. Protrusions are provided on both sides of the card block, and limiting grooves adapted to the protrusions are provided on the inner walls of both sides of the sliding groove.

[0013] As a preferred technical solution of this application, the protrusion is set as an arc-shaped block with an outer rubber sleeve, and the inner cavity size of the groove is adapted to the protrusion. The number of protrusions and grooves is set in multiple sets, and the protrusions and grooves correspond one-to-one.

[0014] (III) Beneficial Effects With the addition of a clamping assembly, during the installation of the satellite station body, it is only necessary to insert the bottom end of the mounting base into the mounting hole, align the docking ring with the annular cavity, and then flatten the two sets of base plates. At this time, the docking ring is inserted into the annular cavity. Simultaneously, due to the pushing force of the side walls of the two sets of base plates, the push rod drives the crossbeam and the abutment block to generate a downward pushing force on the locking block, causing the locking block to enter the locking groove. This keeps the docking ring and the mounting base stable on the base plate. The downward pressure generated by the weight of the satellite station body itself and the docking ring on the two sets of base plates maintains the stability of the satellite station body's center of gravity while preventing it from shifting or detaching. Attached Figure Description

[0015] Figure 1 This is a schematic diagram of the main structure of a lightweight portable satellite communication station. Figure 2 A partial three-dimensional structural diagram of a lightweight portable satellite communication station; Figure 3 A schematic diagram of the three-dimensional structure of the base plate of a lightweight portable satellite communication station. Figure 4 A schematic diagram of the cross-sectional structure of the base plate of a lightweight portable satellite communication station. Figure 5 A schematic diagram of the push rod and crossbeam structure of a lightweight portable satellite communication station; Figure 6 This is a schematic diagram of the three-dimensional structure of the cross frame and card blocks of a lightweight portable satellite communication station.

[0016] In the picture: 1. Satellite station main body; 2. Mounting base; 3. Base plate; 4. Mounting hole; 5. Annular cavity; 6. Docking ring; 7. Push rod; 8. Spring; 9. Horizontal frame; 10. Abutment block; 11. Locking block; 12. Trapezoidal block; 13. Locking groove; 14. Protrusion; 15. Groove. Detailed Implementation

[0017] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0018] This utility model provides a lightweight, portable satellite communication station integrated device, such as... Figure 1-6 As shown, the satellite station includes a main body 1, a mounting base 2 is fixedly connected to the side of the main body 1, a base plate 3 is detachably connected to the bottom of the mounting base 2, a mounting hole 4 is provided at the center of the side of the base plate 3, and a fastening component for quick docking and stable installation of the mounting base 2 is provided inside the base plate 3.

[0019] In actual operation, an adjustable height and angle control module is provided between the satellite station body 1 and the mounting base 2, and a corresponding power supply module is provided inside the mounting base 2 to facilitate the normal use of the satellite communication integrated machine. At the same time, corresponding support feet are provided at the top corner of the base plate 3, and through holes are provided on the inner wall of the base plate 3 and inside the support feet, so that users can fix the base plate 3 to the ground with pins or rods. This allows for easy fixation anytime and anywhere during field use, and also allows for leveling of the base plate 3 to ensure the normal and safe use of the satellite station body 1.

[0020] There are two sets of base plates 3, and the internal configuration of the two sets of base plates 3 is exactly the same. The two sets of base plates 3 are mirror images of each other on the left and right sides of the mounting base 2, and the two sets of base plates 3 are connected by hinges.

[0021] In actual operation, handles are provided on the side of the two sets of base plates 3 that are far apart from each other, so that the base plates 3 can be folded and stored after being disassembled, and can be picked up and carried by the handles, improving the overall practicality and convenience of the device. The hinge is located at the bottom of the base plates 3, so that when the two sets of base plates 3 are unfolded, the pressure generated by the self-weight of the mounting base 2 and the satellite station body 1 on the base plates 3 can also ensure the stability of the base plates 3 in the unfolded state to a certain extent.

[0022] The clamping assembly includes an annular cavity 5, which is formed on the arc-shaped inner wall of the mounting hole 4. A mating ring 6 is fixedly installed on the bottom outer wall of the mounting base 2. A push rod 7 is slidably installed on the inner wall of the base plate 3. A spring 8 is fixedly connected to the end of the push rod 7. A crossbar 9 is also fixedly connected to the side wall of the push rod 7. A stop block 10 is fixedly installed on the lower surface of the crossbar 9. A locking block 11 is slidably installed on the inner wall of the base plate 3. A trapezoidal block 12 is fixedly installed on the upper surface of the locking block 11. A locking groove 13 is formed on the upper surface of the mating ring 6. A protrusion 14 is fixedly installed on the arc-shaped inner wall of the mounting hole 4. A groove 15 is formed on the bottom arc-shaped outer wall of the mounting base 2.

[0023] In actual operation, both the mounting hole 4 and the annular cavity 5 are semi-circular. Therefore, only after the two sets of base plates 3 are spliced ​​can a complete mounting hole 4 and annular cavity 5 be formed, which are respectively adapted to the outer wall of the bottom end of the mounting base 2 and the outer wall of the docking ring 6. At the same time, there are two sets of push rods 7, which are mirror images of each other at both ends of the cross frame 9. This makes the cross frame 9 more stable and balanced during the sliding process under force. In addition, both the abutment block 10 and the trapezoidal block 12 are trapezoidal in shape, and the abutment block 10 and the trapezoidal block 12 are mirror images of each other and centrally symmetrical, so that their inclined surfaces are close to each other. When the cross frame 9 moves in the horizontal direction, the inclined surface of the abutment block 10 will contact the trapezoidal block 12 to generate a squeezing force.

[0024] The inner diameter of the mounting hole 4 is matched with the outer diameter of the bottom end of the mounting base 2, and the outer diameter of the mating ring 6 is the same as the inner diameter of the annular cavity 5. The thickness of the mating ring 6 is less than the thickness of the annular cavity 5, and the mating ring 6 is located inside the annular cavity 5.

[0025] In actual operation, during the docking installation, it is only necessary to align the mounting base 2 with the mounting hole 4 opened on the side of the base plate 3. First, the two sets of hinged base plates 3 need to be unfolded into an inverted V shape. Then, the mounting base 2 is inserted into the center of the mounting hole 4. At this time, the docking ring 6 is in the annular cavity 5 on the side of the two sets of mounting holes 4. Since the docking ring 6 is relatively thin, there will be no movement interference or collision when the two sets of base plates 3 are rotated to a straight position after alignment. Finally, the arc-shaped outer surface of the docking ring 6 is completely in contact with the inner wall of the annular cavity 5. The bottom surface of the docking ring 6 is also in contact with the annular cavity 5 under the influence of the weight of the mounting base 2 and the satellite station body 1. At the same time, the upper surface of the docking ring 6 has a certain distance from the top inner wall of the annular cavity 5.

[0026] The push rods 7 installed in the two sets of base plates 3 are staggered in the horizontal direction, and the inner wall of the base plate 3 is provided with a rectangular cavity that matches the width of the cross frame 9.

[0027] In actual operation, when the two sets of base plates 3 rotate to a flat position, the side walls of the base plates 3 will exert a squeezing force on the end of the push rod 7. The push rods 7 in the two sets of base plates 3 that are staggered will not affect each other. When squeezed by the side walls of the base plates 3, they will move towards the spring 8. The rectangular cavity setting allows the crossbar 9 to have a range of movement in the horizontal direction, so that it will not move too far away from the mounting hole 4, nor will it fall off from the interior of the base plate 3.

[0028] The size of the locking block 11 is adapted to the trapezoidal block 12, and a sliding groove adapted to the locking block 11 is provided on the inner wall of the base plate 3. The locking block 11 has protrusions on both sides, and a limiting groove adapted to the protrusions is provided on the inner wall of both sides of the sliding groove.

[0029] During actual operation, the locking block 11 is affected by the protrusion on its side and the limiting groove, so that it can only slide in the vertical direction and will not detach. The cooperation between the abutment block 10 and the trapezoidal block 12 can limit the height of the locking block 11 in the vertical direction, so that it will not move in this position. Finally, the bottom of the locking block 11 is inserted into the locking groove 13 to ensure the stability of the docking ring 6 in the annular cavity 5, thereby ensuring the stability of the mounting base 2 and the satellite station body 1 after installation.

[0030] The protrusion 14 is set as an arc-shaped block with an outer rubber sleeve, and the inner cavity size of the groove 15 is adapted to the protrusion 14. There are multiple sets of both the protrusion 14 and the groove 15, and the protrusion 14 and the groove 15 correspond one-to-one.

[0031] In actual operation, the rubber sleeve wrapped around the outside of the protrusion 14 gives the surface of the protrusion 14 a certain deformation capability, so that the protrusion 14 can be embedded in the groove 15 when the base plate 3 rotates. At the same time, the protrusion 14 is actually on the inner wall of the mounting hole 4 near the top, so that multiple sets of protrusions 14 and grooves 15 can further increase the contact area between the base plate 3 and the mounting base 2, so as to ensure the stability of the mounting base 2 and the satellite station body 1 during splicing and installation.

[0032] Working principle: First, open the two sets of base plates 3 to unfold them into an inverted V shape. Then, align the center of the mounting base 2 with the mounting hole 4 and insert it. At this time, the docking ring 6 is aligned with the mounting hole 4 and the annular cavity 5 on the side of the two sets of base plates 3. Then, the operator rotates the two sets of base plates 3 and gradually rotates them to a horizontal position. The side wall of the base plate 3 generates a squeezing and pushing force on the end of the push rod 7, so that the cross frame 9 slides away from the mounting base 2. With the cooperation of the inclined surface of the abutment block 10 and the trapezoidal block 12, a vertical pressure is generated on the locking block 11, so that the locking block 11 is inserted into the locking groove 13 opened on the upper surface of the docking ring 6, so that the docking ring 6 can remain stable in the annular cavity 5, thereby ensuring the stability of the mounting base 2 and the satellite station body 1 after installation.

[0033] The above description is only a preferred embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any equivalent substitutions or changes made by those skilled in the art within the technical scope disclosed in the present utility model, based on the technical solution and the inventive concept of the present utility model, should be included within the protection scope of the present utility model.

Claims

1. A lightweight portable satellite communication station, comprising a satellite station body (1), characterized in that: The satellite station body (1) is fixedly connected to a mounting base (2) on its side. The bottom of the mounting base (2) is detachably connected to a base plate (3). The base plate (3) has a mounting hole (4) at the center of its side. The base plate (3) is equipped with a fastening component for quick docking and stable installation of the mounting base (2).

2. The portable satellite communication station all-in-one machine according to claim 1, characterized in that: The number of base plates (3) is set in two sets, and the interior of the two sets of base plates (3) is exactly the same. The two sets of base plates (3) are mirror images of each other on the left and right sides of the mounting base (2), and the two sets of base plates (3) are connected by hinges.

3. The portable satellite communication station integrated device according to claim 2, characterized in that: The clamping assembly includes an annular cavity (5), which is opened on the arc-shaped inner wall of the mounting hole (4). A docking ring (6) is fixedly installed on the bottom outer wall of the mounting base (2). A push rod (7) is slidably installed on the inner wall of the base plate (3). A spring (8) is fixedly connected to the end of the push rod (7). A crossbar (9) is also fixedly connected to the side wall of the push rod (7). A stop block (10) is fixedly installed on the lower surface of the crossbar (9). A locking block (11) is slidably installed on the inner wall of the base plate (3). A trapezoidal block (12) is fixedly installed on the upper surface of the locking block (11). A locking groove (13) is opened on the upper surface of the docking ring (6). A protrusion (14) is fixedly installed on the arc-shaped inner wall of the mounting hole (4). A groove (15) is opened on the bottom arc-shaped outer wall of the mounting base (2).

4. The lightweight satellite communication portable station integrated machine according to claim 3, characterized in that: The inner diameter of the mounting hole (4) is adapted to the outer diameter of the bottom end of the mounting base (2), and the outer diameter of the mating ring (6) is the same as the inner diameter of the annular cavity (5). The thickness of the mating ring (6) is less than the thickness of the annular cavity (5), and the mating ring (6) is disposed inside the annular cavity (5).

5. A lightweight satellite communication portable station integrated machine according to claim 3, characterized in that: The push rods (7) installed in the two sets of base plates (3) are staggered in the horizontal direction, and a rectangular cavity adapted to the width of the cross frame (9) is opened on the inner wall of the base plate (3).

6. A lightweight satellite communication portable station integrated machine according to claim 3, characterized in that: The size of the card block (11) is adapted to the trapezoidal block (12), and a sliding groove adapted to the card block (11) is provided on the inner wall of the base plate (3). The card block (11) has protrusions on both sides, and a limiting groove adapted to the protrusions is provided on the inner wall of both sides of the sliding groove.

7. A lightweight satellite communication portable station integrated machine according to claim 3, characterized in that: The protrusion (14) is set as an arc-shaped block with an outer rubber sleeve, and the inner cavity size of the groove (15) is adapted to the protrusion (14). The number of protrusions (14) and grooves (15) are set in multiple sets, and the protrusions (14) and grooves (15) correspond one-to-one.

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