A low earth orbit constellation phased array antenna control device

Abstract

The utility model relates to low orbit satellite phased array antenna control technical field, concretely relates to a low orbit star chain phased array antenna control device including control box, the front surface threaded connection of control box has fixed peg, the surface threaded connection of fixed peg has the overhauling board, the middle part fixed mounting of control box top surface has the rotary disc, the top fixed mounting of rotary disc has the connecting frame, the surface mounting of connecting frame has signal receiver, the both sides threaded connection of control box has the threaded peg, the surface threaded connection of threaded peg has cooling assembly, the both sides of control box are provided with stability component. Through the setting of cooling assembly and control box, when the use time of control box is too long, the personnel can connect the power of semiconductor refrigerator and cooling fan, make the semiconductor refrigerator deliver the cold air to the inside of energy storage box, and the cooling fan carries the cold air to the inside of control box, make the hot air in the inside of control box and the outside air carry out air conversion, and improve the heat dissipation of control box.

Description

Technical Field

[0001] This utility model relates to the field of low-orbit satellite phased array antenna control technology, specifically to a low-orbit starlink phased array antenna control device. Background Technology

[0002] In recent years, with the rapid development of low-Earth orbit (LEO) communication constellations and the growing demand for flexible application services, beam control of phased array antennas based on LEO satellites has become one of the research hotspots in the field of satellite communications.

[0003] Although an existing low-orbit starlink phased array antenna control device has the characteristics of convenient correction and accurate calculation.

[0004] However, this low-orbit starlink phased array antenna control device has the following shortcomings: during the use of the antenna control device by personnel, it is not easy to further dissipate the hot air inside the control device, which causes the hot air to affect the internal computing efficiency of the control device, and it is also not easy for personnel to position and install the control device. Utility Model Content

[0005] To address the aforementioned shortcomings of existing technologies, this utility model provides a low-orbit starlink phased array antenna control device, which effectively solves the problems of existing technologies where it is difficult to further dissipate the hot air inside the control device during personnel use, resulting in the hot air affecting the internal computing efficiency of the control device, and also making it difficult for personnel to position and install the control device.

[0006] To achieve the above objectives, this utility model provides the following technical solution:

[0007] This utility model provides a low-orbit starlink phased array antenna control device, including a control box. A fixing bolt is threadedly connected to the front of the control box, and a maintenance plate is threadedly connected to the surface of the fixing bolt. A rotating disk is fixedly installed in the middle of the top surface of the control box, and a connecting frame is fixedly installed on the top of the rotating disk. A signal receiver is installed on the surface of the connecting frame. Threaded bolts are threadedly connected to both sides of the control box, and cooling components are threadedly connected to the surface of the threaded bolts. Stabilizing components are provided on both sides of the control box.

[0008] Preferably, the cooling assembly includes an energy storage box fixedly installed on one side of the threaded bolt surface, with semiconductor coolers embedded on both sides of the energy storage box, and cooling fans embedded on both sides of the front of the energy storage box.

[0009] Preferably, the cooling fan has a battery block inside for providing power, and the other side of the cooling fan has an anti-oxidation coating.

[0010] Preferably, the stabilizing component includes connecting pieces threaded to both sides of the outer surface of the control box, with a threaded cone threaded through the center of the top surface of the connecting piece, and a conical head fixedly connected to the bottom of the threaded cone.

[0011] Preferably, the inspection plate has an observation window on its front side, and a transparent plate is embedded in the surface of the observation window.

[0012] Preferably, the rotating disk is equipped with an electric device inside, and the top of the threaded cone is provided with a circular block.

[0013] Preferably, the heat dissipation end of the semiconductor cooler is located outside the energy storage box, and the cooling end of the semiconductor cooler is located inside the energy storage box.

[0014] The technical solution provided by this utility model has the following advantages compared with the known prior art:

[0015] 1. By setting up the cooling components and control box, when the control box has been used for a long time, the personnel can turn on the power of the semiconductor cooler and the cooling fan, so that the semiconductor cooler delivers cold air to the inside of the energy storage box, and then the cooling fan delivers the cold air to the inside of the control box, so that the hot air inside the control box is exchanged with the outside air, thereby improving the heat dissipation of the control box.

[0016] 2. Through the coordinated use of the stabilizing components and the control box, when personnel install the control box, they can place the control box in the designated working position and turn the threaded cone to move the conical head downwards. Then, the threaded cone will drive the conical head into the interior of the designated working position, thereby improving the stability of the control box. Attached Figure Description

[0017] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0018] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0019] Figure 2 This utility model Figure 1 Enlarged structural diagram at point A in the middle;

[0020] Figure 3 This is a schematic diagram of the cooling component structure of this utility model;

[0021] Figure 4 This is a schematic diagram of the rotating disk structure of this utility model.

[0022] Reference numerals: 1. Control box; 2. Fixing bolt; 3. Inspection plate; 4. Rotating disk; 5. Connecting frame; 6. Signal receiver; 7. Threaded bolt; 8. Cooling assembly; 81. Energy storage box; 82. Semiconductor cooler; 83. Cooling fan; 9. Stabilizing assembly; 91. Connecting piece; 92. Threaded taper; 93. Conical head. Detailed Implementation

[0023] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some, not all, of the embodiments of this utility model. All other embodiments obtained by those skilled in the art based on the embodiments of this utility model without creative effort are within the scope of protection of this utility model.

[0024] The present invention will be further described below with reference to the embodiments.

[0025] Example: Refer to Figures 1 to 4 A low-orbit starlink phased array antenna control device includes a control box 1, a fixing bolt 2 is threadedly connected to the front of the control box 1, a maintenance plate 3 is threadedly connected to the surface of the fixing bolt 2, a rotating disk 4 is fixedly installed in the middle of the top surface of the control box 1, a connecting frame 5 is fixedly installed on the top of the rotating disk 4, and a signal receiver 6 is installed on the surface of the connecting frame 5.

[0026] When personnel use the low-orbit starlink phased array antenna control device, when installing the control box 1, they can place the control box 1 in the designated working position and turn the threaded cone 92 to move the cone head 93 downwards, fixing the control box 1 to the ground. Then, the personnel can turn on the power of the rotating disk 4, causing the rotating disk 4 to drive the signal receiver 6 to rotate slowly to receive signals. If the control box 1 has been used for a long time, the personnel can directly turn on the power of the semiconductor cooler 82, causing the semiconductor cooler 82 to deliver cold air to the inside of the energy storage box 81. Then, the personnel can turn on the power of the cooling fan 83, causing the airflow to carry cold air to the inside of the control box 1, thus cooling the hot air inside the control box 1. Finally, if the personnel need to inspect the control box 1, they can turn on the fixing bolt 2 to open the inspection plate 3, thereby facilitating the maintenance personnel to repair the internal parts of the control box 1.

[0027] Reference Figures 1 to 4Both sides of the control box 1 are threaded with threaded bolts 7, and the surface of the threaded bolts 7 is threaded with a cooling assembly 8. The cooling assembly 8 includes an energy storage box 81 fixedly installed on one side of the surface of the threaded bolts 7. Both sides of the energy storage box 81 are embedded with semiconductor coolers 82. Both sides of the front of the energy storage box 81 are embedded with cooling fans 83. The inside of the cooling fan 83 is a battery block for providing power. The other side of the cooling fan 83 is provided with an anti-oxidation coating. The heat dissipation end of the semiconductor cooler 82 is located outside the energy storage box 81, and the cooling end of the semiconductor cooler 82 is located inside the energy storage box 81.

[0028] With the cooling assembly 8 and the control box 1 in place, when the control box 1 has been used for a long time, the personnel can turn on the power to the semiconductor cooler 82 and the cooling fan 83, so that the semiconductor cooler 82 delivers cold air to the inside of the energy storage box 81, and then the cooling fan 83 delivers the cold air to the inside of the control box 1 with the air force, so that the hot air inside the control box 1 is converted with the outside air, thereby improving the heat dissipation of the control box 1.

[0029] Reference Figures 1 to 4 Both sides of the control box 1 are provided with stabilizing components 9. The stabilizing components 9 include connecting pieces 91 that are threaded to both sides of the outer surface of the control box 1. A threaded cone 92 is threaded through the middle of the top surface of the connecting piece 91, and a conical head 93 is fixedly connected to the bottom of the threaded cone 92.

[0030] By using the stabilizing component 9 and the control box 1 together, when personnel install the control box 1, they can place the control box 1 in the designated working position and turn the threaded cone 92 to drive the conical head 93 downward. Then the threaded cone 92 drives the conical head 93 to penetrate into the interior of the designated working position, thereby improving the stability of the control box 1.

[0031] Reference Figures 1 to 4 An observation window is provided on the front of the inspection plate 3, and a transparent plate is embedded in the surface of the observation window;

[0032] The observation window and transparent panel facilitate personnel to observe the internal situation of control box 1;

[0033] Reference Figures 1 to 4 The rotating disk 4 is equipped with an electric device, and the top of the threaded cone 92 is equipped with a circular block;

[0034] The circular block design facilitates the rotation of the threaded taper 92.

[0035] Working principle: When personnel use the low-orbit starlink phased array antenna control device, when installing the control box 1, they can place the control box 1 in the designated working position and turn the threaded cone 92 to move the cone head 93 downwards, fixing the control box 1 to the ground. Then, the personnel can turn on the power to the rotating disk 4, causing the rotating disk 4 to slowly rotate the signal receiver 6 to receive signals. If the control box 1 has been used for a long time, the personnel can directly turn on the power to the semiconductor cooler 82, causing the semiconductor cooler 82 to deliver cold air to the inside of the energy storage box 81. Then, the power to the cooling fan 83 is turned on, causing the airflow to carry cold air to the inside of the control box 1, thus cooling the hot air inside the control box 1. Finally, if personnel need to inspect the control box 1, they can turn on the fixing bolt 2 to open the inspection plate 3, thereby facilitating the maintenance of the internal parts of the control box 1.

[0036] The above embodiments are only used to illustrate the technical solutions of this utility model, and are not intended to limit it. Although this utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some of the technical features. Such modifications or substitutions will not cause the essence of the corresponding technical solutions to deviate from the protection scope of the technical solutions of the embodiments of this utility model.

Claims

1. A low-orbit starlink phased array antenna control device, comprising a control box (1), characterized in that: The control box (1) has a fixing bolt (2) threaded on its front side, and a maintenance plate (3) threaded on the surface of the fixing bolt (2). A rotating disk (4) is fixedly installed in the middle of the top surface of the control box (1). A connecting frame (5) is fixedly installed on the top of the rotating disk (4). A signal receiver (6) is installed on the surface of the connecting frame (5). Threaded bolts (7) are threaded on both sides of the control box (1). A cooling component (8) is threaded on the surface of the threaded bolt (7). Stabilizing components (9) are provided on both sides of the control box (1).

2. The low-orbit starlink phased array antenna control device according to claim 1, characterized in that, The cooling assembly (8) includes an energy storage box (81) fixedly installed on one side of the surface of the threaded bolt (7). Semiconductor coolers (82) are embedded on both sides of the energy storage box (81), and heat dissipation fans (83) are embedded on both sides of the front of the energy storage box (81).

3. The low-orbit starlink phased array antenna control device according to claim 2, characterized in that, The cooling fan (83) has a battery block inside for providing power, and an anti-oxidation coating is provided on the other side of the cooling fan (83).

4. The low-orbit starlink phased array antenna control device according to claim 3, characterized in that, The stabilizing component (9) includes connecting pieces (91) threaded to both sides of the outer surface of the control box (1). A threaded cone (92) is threaded through the middle of the top surface of the connecting piece (91), and a conical head (93) is fixedly connected to the bottom of the threaded cone (92).

5. A low-orbit starlink phased array antenna control device according to claim 4, characterized in that, The inspection plate (3) has an observation window on its front side, and a transparent plate is embedded in the surface of the observation window.

6. A low-orbit starlink phased array antenna control device according to claim 5, characterized in that, The rotating disk (4) is equipped with an electric device inside, and the top of the threaded cone (92) is provided with a circular block.

7. A low-orbit starlink phased array antenna control device according to claim 6, characterized in that, The heat dissipation end of the semiconductor cooler (82) is located outside the energy storage box (81), and the cooling end of the semiconductor cooler (82) is located inside the energy storage box (81).

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