Passive docking device with antenna module capable of being unlocked
By adopting multiple limit and support structures in the docking device of the space antenna module, combined with the cooperation of spring and metal ball, the problems of unstable docking and cumbersome installation are solved, and the stability, accuracy and maintenance efficiency of docking are improved.
Patent Information
- Application Number
- CN202510515559.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-04-23
- Publication Date
- 2025-06-13
AI Technical Summary
The existing space antenna module docking device is difficult to effectively limit the position of each component in a complex space environment, resulting in unstable docking, affecting antenna performance, and the installation and disassembly process is cumbersome, making it difficult to adapt to the needs of different spacecraft missions.
An antenna module unlocks the passive docking device, adopting multiple limit and support structures, such as limit rings, limit rings, limit blocks and extrusion blocks of the inner wall of the barrel, combined with the cooperation of springs and metal balls, the precise positioning and stable connection of the docking components are achieved.
It effectively reduces shaking and offset during docking, improves the stability and accuracy of docking, simplifies the installation and disassembly process, improves maintenance efficiency, and enhances the adaptability and reliability of the device in complex environments.
Smart Images

Figure CN120149786A_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the technical field of space docking of spacecrafts, and specifically to an unlockable passive docking device for an antenna module. Background Art
[0002] In the era of booming space technology today, as a key device for spacecrafts to achieve functions such as communication, remote sensing, and navigation, the performance and reliability of space antennas are crucial. The docking technology of space antenna modules directly affects the installation, debugging, and subsequent stable operation of antennas. However, there are many problems with existing space antenna module docking devices, which seriously restrict the smooth progress of space missions.
[0003] Traditional docking devices are difficult to effectively restrict the positions of various components in a complex space environment. Micro-meteorite impacts in the space environment, vibrations generated by spacecraft attitude adjustments, etc. may all cause the docking components to shake and shift. This will not only affect the accuracy of antenna module docking, but may also cause loose connections, thereby interfering with signal transmission, reducing antenna performance, and even making the entire communication, remote sensing, etc. systems unable to work properly.
[0004] The installation and disassembly processes of existing docking devices are often cumbersome. In space operations, each operation requires a large amount of time and effort. The complex installation process increases the operation difficulty and workload of astronauts and prolongs the execution time of space missions. Moreover, when the antenna module needs to be maintained or replaced, difficult disassembly operations may damage the equipment, further increasing costs and risks.
[0005] The space environment has characteristics such as high vacuum, strong radiation, and extreme temperature changes. Existing docking devices are difficult to adapt to these harsh conditions. When the temperature changes violently, the materials of the docking components may expand and contract thermally, resulting in a decrease in connection accuracy; strong radiation may also affect the performance of electronic components in the docking device and reduce its reliability. In addition, under different spacecraft mission requirements, the versatility and flexibility of docking devices are insufficient and cannot meet diverse docking requirements. Summary of the Invention
[0006] The purpose of the present invention is to provide an unlockable passive docking device for an antenna module to solve the problems raised in the above background art.
[0007] The technical solution of the present invention is: an antenna module unlockable passive docking device, including a housing, wherein a cylinder is provided on the inner wall of the housing, two symmetrically arranged straight slots are provided on the surface of the cylinder, two symmetrically arranged circular holes are provided on the surface of the cylinder, a limiting ring is connected to the surface of the cylinder by a fixing rod, a circular block is fixedly connected to the upper end of the cylinder, a first fixing hole communicating with the surface of the circular block is provided at the upper end of the circular block, a first fixing member is provided at the upper end of the circular block, the surface of the first fixing member matches the inner wall of the first fixing hole, a through hole is provided at the upper end of the circular block, a cylinder is provided on the inner wall of the through hole, a second fixing rod hole communicating with the surface of the cylinder is provided at the upper end of the cylinder, a second fixing member is provided at the upper end of the cylinder, the surface of the second fixing member matches the inner wall of the second fixing rod hole, a connecting component is fixedly connected to the lower end of the cylinder, and a disk is fixedly connected to the lower end of the connecting component.
[0008] Preferably, a support column is fixedly connected to the inner wall of the housing, a first spring is fixedly connected to the surface of the support column, and the other end of the first spring is fixedly connected to a pressing block.
[0009] Preferably, a limiting block is fixedly connected to the inner wall of the cylinder, the surface of the limiting block abuts against the surface of the pressing block, and the upper end of the pressing block abuts against the lower end of the disk.
[0010] Preferably, there are two symmetrically arranged metal balls in the housing, and the metal balls match the circular holes.
[0011] Preferably, a limiting ring is provided on the inner wall of the housing, a second spring is fixedly connected to the upper end of the limiting ring, and the upper end of the second spring is fixedly connected to the inner wall of the housing.
[0012] Preferably, a fixing groove is provided on the surface of the housing, a fixing circular ring plate is provided at the upper end of the housing, and the fixing circular ring plate matches the fixing groove.
[0013] Preferably, the limiting ring is located above the limiting ring, and the lower end of the limiting ring abuts against the upper end of the limiting ring.
[0014] Preferably, a docking head is slidably connected to the inner walls of the first fixing hole and the second fixing rod hole, and two symmetrically arranged third limiting holes are provided on the surface of the docking head.
[0015] The present invention provides an antenna module unlockable passive docking device through improvement. Compared with the prior art, it has the following improvements and advantages:
[0016] First: In the present invention, a plurality of limiting and supporting structures are provided in the device. For example, the limiting ring and the limiting circular ring cooperate with each other and abut against each other. The limiting block on the inner wall of the barrel abuts against the extrusion block, and the upper end of the extrusion block abuts against the lower end of the disc. These structures can effectively limit the positions of various components during the docking process, reduce shaking and offset, make the docking more stable, ensure the stability of the space antenna module during docking, and ensure the normal operation of functions such as signal transmission.
[0017] Second: In the present invention, the fixing groove opened on the surface of the outer shell matches the fixing circular ring plate. This design facilitates the overall installation and fixation of the device. At the same time, the first fixing hole and the second fixing rod hole respectively match the first fixing member and the second fixing member, and the inner walls are all slidably connected to the docking head. When docking or disassembling is required, the operation is simple and convenient, improving the installation and maintenance efficiency of the space antenna module. Brief Description of the Drawings
[0018] The present invention will be further explained below in conjunction with the drawings and embodiments:
[0019] Figure 1 is the front view structural schematic diagram of the present invention;
[0020] Figure 2 is the sectional view structural schematic diagram of the present invention;
[0021] Figure 3 is the three-dimensional view structural schematic diagram of the present invention;
[0022] Figure 4 is the internal view structural schematic diagram of the present invention;
[0023] Figure 5 is the internal view structural schematic diagram of the present invention;
[0024] Figure 6 is the sectional view structural schematic diagram of the present invention.
[0025] Explanation of the Reference Numerals in the Drawings:
[0026] 1. Outer shell; 2. Barrel; 3. Straight slot; 4. Round hole; 5. Limiting ring; 6. Circular block; 7. First fixing hole; 8. First fixing member; 9. Through hole; 10. Cylinder; 11. Second fixing rod hole; 12. Second fixing member; 13. Connection component; 14. Disc; 15. Support column; 16. First spring; 17. Extrusion block; 18. Metal ball; 19. Limiting circular ring; 20. Second spring; 21. Fixing groove; 22. Fixing circular ring plate; 23. Docking head; 24. Third limiting hole. Detailed Embodiment
[0027] The present invention will be described in detail below. The technical solutions in the embodiments of the present invention are clearly and completely described. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
[0028] The present invention provides an unlockable passive docking device for an antenna module through improvement. The technical solution of the present invention is as follows:
[0029] As Figure 1 - Figure 6 shown, an unlockable passive docking device for an antenna module includes a housing 1. An inner wall of the housing 1 is provided with a barrel 2. Two symmetrically arranged straight slots 3 are formed on a surface of the barrel 2. Two symmetrically arranged circular holes 4 are formed on the surface of the barrel 2. A limiting ring 5 is fixedly connected to the surface of the barrel 2 by a fixing rod. An upper end of the barrel 2 is fixedly connected with a circular block 6. A first fixing hole 7 communicating with a surface of the circular block 6 is formed in an upper end of the circular block 6. A first fixing member 8 is arranged at the upper end of the circular block 6. A surface of the first fixing member 8 matches an inner wall of the first fixing hole 7. A through hole 9 is formed in the upper end of the circular block 6. A cylinder 10 is arranged on an inner wall of the through hole 9. A second fixing rod hole 11 communicating with a surface of the cylinder 10 is formed in an upper end of the cylinder 10. A second fixing member 12 is arranged at the upper end of the cylinder 10. A surface of the second fixing member 12 matches an inner wall of the second fixing rod hole 11. A lower end of the cylinder 10 is fixedly connected with a connecting component 13. A lower end of the connecting component 13 is fixedly connected with a disc 14.
[0030] Furthermore, a support column 15 is fixedly connected to the inner wall of the housing 1. A first spring 16 is fixedly connected to a surface of the support column 15. The other end of the first spring 16 is fixedly connected with a pressing block 17. The first spring 16 and the pressing block 17 constitute a buffer structure. During the docking process, if there is an external impact or a slight deviation in the position of the docking component, the first spring 16 can absorb part of the impact force through its own elastic deformation. The pressing block 17 can flexibly adjust its position under the action of the first spring 16 to provide stable support for the disc 14, avoiding damage to the disc 14 due to external impact, improving the adaptability and reliability of the docking device in a complex environment, and ensuring the smooth progress of the docking process.
[0031] Furthermore, a limiting block is fixedly connected to the inner wall of the barrel 2. The limiting block abuts against the surface of the extrusion block 17, and the upper end of the extrusion block 17 abuts against the lower end of the disc 14. The limiting block restricts the movement range of the extrusion block 17, so that when the extrusion block 17 provides support for the disc 14, excessive deviation or shaking will not occur. At the same time, the extrusion block 17 is in close contact with the disc 14, ensuring uniform force on the disc 14, further enhancing the stability of the docking structure, helping to maintain the relative position accuracy of each component during the docking process, improving the docking accuracy, and thus ensuring the stable operation of functions such as signal transmission after the space antenna module is docked.
[0032] Furthermore, there are two symmetrically arranged metal balls 18 in the outer shell 1. The metal balls 18 match the round holes 4. The cooperation between the metal balls 18 and the round holes 4 can play a role in positioning and locking. When the docking is completed, the metal balls 18 are embedded in the round holes 4, which can prevent relative rotation or displacement between the barrel 2 and the outer shell 1, making the connection of the entire docking device more firm, enhancing the stability and reliability of the docking structure, ensuring that the docking device can still maintain a good docking state under the complex external forces in the space environment, and guaranteeing the normal operation of the space antenna module.
[0033] Furthermore, a limiting ring 19 is arranged on the inner wall of the outer shell 1. The upper end of the limiting ring 19 is fixedly connected with a second spring 20. The upper end of the second spring 20 is fixedly connected with the inner wall of the outer shell 1. The second spring 20 and the limiting ring 19 work together to further enhance the buffering and positioning ability of the device. The second spring 20 can provide an upward elastic force for the limiting ring 19. When the device is subjected to external forces, it can absorb part of the energy through elastic deformation and play a buffering role. At the same time, the limiting ring 19 abuts against the limiting ring 5, restricting the axial movement range of the barrel 2, ensuring that the barrel 2 moves within a certain position range, helping to maintain the relative position stability between the components of the docking device, and improving the adaptability and reliability of the docking device under different working conditions.
[0034] Furthermore, a fixing groove 21 is formed on the surface of the outer shell 1, and a fixing ring plate 22 is arranged at the upper end of the outer shell 1. The fixing ring plate 22 matches the fixing groove 21. This structural design facilitates the installation and fixation of the entire docking device. In practical applications, the docking device can be quickly and accurately installed at the specified position by embedding the fixing ring plate 22 into the fixing groove 21, improving the installation efficiency. Moreover, the close cooperation between the fixing groove 21 and the fixing ring plate 22 can ensure that the docking device will not loosen or displace easily after installation, enhancing the overall stability of the device and providing a strong guarantee for the stable docking of the space antenna module.
[0035] Furthermore, the limiting ring 5 is located above the limiting circular ring 19. The lower end of the limiting ring 5 abuts against the upper end of the limiting circular ring 19. The limiting ring 5 and the limiting circular ring 19 cooperate with each other to accurately limit the position of the barrel 2 in the axial direction. Their abutment can effectively prevent the barrel 2 from moving up and down excessively, ensure that the barrel 2 is always in a proper position during the docking process, maintain the relative position accuracy between components, contribute to improving the accuracy and stability of docking, ensure that the space antenna module can work properly after docking, and avoid the problem of poor docking caused by the position deviation of the barrel 2.
[0036] Furthermore, docking heads 23 are slidably connected to the inner walls of the first fixing hole 7 and the second fixing rod hole 11. Two symmetrically arranged third limiting holes 24 are formed on the surface of the docking head 23. The inner walls of the first fixing hole 7 and the second fixing rod hole 11 are slidably connected to the docking head 23. This design makes the installation and disassembly of the docking head 23 easy and convenient. In the actual space operation scenario, the staff can quickly insert the docking head 23 into the corresponding holes to complete the preliminary positioning, greatly shortening the time required for docking and improving the operation efficiency. At the same time, the sliding connection method also allows the docking head 23 to fine-tune its position within a certain range to adapt to different docking environments and accuracy requirements, enhancing the flexibility of the docking operation.
[0037] Working principle: When docking the space antenna module, first insert the docking head 23 into the first fixing hole 7 and the second fixing rod hole 11. The third limiting holes 24 on the docking head 23 can be used for further cooperation and fixation with other components. During the insertion process, if an external force causes the disc 14 to move downward, the extrusion block 17 will support the disc 14 upward under the action of the first spring 16, playing a buffering and stabilizing role. At the same time, the limiting block on the inner wall of the barrel 2 restricts the position of the extrusion block 17 to prevent it from moving excessively. After docking is completed, the symmetrically arranged metal balls 18 in the housing 1 can cooperate with the circular holes 4 on the surface of the barrel 2 to further fix the docking state. If unlocking is required, apply a certain external force to overcome the elastic forces of the first spring 16 and the second spring 20, move the relevant components, and release the fixed state of the docking head 23 to complete the unlocking and separation operation. The above description enables those skilled in the art to implement or use the present invention. Various modifications to these embodiments will be obvious to those skilled in the art. The general principles defined herein can be implemented in other embodiments without departing from the spirit or scope of the present invention. Therefore, the present invention will not be limited to these embodiments shown herein, but will be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims
1. An antenna module unlockable passive docking device, comprising a housing (1), characterized in that: The inner wall of the shell (1) is provided with a barrel (2), the surface of the barrel (2) is provided with two symmetrically arranged straight notches (3), the surface of the barrel (2) is provided with two symmetrically arranged circular holes (4), the surface of the barrel (2) is fixed with a rod connected to a limiting ring (5), the upper end of the barrel (2) is fixedly connected with a circular block (6), the upper end of the circular block (6) is provided with a first fixing hole (7) connected to the surface of the circular block (6), the upper end of the circular block (6) is provided with a first fixing member (8), the surface of the first fixing member (8) is connected to the first fixing hole The circular block (6) is provided with a through hole (9) at the upper end, and a cylinder (10) is provided on the inner wall of the through hole (9). The upper end of the cylinder (10) is provided with a second fixing rod hole (11) which is connected to the surface of the cylinder (10). The upper end of the cylinder (10) is provided with a second fixing member (12), and the surface of the second fixing member (12) matches the inner wall of the second fixing rod hole (11). The lower end of the cylinder (10) is fixedly connected with a connecting component (13), and the lower end of the connecting component (13) is fixedly connected with a disc (14).
2. The antenna module unlockable passive docking device according to claim 1, characterized in that: A support column (15) is fixedly connected to the inner wall of the housing (1), a first spring (16) is fixedly connected to the surface of the support column (15), and an extrusion block (17) is fixedly connected to the other end of the first spring (16).
3. The antenna module unlockable passive docking device according to claim 1, characterized in that: The inner wall of the barrel (2) is fixedly connected to a limit block, the limit block abuts against the surface of the extrusion block (17), and the upper end of the extrusion block (17) abuts against the lower end of the disc (14).
4. The antenna module unlockable passive docking device according to claim 1, characterized in that: Two symmetrically arranged metal balls (18) are arranged inside the housing (1), and the metal balls (18) match the circular holes (4).
5. The antenna module unlockable passive docking device according to claim 1, characterized in that: The inner wall of the outer shell (1) is provided with a limiting circular ring (19), the upper end of the limiting circular ring (19) is fixedly connected to a second spring (20), and the upper end of the second spring (20) is fixedly connected to the inner wall of the outer shell (1).
6. The antenna module unlockable passive docking device according to claim 1, characterized in that: A fixing groove (21) is provided on the surface of the shell (1), and a fixing annular plate (22) is provided at the upper end of the shell (1), wherein the fixing annular plate (22) matches the fixing groove (21).
7. The antenna module unlockable passive docking device according to claim 1, characterized in that: The limiting ring (5) is located above the limiting circular ring (19), and the lower end of the limiting ring (5) abuts against the upper end of the limiting circular ring (19).
8. The antenna module unlockable passive docking device according to claim 1, characterized in that: The inner walls of the first fixing hole (7) and the second fixing rod hole (11) are both slidably connected with a butt joint (23), and the surface of the butt joint (23) is provided with two symmetrically arranged third limiting holes (24).