Avionics bus test platform

Abstract

The utility model discloses an avionics bus test platform, relates to the bus test technology field, and comprises a processor and a coupler, one side of the processor is provided with a first threaded hole, a mounting rack is installed through a bolt, two ends of the bottom of the coupler are fixedly provided with a connecting rack, the connecting rack is provided with a connecting hole, and the connecting hole is connected with the processor. An L-shaped fixing frame is fixedly mounted on the mounting frame, a push plate is arranged between the fixing frame and the mounting frame, positioning rods are fixedly mounted at the tops of the two ends of the push plate, penetrate through the mounting frame and are matched with the connecting holes, guide rods are fixedly mounted at the bottoms of the two ends of the push plate and penetrate through the fixing frame, and springs are arranged on the peripheral sides of the guide rods. The two ends of the spring are connected with the push plate and the fixing frame respectively, and a pull rod fixedly arranged at the bottom of the push plate penetrates through the fixing frame to be connected with a pull handle. According to the utility model, the push plate is moved by pulling the pull handle, and the positioning rod can be pulled out of or inserted into the connecting hole, so that the mounting and dismounting time is greatly shortened, and the testing efficiency is improved.

Description

Technical Field

[0001] This utility model relates to the field of bus testing technology, specifically to an avionics bus testing platform. Background Technology

[0002] Avionics bus is a general term for communication lines and related protocols used in avionics systems to enable data transmission and information exchange between various subsystems and devices. The 1553B bus is a serial data bus widely used in the aviation field and is a type of avionics bus. Developed by the U.S. Department of Defense, it features dual redundancy and time-division multiplexing, ensuring reliable data transmission. It is commonly used to connect critical systems on aircraft, such as engine control systems and flight management systems.

[0003] Chinese utility model patent application number 202420973667.9 provides a testing device for the 1553B bus. When using the testing device for the 1553B bus, the first cable and the second cable are connected by a socket and a connector. This not only makes the internal connection more convenient, but also prevents the internal connecting wires from becoming tangled after connection. At the same time, the cooperation between the first connecting tube and the second connecting tube can easily protect the connected cables and prevent poor contact or detachment due to contact.

[0004] However, during the use of the above equipment, it was found that the threaded connection needs to be screwed in one turn at a time. When the limit rod needs to be installed and removed frequently, it will consume a lot of time and reduce the efficiency of the testing work. Utility Model Content

[0005] To address the shortcomings of existing technologies, this utility model provides an avionics bus test platform, which solves the problem mentioned in the background art that the spiral connection consumes a lot of time and reduces the efficiency of the test work when the limit rod needs to be frequently installed and disassembled.

[0006] To achieve the above objectives, this utility model provides the following technical solution: an avionics bus test platform, comprising a processor and a coupler. A first threaded hole is provided on one side of the processor, and a mounting bracket is installed in the first threaded hole via bolts. Connecting brackets are fixedly installed at both ends of the bottom of the coupler, and connecting holes are provided on the connecting brackets. An L-shaped fixing bracket is fixedly installed on the mounting bracket. A push plate is provided between the fixing bracket and the mounting bracket. Positioning rods are fixedly installed at the top of both ends of the push plate, passing through the mounting bracket and fitting into the connecting holes. Guide rods are fixedly installed at the bottom of both ends of the push plate, passing through the fixing bracket. Springs are provided around the guide rods, with both ends of the springs connected to the push plate and the fixing bracket respectively. A pull rod is fixedly installed at the bottom of the push plate, passing through the fixing bracket and connected to a pull handle.

[0007] Preferably, the coupler has second threaded holes equidistantly spaced on one side, and a first cable is connected inside the second threaded holes, with a connector at one end of the first cable.

[0008] Preferably, a first sleeve is installed in the second threaded hole, one end of the first sleeve is provided with a first threaded tube, the first sleeve is spirally connected to the second threaded hole through the first threaded tube, and a first rotating frame is fixedly provided on the first sleeve.

[0009] Preferably, a third threaded hole is provided at equal intervals on one side of the processor, and a second cable is connected inside the third threaded hole. One end of the second cable is provided with a connector, and the connector is adapted to the connector.

[0010] Preferably, a second sleeve is installed in the third threaded hole, one end of the second sleeve is provided with a second threaded tube, the second sleeve is spirally connected to the third threaded hole through the second threaded tube, and a second rotating frame is provided on the second sleeve.

[0011] Preferably, the outer diameter of the second sleeve is adapted to the inner diameter of the first sleeve.

[0012] This utility model provides an avionics bus test platform. It has the following advantages:

[0013] (1) When the coupler needs to be connected or disassembled, simply pull the handle to move the push plate downward, compress the spring, and release the positioning rod from the fixed position, making it easy to disassemble the coupler. When installation is required, align the coupler's connecting bracket with the processor's mounting bracket, release the handle, the spring returns to its original shape, pushes the push plate upward, and the positioning rod is accurately inserted into the connecting hole of the connecting bracket, quickly completing the positioning connection and greatly saving connection time.

[0014] (2) When the connector head and the connector seat are connected in correspondence, the first sleeve and the second sleeve are adapted to each other. Combined with the positioning rod and the connecting hole, the stability of the connection between the coupler and the processor can be further improved, ensuring the reliability and stability of signal transmission. Attached Figure Description

[0015] Figure 1 This is a diagram showing the overall structure of the present utility model;

[0016] Figure 2 This utility model Figure 1 A diagram illustrating the structure of the processor.

[0017] Figure 3 This utility model Figure 1 A structural diagram of the intermediate coupler;

[0018] Figure 4 This utility model Figure 1 Structural diagram of the mounting bracket.

[0019] In the diagram, 1 is the processor; 11 is the third threaded hole; 12 is the second cable; 13 is the connector; 14 is the first threaded hole; 15 is the second sleeve; 151 is the second rotating frame; and 152 is the second threaded tube.

[0020] 2. Coupler; 21. Connecting bracket; 22. Connecting hole; 23. Second threaded hole; 24. First cable; 25. Connecting seat; 26. First sleeve; 261. First rotating bracket; 262. First threaded tube;

[0021] 3. Mounting bracket; 31. Fixing bracket; 32. Push plate; 321. Pull rod; 322. Pull handle; 323. Positioning rod; 324. Guide rod; 33. Spring. Detailed Implementation

[0022] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings. 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.

[0023] Example 1:

[0024] Please see Figures 1-4This utility model provides an avionics bus test platform, including a processor 1 and a coupler 2. A first threaded hole 14 is provided on one side of the processor 1, and a mounting bracket 3 is installed on the first threaded hole 14 by bolts. Connecting brackets 21 are fixedly provided at both ends of the bottom of the coupler 2, and connecting holes 22 are provided on the connecting brackets 21. An L-shaped fixing bracket 31 is fixedly installed on the mounting bracket 3. A push plate 32 is provided between the fixing bracket 31 and the mounting bracket 3. Positioning rods 323 are fixedly installed at the top of both ends of the push plate 32. The positioning rods 323 pass through the mounting bracket 3 and are adapted to the connecting holes 22. Guide rods 324 are fixedly installed at the bottom of both ends of the push plate 32. The guide rods 324 pass through the fixing bracket 31. Springs 33 are provided around the guide rods 324. The two ends of the springs 33 are respectively connected to the push plate 32 and the fixing bracket 31. A pull rod 321 is fixedly provided at the bottom of the push plate 32. The pull rod 321 passes through the fixing bracket 31 and is connected to the pull handle 322.

[0025] Specifically, when installing the coupler 2, align the mounting bracket 3 on the processor 1 with the connecting bracket 21 at the bottom of the coupler 2, so that the positioning rod 323 is aligned with the connecting hole 22. Then pull the handle 322. The handle 322 drives the push plate 32 to move downward through the pull rod 321. At this time, the spring 33 is compressed, and the positioning rod 323 is pulled out downward from the mounting bracket 3. When the positioning rod 323 is fully aligned with the connecting hole 22, release the handle 322. The spring 33 returns to its elastic deformation, pushes the push plate 32 to move upward, and then inserts the positioning rod 323 into the connecting hole 22, thus completing the installation of the coupler 2 and the processor 1.

[0026] When disassembling coupler 2, pull handle 322. Pull handle 322 drives push plate 32 to move downward through pull rod 321. Spring 33 is compressed, and positioning rod 323 is pulled out from connection hole 22. After positioning rod 323 is completely pulled out from connection hole 22, the connecting bracket 21 of coupler 2 is separated from mounting bracket 3 on processor 1, and the disassembly of coupler 2 can be completed. Installation and disassembly can be completed by pulling and releasing handle 322, which greatly saves operation time and improves work efficiency.

[0027] Furthermore, to improve the stability of coupler 2 and protect the cable connection, please refer to [link / reference needed]. Figures 1-4 The coupler 2 has a second threaded hole 23 equidistantly opened on one side, and a first cable 24 is connected inside the second threaded hole 23. A connector 25 is provided at one end of the first cable 24.

[0028] A first sleeve 26 is installed in the second threaded hole 23. A first threaded tube 262 is provided at one end of the first sleeve 26. The first sleeve 26 is spirally connected to the second threaded hole 23 through the first threaded tube 262. A first rotating frame 261 is fixedly provided on the first sleeve 26.

[0029] A third threaded hole 11 is provided at equal intervals on one side of the processor 1. A second cable 12 is connected inside the third threaded hole 11. One end of the second cable 12 is provided with a connector 13, which is correspondingly adapted to the connector 25.

[0030] A second sleeve 15 is installed in the third threaded hole 11. A second threaded tube 152 is provided at one end of the second sleeve 15. The second sleeve 15 is spirally connected to the third threaded hole 11 through the second threaded tube 152. A second rotating frame 151 is provided on the second sleeve 15.

[0031] The outer diameter of the second sleeve 15 is compatible with the inner diameter of the first sleeve 26.

[0032] Specifically, when coupler 2 is connected to processor 1, the connector 25 on the first cable 24 is connected to the connector 13 on the second cable 12. At this time, the second threaded tube 152, which is spirally connected in the third threaded hole 11, is inserted into the first threaded tube 262. The outer diameter of the second sleeve 15 matches the inner diameter of the first sleeve 26, and the two cooperate with each other during connection. This not only enables coupler 2 and processor 1 to be more precisely aligned and ensures accurate docking of connector 13 and connector 25, but also further enhances the stability of the connection. Combined with the cooperation of positioning rod 323 and connecting hole 22, the stability of coupler 2 is improved from multiple dimensions.

[0033] The sheath encloses the cable, preventing external mechanical damage such as friction, compression, and impact. It also prevents damage to the outer sheath caused by friction with other components, thus protecting the internal core wires. Furthermore, when the cable is subjected to tensile or torsional forces, the sheath distributes these forces across its entire surface, rather than concentrating them at the cable connection points. This effectively reduces stress at the cable connection points, preventing excessive stress from causing the internal core wires to break or the connection points to loosen.

[0034] Working principle: Connect the first sleeve 26 in the second threaded hole 23 on one side of the coupler 2 to the second sleeve 15 in the third threaded hole 11 on the side of the processor 1, so that the second threaded tube 152 is inserted into the first threaded tube 262. By utilizing the matching relationship between the second sleeve 15 and the first sleeve 26, the connector 13 and the connector 25 are accurately aligned to complete the electrical connection. Then, align the mounting bracket 3 on the processor 1 with the connecting bracket 21 at the bottom of the coupler 2, so that the positioning rod 323 is aligned with the connecting hole 22. Then pull the handle 322. The handle 322 drives the push plate 32 to move downward through the pull rod 321, compressing the spring 33, so that the positioning rod 323 is pulled out downward from the mounting bracket 3. When the positioning rod 323 is completely aligned with the connecting hole 22, release the handle 322. The spring 33 returns to its elastic deformation, pushing the push plate 32 to move upward, so that the positioning rod 323 is inserted into the connecting hole 22, thus completing the mechanical installation and fixation of the coupler 2 and the processor 1.

[0035] After the coupler 2 and processor 1 are installed and connected, the avionics bus test platform can be put into use. The processor 1 controls and utilizes the coupler 2 to perform various test tasks on the avionics bus, such as signal transmission testing and data communication testing. When the test is completed and the coupler 2 needs to be disassembled, pull the handle 322. The handle 322, through the pull rod 321, moves the push plate 32 downwards, compressing the spring 33, and pulling the positioning rod 323 out of the connection hole 22. After the positioning rod 323 is completely pulled out of the connection hole 22, separate the connecting bracket 21 of the coupler 2 from the mounting bracket 3 on the processor 1 to complete the disassembly of the coupler 2.

[0036] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. It will be apparent to those skilled in the art that this utility model is not limited to the details of the exemplary embodiments described above, and that it can be implemented in other specific forms without departing from the spirit or basic characteristics of this utility model. Therefore, the embodiments should be considered exemplary and non-limiting in all respects. The scope of this utility model is defined by the appended claims rather than the foregoing description, and thus all variations falling within the meaning and scope of equivalents of the claims are intended to be included within this utility model. No reference numerals in the claims should be construed as limiting the scope of the claims.

[0037] Furthermore, it should be understood that although this specification describes embodiments, not every embodiment contains only one independent technical solution. This narrative style is merely for clarity. Those skilled in the art should consider the specification as a whole, and the technical solutions in each embodiment can also be appropriately combined to form other embodiments that can be understood by those skilled in the art.

Claims

1. An avionics bus test platform, comprising a processor (1) and a coupler (2), characterized in that: The processor (1) has a first threaded hole (14) on one side, and a mounting bracket (3) is installed on the first threaded hole (14) by bolts. A connecting bracket (21) is fixedly installed at both ends of the bottom of the coupler (2). A connecting hole (22) is opened on the connecting bracket (21). An L-shaped fixing bracket (31) is fixedly installed on the mounting bracket (3). A push plate (32) is provided between the fixing bracket (31) and the mounting bracket (3). Positioning rods (323) are fixedly installed at the top of both ends of the push plate (32). 323) The push plate (32) is fitted with a guide rod (324) at both ends of the bottom of the push plate (32). The guide rod (324) passes through the fixed frame (31). A spring (33) is provided on the periphery of the guide rod (324). The two ends of the spring (33) are respectively connected to the push plate (32) and the fixed frame (31). A pull rod (321) is fixedly provided at the bottom of the push plate (32). The pull rod (321) passes through the fixed frame (31) and is connected to the handle (322).

2. The avionics bus test platform according to claim 1, characterized in that: The coupler (2) has a second threaded hole (23) equidistantly opened on one side. A first cable (24) is connected inside the second threaded hole (23). A connector (25) is provided at one end of the first cable (24).

3. The avionics bus test platform according to claim 2, characterized in that: A first sleeve (26) is installed in the second threaded hole (23). One end of the first sleeve (26) is provided with a first threaded tube (262). The first sleeve (26) is spirally connected to the second threaded hole (23) through the first threaded tube (262). A first rotating bracket (261) is fixedly provided on the first sleeve (26).

4. The avionics bus test platform according to claim 3, characterized in that: The processor (1) has a third threaded hole (11) equidistantly opened on one side. A second cable (12) is connected inside the third threaded hole (11). One end of the second cable (12) is provided with a connector (13). The connector (13) is correspondingly adapted to the connector (25).

5. The avionics bus test platform according to claim 4, characterized in that: A second sleeve (15) is installed in the third threaded hole (11). A second threaded tube (152) is provided at one end of the second sleeve (15). The second sleeve (15) is spirally connected to the third threaded hole (11) through the second threaded tube (152). A second rotating frame (151) is provided on the second sleeve (15).

6. The avionics bus test platform according to claim 5, characterized in that: The outer diameter of the second sleeve (15) is compatible with the inner diameter of the first sleeve (26).

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