Rectangular aviation socket

By designing the structure of the pressing plate, locking block and rubber pad in a rectangular aviation socket, the problem of the installation plate falling off is solved, the protection performance and connection stability of the plug are improved, the service life is extended and the installation and maintenance are facilitated.

CN222953465UActive Publication Date: 2025-06-06ZHEJIANG ZHIBANG ELECTRIC POWER TECH CO LTD
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Patent Information

Application Number
CN202421984138.5
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-08-16
Publication Date
2025-06-06
Estimated Expiration
2034-08-16

AI Technical Summary

Technical Problem

During multiple plugging and separation operations, the mounting plate is prone to fall off from the tail of the shell, resulting in poor connectivity and reduced service life.

Method used

By designing the plug-in and installation process between the base shell and the plug shell, combining the structure of the pressing plate, locking block and rubber pad, the limit installation and tightening fixing functions are achieved, and the effectiveness of the locking mechanism is enhanced.

Benefits of technology

It improves the protection performance and connection stability of the plug, extends the service life of rectangular aviation sockets, and provides convenient installation and maintenance under the premise of electrical safety.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses a rectangular aviation socket, which relates to the technical field of electric connectors, and comprises a base shell, a plug shell is detachably connected in the base shell, a plugging groove is arranged in the plug shell, a rectangular aviation plug main body is fixedly arranged in the plugging groove, a connecting hole is arranged on one side of the base shell, and a rectangular aviation plug main body is fixedly arranged on the other side of the base shell. The two ends of the plug housing are fixedly provided with protective frames. In the plug-in installation process of the base shell and the plug shell, the pressing plate is tightly combined with the top of the locking block, and the connecting column at the bottom of the pressing plate applies pressure on the rubber pad, so that the rubber pad pushes the pushing block to move downwards along the sliding rail after being stressed, and the pushing block is matched with the connectivity synergistic effect of the stretching rod; therefore, the efficiency of the locking mechanism is enhanced, and the protection performance of the plug is improved.
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Description

Technical Field

[0001] The utility model relates to the technical field of electric connectors, in particular to a rectangular aviation socket. Background Art

[0002] Rectangular aviation socket, as a kind of aviation plug, is an electromechanical component that connects electrical circuits. It is widely used in complex industrial environments and outdoor environments such as aviation, aerospace, navigation, national defense, military, and electricity. Rectangular aviation socket is a type of connector developed for application scenarios such as complex industrial environments and outdoor environments. It is formally called "industrial connector". It is mainly used for circuit connection between cables and cables, and cables and equipment of electrical and electronic equipment to realize the transmission of signals and electrical energy.

[0003] In the existing technical solution, a rectangular high-voltage electrical socket connector is proposed, including a shell, a mounting plate installed in the shell, the mounting plate is glued and fixed to the shell, the high-voltage wire and the pin contact are crimped and then installed in the mounting plate, and the tail of the shell also has a blocking rib.

[0004] In order to solve the problem that the mounting plate is easily detached from the rear of the shell during multiple plugging and separation operations, the prior art uses a method of fixing the pin contact and the mounting plate by bonding to ensure good voltage resistance performance. Since there are blocking ribs at the rear of the shell, the blocking ribs of the shell can prevent the mounting plate from detaching from the shell when the socket connector and the matching plug connector are plugged in and separated, but the connection between the plug and the socket is poor, and it is easy to fall off after plugging, which leads to the problem of reduced service life of the rectangular aviation socket. Utility Model Content

[0005] The purpose of the utility model is to provide a rectangular aviation socket to solve the problems raised in the above background technology.

[0006] In order to solve the above technical problems, the technical solution adopted by the utility model is:

[0007] A rectangular aviation socket comprises a base shell, the interior of which is detachably connected to a plug shell, the interior of which is provided with a plugging slot, the interior of which is fixedly installed with a rectangular aviation plug body, a connecting hole is provided on one side of the base shell, and protective frames are fixedly installed at both ends of the plug shell.

[0008] Locking blocks are fixedly installed on both sides of the base shell, and a locking mechanism is fixedly installed inside the locking block.

[0009] Mounting plates are fixedly mounted on both ends of the plug housing, and a protective mechanism is arranged on the surface of the mounting plate.

[0010] A further improvement of the technical solution of the utility model is that the locking mechanism comprises a plug board, a pressing plate is movably mounted on the top of the plug board, and one side of the pressing plate is fixedly mounted on both sides of the plug housing.

[0011] By adopting the above technical solution, the function of position limiting installation is achieved through the cooperation between the plug board, the pressing plate and the plug shell.

[0012] A further improvement of the technical solution of the utility model is that: mounting holes are opened at both ends of the top of the locking block, and an extension column is movably installed inside the mounting hole, and the top of the extension column is fixedly installed on the bottom of the pressing plate.

[0013] By adopting the above technical solution, the function of sleeve assembly is achieved through the cooperation between the mounting hole and the extension column.

[0014] A further improvement of the technical solution of the utility model is that a locking column is fixedly installed inside the locking block, a clamping ring is movably sleeved inside the locking column, a reset spring column is movably installed on the inner wall of the clamping ring, and a clamping block is movably installed on the inner side of the reset spring column.

[0015] By adopting the above technical solution, the locking column, the clamping ring, the return spring and the clamping block cooperate with each other to achieve the function of pressing and fixing.

[0016] A further improvement of the technical solution of the utility model is that: a stretching rod is fixedly connected to the bottom of the clamping ring, a pushing block is fixedly installed at the bottom of the stretching rod, and a rubber pad is fixedly installed inside the pushing block.

[0017] By adopting the above technical solution, the tensioning function is achieved through the cooperation between the stretching rod, the pushing block and the rubber pad.

[0018] A further improvement of the technical solution of the utility model is that a slide rail is movably installed on the outer side of the pushing block, and the outer side of the slide rail is fixedly installed on the inner wall of the plug board.

[0019] A further improvement of the technical solution of the utility model is that the protection mechanism comprises an anti-insertion ring, the bottom of the anti-insertion ring is fixedly mounted on the surface of the assembly plate, and a blocking bar is fixedly mounted inside the anti-insertion ring.

[0020] By adopting the above technical solution, the function of preventing wrong insertion is achieved through the cooperation between the anti-insertion ring, the assembly plate and the baffle.

[0021] Due to the adoption of the above technical solution, the utility model has achieved the following technical progress compared with the prior art:

[0022] 1. The utility model provides a rectangular aviation socket. During the plug-in installation process of the base shell and the plug shell, the clamping plate is tightly combined with the top of the locking block, and the connecting column at the bottom of the clamping plate applies pressure on the rubber pad, causing the rubber pad to push the pushing block to move downward along the slide rail after being stressed, and cooperates with the connectivity of the stretching rod to urge the clamping mechanism to perform a downward pressing action, thereby enhancing the effectiveness of the locking mechanism and further improving the protective performance of the plug.

[0023] 2. The utility model provides a rectangular aviation socket. The product adopts a separate design of the plug shell and the base shell to ensure that after the plug and the socket are connected, the double locking mechanism is firmly locked. On the basis of ensuring that the PE double grounding terminal is reliably grounded, the plug-and-play function is achieved, and convenience is provided for installation and maintenance work while ensuring electrical safety.

[0024] 3. The utility model provides a rectangular aviation socket. We have carefully designed the anti-insertion ring and the limiting function of the baffle at both ends of the assembly plate to ensure that the rectangular aviation socket has the anti-misinsertion feature, thereby improving the protection performance of the device. The termination of the pin and the wire adopts a straight-insertion self-locking connection method to ensure the stability of the connection. For the electrical contact, high-quality copper alloy is selected and silver-plated to ensure its conductivity and corrosion resistance, so that the protection level is not lower than IP65. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] Figure 1 It is a structural schematic diagram of the utility model;

[0026] Figure 2 For the utility model Figure 1 A in the enlarged view;

[0027] Figure 3 This is a schematic diagram of the locking block structure of the utility model;

[0028] Figure 4 This is a schematic diagram of the plug board structure of the utility model;

[0029] Figure 5 It is a schematic diagram of the main structure of the rectangular aviation plug of the utility model.

[0030] In the figure: 1. base shell; 2. plug shell; 3. plug-in slot; 4. rectangular aviation plug body; 5. connecting hole; 6. protective frame; 11. locking block; 12. mounting hole; 13. extension column; 14. locking plug column; 15. plug-in board; 21. clamping plate; 40. assembly plate; 41. anti-plug-in ring; 42. baffle; 151. clamping ring; 152. reset spring column; 153. clamping block; 154. stretching rod; 155. pushing block; 156. slide rail; 157. rubber pad. DETAILED DESCRIPTION

[0031] The present invention is further described in detail below in conjunction with the embodiments:

[0032] like Figure 1-5 As shown, the utility model provides the following technical solutions.

[0033] Example 1

[0034] The present embodiment provides a rectangular aviation socket, including a base shell 1, wherein a plug shell 2 is detachably connected to the interior of the base shell 1, a plugging slot 3 is provided inside the plug shell 2, a rectangular aviation plug body 4 is fixedly installed inside the plugging slot 3, a connecting hole 5 is provided on one side of the base shell 1, protective frames 6 are fixedly installed at both ends of the plug shell 2, locking blocks 11 are fixedly installed on both sides of the base shell 1, a locking mechanism is fixedly installed inside the locking block 11, and the locking mechanism includes a plug-in board 15, a clamping plate 21 is movably installed on the top of the plug-in board 15, one side of the clamping plate 21 is fixedly installed on both sides of the plug shell 2, mounting holes 12 are provided at both ends of the top of the locking block 11, an extension column 13 is movably installed inside the mounting hole 12, the top of the extension column 13 is fixedly installed on the bottom of the clamping plate 21, a locking plug column 14 is fixedly installed inside the locking block 11, a clamping ring 151 is movably sleeved inside the locking plug column 14, and a reset spring column 152 is movably installed on the inner wall of the clamping ring 151 The inner side of the reset spring column 152 is movably installed with a clamping block 153, which is sleeved on the inside of the base shell 1 through the plug shell 2, and is plugged into the top of the locking block 11 with the clamping plate 21, so that the connecting column at the bottom of the clamping plate 21 is plugged into the inside of the locking plug column 14, thereby pushing the clamping block 153 to compress the reset spring column 152, and utilizing the resilience of the reset spring column 152 to perform the clamping function, which is conducive to the limited installation of the device, and the coordinated rectangular aviation plug should be arranged and installed in the secondary small room, and the wire trough is arranged on the top of the cabinet for prefabricated cable routing. The rectangular aviation plugs in the terminal DTU cabinet of the station are centrally arranged on the aviation plug mounting plate, and the aviation plug mounting plate should be horizontally arranged and installed on the lower side of the cabinet. The aviation plug mounting plate shall not block the terminal row, which is convenient for use. The plug shell and the base shell are designed separately. After the plug and the socket are plugged in, a double lock locking method is adopted, and while ensuring that the PE double grounding position is reliably grounded, plug and play is realized to ensure convenient installation and maintenance under the premise of electrical safety.

[0035] Example 2

[0036] On the basis of Example 1, this embodiment provides a technical solution: preferably, a stretching rod 154 is fixedly connected to the bottom of the clamping ring 151, a pushing block 155 is fixedly installed on the bottom of the stretching rod 154, a rubber pad 157 is fixedly installed inside the pushing block 155, a slide rail 156 is movably installed on the outer side of the pushing block 155, the outer side of the slide rail 156 is fixedly installed on the inner wall of the plug board 15, and the base shell is plugged into the plug shell to drive the clamping plate 21 to be merged on the top of the locking block 11, so that the connecting column at the bottom of the clamping plate 21 is pushed on the rubber pad 157, and the rubber pad 157 is driven by force to drive the pushing block 155 to slide downward along the slide rail 156, and cooperate with the connectivity of the stretching rod 154 to drive the clamping mechanism to press down, thereby further increasing the locking function and increasing the protection function of the plug.

[0037] Example 3

[0038] On the basis of Example 1, this embodiment provides a technical solution: preferably, assembly plates 40 are fixedly installed at both ends of the plug shell 2, and a protective mechanism is arranged on the surface of the assembly plate 40, the protective mechanism includes an anti-insertion ring 41, the bottom of the anti-insertion ring 41 is fixedly installed on the surface of the assembly plate 40, and a baffle 42 is fixedly installed inside the anti-insertion ring 41. By arranging the anti-insertion ring 41 at both ends of the assembly plate 40 and utilizing the limiting property of the baffle 42, the rectangular aviation socket has the function of preventing mis-insertion, thereby increasing the protection function of the device, and the termination of the pin and the wire adopts a straight-insertion self-locking connection method, and the electrical contact is made of high-quality copper alloy plated with silver, and the protection level is not lower than IP65.

[0039] The following is a detailed description of the working principle of the rectangular aviation socket.

[0040] like Figure 1-5As shown, the plug shell 2 is sleeved inside the base shell 1, and the clamping plate 21 is inserted into the top of the locking block 11, so that the connecting column at the bottom of the clamping plate 21 is inserted into the inside of the locking plug column 14, thereby pushing the clamping block 153 to compress the reset spring column 152, and utilizing the resilience of the reset spring column 152 to perform the clamping function, which is beneficial to the limited installation of the device, and the coordinated rectangular aviation plug should be arranged and installed in the secondary small room, and the wire trough is arranged on the top of the cabinet for prefabricated cable routing. The rectangular aviation plugs in the terminal DTU cabinet of the station are centrally arranged on the aviation plug mounting plate, and the aviation plug mounting plate should be horizontally arranged and installed on the lower side of the cabinet. The aviation plug mounting plate shall not block the terminal row, which is convenient for use. The plug shell and the base shell are designed as separate bodies. After the plug and the socket are plugged in, a double lock locking method is adopted, and while ensuring the PE double connection position While achieving reliable grounding, plug and play is realized to ensure convenient installation and maintenance under the premise of electrical safety. The base shell and the plug shell are plugged and installed, driving the clamping plate 21 to merge on the top of the locking block 11, so that the connecting column at the bottom of the clamping plate 21 is pushed on the rubber pad 157. The rubber pad 157 is driven by force to drive the pushing block 155 to slide downward along the slide rail 156, and cooperates with the connectivity of the stretching rod 154 to drive the clamping mechanism to press down, thereby further achieving the locking function and increasing the protection function of the plug. Anti-insertion rings 41 are set at both ends of the assembly plate 40, and the limiting property of the baffle 42 is used to make the rectangular aviation socket have the function of preventing mis-insertion, thereby increasing the protection function of the device. The termination of the pin and the wire adopts a direct plug-in self-locking connection method, and the electrical contact is made of high-quality copper alloy plated with silver, and the protection level is not lower than IP65.

[0041] The above generally describes the present invention in detail, but it is obvious to a person skilled in the art that some modifications or improvements can be made to the present invention. Therefore, modifications or improvements that do not deviate from the spirit of the present invention are within the scope of protection of the present invention.

Claims

1. A rectangular aviation socket, comprising a base housing (1), characterized in that: The base shell (1) is detachably connected to a plug shell (2), a plug slot (3) is provided inside the plug shell (2), a rectangular aviation plug body (4) is fixedly installed inside the plug slot (3), a connection hole (5) is provided on one side of the base shell (1), and protective frames (6) are fixedly installed at both ends of the plug shell (2); Locking blocks (11) are fixedly mounted on both sides of the base shell (1), and a locking mechanism is fixedly mounted inside the locking block (11); Mounting plates (40) are fixedly mounted on both ends of the plug housing (2), and a protective mechanism is provided on the surface of the mounting plate (40).

2. The rectangular aviation socket according to claim 1, characterized in that: The locking mechanism comprises a plug-in board (15), a pressing plate (21) is movably mounted on the top of the plug-in board (15), and one side of the pressing plate (21) is fixedly mounted on two sides of the plug housing (2).

3. The rectangular aviation socket according to claim 1, characterized in that: Both ends of the top of the locking block (11) are provided with mounting holes (12), an extension column (13) is movably installed inside the mounting hole (12), and the top of the extension column (13) is fixedly installed on the bottom of the pressing plate (21).

4. The rectangular aviation socket according to claim 1, characterized in that: A locking plug post (14) is fixedly installed inside the locking block (11), a clamping ring (151) is movably sleeved inside the locking plug post (14), a reset spring post (152) is movably installed on the inner wall of the clamping ring (151), and a clamping block (153) is movably installed inside the reset spring post (152).

5. The rectangular aviation socket according to claim 4, characterized in that: The bottom of the clamping ring (151) is fixedly connected to a stretching rod (154), the bottom of the stretching rod (154) is fixedly installed with a pushing block (155), and the interior of the pushing block (155) is fixedly installed with a rubber pad (157).

6. The rectangular aviation socket according to claim 5, characterized in that: A slide rail (156) is movably mounted on the outer side of the pushing block (155), and the outer side of the slide rail (156) is fixedly mounted on the inner wall of the plug board (15).

7. The rectangular aviation socket according to claim 1, characterized in that: The protection mechanism comprises an anti-insertion ring (41), the bottom of the anti-insertion ring (41) is fixedly mounted on the surface of the assembly plate (40), and a blocking bar (42) is fixedly mounted inside the anti-insertion ring (41).