Aviation connector assembly

Abstract

The utility model discloses an aviation connector assembly, and relates to the technical field of aviation equipment. The socket comprises a socket, one side of the socket is provided with a column groove, and the inner side of the column groove is provided with pins in an annular array; the plug is in a column shape, one end of the plug is inserted into the column groove in a sliding mode, jacks are formed in the end, close to the socket, of the plug in an annular array mode, the jacks are matched with the contact pins in size, and an insulating tray is fixedly arranged on the side, away from the socket, of the plug; and the locking sleeve is arranged at the top of the socket. Through innovative design of the locking sleeve and cooperative work of the sliding block, the spring, the hinge plate, the [-shaped cover and the limiting block, stable locking of the plug is realized, stability of connection between the plug and the socket is remarkably improved, connection interruption caused by vibration or collision is reduced, and meanwhile, the device is reasonable in structural design, very simple to operate and convenient to use. And the method is high in practicability and worthy of general application and popularization.

Description

TECHNICAL FIELD

[0001] The utility model relates to aviation equipment technical field, concretely relates to an aviation plug seat. BACKGROUND

[0002] The aviation plug seat is a device for connecting and disconnecting electrical lines, and is widely used in aviation, aerospace, military, industry and other fields. Its main function is to ensure the reliable connection of electrical equipment, and is convenient for disassembly and maintenance. In the aircraft, the aviation plug seat is used for connecting airborne equipment, control system, communication system and other key components to ensure the transmission of electrical signals and power,

[0003] In the traditional technology, after the aviation plug seat is inserted into the socket, due to the lack of effective fixing mechanism, the plug is very easy to loosen or even fall off after being subjected to vibration or impact, resulting in interruption of current or signal transmission, affecting the normal work of the equipment, therefore we propose an aviation plug seat to solve the above problems. SUMMARY

[0004] The utility model discloses in order to realize above-mentioned purpose specifically adopts following technical scheme:

[0005] An aviation plug seat, comprising:

[0006] The socket is constructed with a column groove on one side, and the inner side of the column groove is annularly arrayed with a pin;

[0007] The plug is columnar, and one end thereof is slidably inserted into the inside of the column groove, the end of the plug close to the socket is annularly arrayed with a socket, the socket is matched in size with the pin, and the side of the plug away from the socket is fixedly provided with an insulating tray;

[0008] The locking sleeve is arranged on the top of the socket, and is used for preventing the plug from being separated from the column groove.

[0009] Further, the locking sleeve comprises a rectangular frame fixedly arranged on the top of the socket, a guide rod fixedly arranged between the two inner side walls of the rectangular frame, a slider slidably sleeved on the surface of the guide rod, a spring connected between the slider and one of the inner side walls of the rectangular frame, the spring being sleeved on the surface of the guide rod, hinged plates hinged on the two sides of the slider, a H-shaped cover fixedly arranged at the other end of the hinged plate, a limiting block fixedly arranged at the other end of the H-shaped cover, the limiting block being arc-shaped, and the insulating tray abutting against the limiting block.

[0010] Further, the side of the limiting block close to the plug is constructed with a circular groove matched in size with the insulating tray.

[0011] Further, the bottom side of the limiting block is constructed with a rectangular gap communicated with the circular groove.

[0012] Further, a transparent observation window is arranged in the middle of the top of the F-shaped cover.

[0013] Further, a rectangular block is arranged in the middle of the side of the plug close to the socket, and a rectangular slot matching the rectangular block is arranged in the middle of the column groove.

[0014] Further, a mounting plate is arranged, and the mounting plate is arranged at the end of the socket away from the plug, and mounting holes are arranged at the four corners of the mounting plate.

[0015] The utility model discloses the beneficial effects are as follows:

[0016] The utility model discloses the beneficial effects are as follows: BRIEF DESCRIPTION OF DRAWINGS

[0017] Figure 1 It is the three-dimensional structure schematic diagram of the utility model;

[0018] Figure 2 It is another three-dimensional structure schematic diagram of the utility model;

[0019] Figure 3 It is the three-dimensional structure schematic diagram of the utility model Figure 2 The top view schematic diagram of the utility model;

[0020] Figure 4 It is the A-A direction section view schematic diagram of the utility model Figure 3 The utility model discloses the beneficial effects are as follows:

[0021] Fig. 1 socket, 101, column groove, 102, pin, 103, rectangular slot, 2, plug, 201, plug hole, 202, insulating tray, 203, rectangular block, 3, locking sleeve, 301, rectangular frame, 302, guide rod, 303, sliding block, 304, spring, 305, hinged plate, 306, F-shaped cover, 3061, transparent observation window, 307, limit block, 3071, round groove, 3072, rectangular gap, 4, mounting plate, 401, mounting hole. DETAILED DESCRIPTION

[0022] In order to make the purpose, technical scheme and advantage of the utility model embodiment more clear, the technical scheme in the utility model embodiment will be described clearly and completely with the drawings in the utility model embodiment.

[0023] The application provides an aviation plug seat, which is mainly used for solving the problem that the plug is very easy to loosen or even fall off after being subjected to vibration or impact due to the lack of effective fixing mechanism after the aviation plug seat is inserted into the socket, thereby interrupting the current or signal transmission and affecting the normal work of the equipment, and provides the following technical scheme, which will be described in detail below Figures 1-4 The application provides an aviation plug seat, which is mainly used for solving the problem that the plug is very easy to loosen or even fall off after being subjected to vibration or impact due to the lack of effective fixing mechanism after the aviation plug seat is inserted into the socket, thereby interrupting the current or signal transmission and affecting the normal work of the equipment, and provides the following technical scheme, which will be described in detail below

[0024] The application provides an aviation plug seat, which is mainly used for solving the problem that the plug is very easy to loosen or even fall off after being subjected to vibration or impact due to the lack of effective fixing mechanism after the aviation plug seat is inserted into the socket, thereby interrupting the current or signal transmission and affecting the normal work of the equipment, and provides the following technical scheme, which will be described in detail below

[0025] The application provides an aviation plug seat, which is mainly used for solving the problem that the plug is very easy to loosen or even fall off after being subjected to vibration or impact due to the lack of effective fixing mechanism after the aviation plug seat is inserted into the socket, thereby interrupting the current or signal transmission and affecting the normal work of the equipment, and provides the following technical scheme, which will be described in detail below

[0026] The application provides an aviation plug seat, which is mainly used for solving the problem that the plug is very easy to loosen or even fall off after being subjected to vibration or impact due to the lack of effective fixing mechanism after the aviation plug seat is inserted into the socket, thereby interrupting the current or signal transmission and affecting the normal work of the equipment, and provides the following technical scheme, which will be described in detail below

[0027] The application provides an aviation plug seat, which is mainly used for solving the problem that the plug is very easy to loosen or even fall off after being subjected to vibration or impact due to the lack of effective fixing mechanism after the aviation plug seat is inserted into the socket, thereby interrupting the current or signal transmission and affecting the normal work of the equipment, and provides the following technical scheme, which will be described in detail below

[0028] The application provides an aviation plug seat, which is mainly used for solving the problem that the plug is very easy to loosen or even fall off after being subjected to vibration or impact due to the lack of effective fixing mechanism after the aviation plug seat is inserted into the socket, thereby interrupting the current or signal transmission and affecting the normal work of the equipment, and provides the following technical scheme, which will be described in detail below

[0029] The application provides an aviation plug seat, which is mainly used for solving the problem that the plug is very easy to loosen or even fall off after being subjected to vibration or impact due to the lack of effective fixing mechanism after the aviation plug seat is inserted into the socket, thereby interrupting the current or signal transmission and affecting the normal work of the equipment, and provides the following technical scheme, which will be described in detail below

[0030] The application provides an aviation plug seat, which is mainly used for solving the problem that the plug is very easy to loosen or even fall off after being subjected to vibration or impact due to the lack of effective fixing mechanism after the aviation plug seat is inserted into the socket, thereby interrupting the current or signal transmission and affecting the normal work of the equipment, and provides the following technical scheme, which will be described in detail below

[0031] The application provides an aviation plug seat, which is mainly used for solving the problem that the plug is very easy to loosen or even fall off after being subjected to vibration or impact due to the lack of effective fixing mechanism after the aviation plug seat is inserted into the socket, thereby interrupting the current or signal transmission and affecting the normal work of the equipment, and provides the following technical scheme, which will be described in detail below

[0032] The aviation plug 2 seat over the innovative locking sleeve 3 design, using the slider 303, spring 304, hinged plate 305, the letter-shaped cover 306 and the limiting block 307 work together, realize the stable locking to the plug 2, significantly improve the stability of the plug 2 and the socket 1 connection, reduce the connection interruption caused by vibration or collision, at the same time, the device structure design is reasonable, the operation is very simple, the practicality is higher.

[0033] As Figure 4 shown, in some embodiments, the limiting block 307 is configured with a circular groove 3071 on the side close to the plug 2, and the circular groove 3071 is matched with the size of the insulating tray 202, more specifically, the design of the circular groove 3071 ensures that the insulating tray 202 can be accurately aligned with the limiting block 307, when the insulating tray 202 enters the circular groove 3071, a close fit is formed between them, limiting the movement of the insulating tray 202 (and the entire plug 2) in the horizontal direction, enhancing the stability of the plug 2 in the socket 1, preventing the plug 2 from loosening or falling off due to vibration or collision.

[0034] As Figure 2 shown, in some embodiments, the limiting block 307 is configured with a rectangular notch 3072 on the bottom side, which is in communication with the circular groove 3071, more specifically, the main purpose of the rectangular notch 3072 is to provide a channel for power lines or data lines, when the plug 2 is inserted into the socket 1 and locked, the limiting block 307 is closely fitted with the insulating tray 202 through the circular groove 3071 on it, ensuring the stability of the plug 2, at the same time, the rectangular notch 3072 as a cable channel allows the power lines or data lines to pass through the bottom of the limiting block 307, enter or exit the plug 2 inside, this design makes the cable can smoothly pass through the limiting block 307, without interfering with the connection between the plug 2 and the socket 1. After the cable passes through the rectangular notch 3072, they can be further fixed or arranged to ensure the neatness and reliability of the overall connection.

[0035] As Figure 1 shown, in some embodiments, the top of the letter-shaped cover 306 is provided with a transparent observation window 3061, more specifically, the transparent observation window 3061 allows the operator to directly observe the connection between the plug 2 and the socket 1 without opening or disassembling any parts. Through the window, it can be clearly seen whether the pin 102 is completely inserted into the corresponding socket 201, ensuring the correctness and integrity of the electrical connection.

[0036] As Figure 1As shown in the drawings, in some embodiments, the plug 2 is fixed with a rectangular block 203 in the middle of one side close to the socket 1, and the column groove 101 is configured with a rectangular groove 103 matched with the rectangular block 203, more specifically, the cooperation of the rectangular block 203 and the rectangular groove 103 provides initial accurate guidance when the plug 2 is inserted into the socket 1, ensuring that the plug 2 can be accurately aligned with the pin 102 in the socket 1, thereby avoiding the situation of misplug or misplug.

[0037] As Figure 2 As shown in the drawings, in some embodiments, the plug 2 is fixed with a rectangular block 203 in the middle of one side close to the socket 1, and the column groove 101 is configured with a rectangular groove 103 matched with the rectangular block 203, more specifically, the cooperation of the rectangular block 203 and the rectangular groove 103 provides initial accurate guidance when the plug 2 is inserted into the socket 1, ensuring that the plug 2 can be accurately aligned with the pin 102 in the socket 1, thereby avoiding the situation of misplug or misplug.

[0038] The above description of disclosed embodiments enables those skilled in the art to carry out or use the present application. Various modifications to these embodiments will be apparent to those skilled in the art, and the general principles defined herein can be implemented in other embodiments without departing from the spirit or scope of the present application. Therefore, the present application will not be limited to the embodiments shown herein, but will conform to the widest scope consistent with the principles and novel features disclosed herein.

Claims

1. An aircraft plug-in receptacle, characterized in that Include: Socket (1), the socket (1) is configured with a column groove (101) on one side, and the inner side of the column groove (101) is annularly arrayed with a pin (102); Plug (2), the plug (2) is columnar, and one end of the plug (2) is slidably inserted into the inside of the column groove (101), the plug (2) is annularly configured with a socket (201) near one end of the socket (1), the socket (201) is matched in size with the pin (102), and the plug (2) is fixedly provided with an insulating tray (202) away from the socket (1); Locking sleeve (3), provided on the top of the socket (1), the locking sleeve (3) is used for preventing the plug (2) from being separated from the column groove (101).

2. An aviation plug-in receptacle according to claim 1, characterized in that The locking sleeve (3) includes a rectangular frame (301) fixedly provided on the top of the socket (1), a guide rod (302) fixedly provided between the two inner side walls of the rectangular frame (301), a slider (303) slidably sleeved on the surface of the guide rod (302), a spring (304) connected between the slider (303) and one of the inner side walls of the rectangular frame (301), the spring (304) being sleeved on the surface of the guide rod (302), hinged plates (305) hinged on both sides of the slider (303), a H-shaped cover (306) fixedly provided at the other end of the hinged plate (305), a limiting block (307) fixedly provided at the other end of the H-shaped cover (306), the limiting block (307) being arc-shaped, and the insulating tray (202) abutting against the limiting block (307).

3. An aviation plug-in receptacle according to claim 2, wherein, The limiting block (307) is configured with a circular groove (3071) on the side close to the plug (2), and the circular groove (3071) is matched in size with the insulating tray (202).

4. An aviation plug-in receptacle according to claim 2, wherein, The limiting block (307) is configured with a rectangular gap (3072) at the bottom side and in communication with the circular groove (3071).

5. An aviation plug-in receptacle according to claim 2, wherein, The H-shaped cover (306) is provided with a transparent observation window (3061) in the middle of the top.

6. An aviation plug-in receptacle according to claim 1, wherein, The plug (2) is fixedly provided with a rectangular block (203) at the middle of the side close to the socket (1), and the column groove (101) is configured with a rectangular groove (103) matched with the rectangular block (203).

7. An aviation plug-in receptacle according to claim 1, wherein, The installation plate (4) is fixedly provided on the end of the socket (1) away from the plug (2), and the installation plate (4) is configured with installation holes (401) at the four corners.

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