Three-core aviation plug connector

Abstract

The utility model provides a three-core aviation plug connector, which is applied to the field of connectors and comprises a male seat rubber coating, a male seat plastic shell, a female head inner core, a grounding pin, a male seat female pin, a female head male pin, a female head female pin, a locking fastener, a wire clamp and a female head rubber coating. One side of the male seat rubber coating is an input side, the other side of the male seat rubber coating is a butt joint side, the butt joint side is matched with one side of the female head inner core, the male seat plastic shell is arranged at the connecting position of the male seat rubber coating and the female head inner core, the female head inner core is embedded in the locking fastener, and the male seat rubber coating is matched with the female head inner core. The two ends of the grounding pin and the two ends of the male base female pin are connected into the male base rubber coating and the female head inner core respectively, the female head male pin and the female head female pin are connected with the male base female pin and the grounding pin respectively, and one end of the female head male pin and one end of the female head female pin are inserted into the female head inner core. The technical problems that at present, if contact is poor, signals are prone to being lost, the signals can be interfered in thunderstorm weather, and the signals are unstable are solved.

Description

Technical Field

[0001] This application relates to the field of connector technology, and in particular to a three-core aviation connector. Background Technology

[0002] A three-core connector is a common electrical connector, typically used in power and signal transmission fields. It consists of three metal contacts and is usually used to connect power lines, signal lines, or other types of cables. The design of a three-core connector can ensure the stability and reliability of the electrical connection.

[0003] Current three-core connectors rely on a good contact environment to transmit signals such as audio and data when they are inserted. Poor contact can easily lead to signal loss and interference during thunderstorms, causing signal instability. Utility Model Content

[0004] This application aims to solve the technical problem that poor contact can easily lead to signal loss and interference during thunderstorms, resulting in signal instability, and provides a three-core aviation connector.

[0005] This application employs the following technical means to solve the technical problem:

[0006] A three-core aviation connector includes a male socket with rubber coating, a male socket plastic shell, a female inner core, a grounding pin, a male socket female pin, a female head male pin, a female head female pin, a locking component, a wire clamp, and a female socket with rubber coating.

[0007] One side of the male connector's rubber coating is the input side, and the other side is the mating side. The mating side is adapted to one side of the female connector's inner core. The male connector's plastic shell is located at the connection between the male connector's rubber coating and the female connector's inner core. The female connector's inner core is nested within the locking mechanism. The grounding pin and the male connector's female pin are respectively connected to the male connector's rubber coating and the female connector's inner core. The female connector's male pin and female pin are respectively connected to the male connector's female pin and the grounding pin. One end of the female connector's male pin and female pin is inserted into the female connector's inner core, and the other end of the female connector's male pin and female pin is housed in a wire clamp. The wire clamp is wrapped around the female connector's inner core and is housed within the female connector's rubber coating.

[0008] Furthermore, the male seat rubber coating, the female head inner core, and the locking component all have internal spaces.

[0009] Furthermore, the grounding pin, male-female pin, female-head pin, and female-head male pin are all located within the space.

[0010] Furthermore, the grounding pin is compatible with the female head pin.

[0011] Furthermore, there are two male-pin-female connectors and two female-pin-male connectors, and the male-pin-female connectors and female-pin-male connectors are compatible with each other.

[0012] Furthermore, it also includes a waterproof cover plate and a waterproof rubber ring, wherein the waterproof cover plate is fitted onto the male seat plastic shell and the waterproof rubber ring is fitted onto the outer side wall of the female head inner core.

[0013] Furthermore, the locking mechanism also includes a torsion spring, a snap button, and a pin;

[0014] The buckle button is mounted on the locking element, and the pin passes through the torsion spring and engages with the buckle button and the locking element.

[0015] This application provides a three-core aviation connector with the following advantages: It comprises a male connector with rubber coating, a male connector plastic shell, a female connector inner core, a grounding pin, a male connector female pin, a female connector male pin, a female connector female pin, a locking mechanism, a wire clamp, and a female connector with rubber coating. One side of the male connector with rubber coating is the input side, and the other side is the mating side. The mating side is adapted to one side of the female connector inner core. The male connector plastic shell is located at the connection between the male connector with rubber coating and the female connector inner core. The female connector inner core is nested within the locking mechanism. The grounding pin is connected to the male connector female pin. The two ends of the needle are respectively connected to the male connector's rubber coating and the female connector's inner core. The female connector's male needle and female connector's female needle are respectively connected to the male connector's female needle and the grounding needle. One end of the female connector's male needle and female connector's female needle is inserted into the female connector's inner core, and the other end of the female connector's male needle and female connector's female needle is housed in a wire clamp. The wire clamp is wrapped around the female connector's inner core and housed in the female connector's rubber coating. This design solves the current technical problem that poor contact can easily lead to signal loss and interference during thunderstorms, causing signal instability. Attached Figure Description

[0016] Figure 1 This is an exploded view of the overall structure of one embodiment of the three-core aviation connector of this application.

[0017] The purpose, features, and advantages of this application will be further explained in conjunction with the embodiments and with reference to the accompanying drawings. Detailed Implementation

[0018] It should be understood that the specific embodiments described herein are merely illustrative of this application and are not intended to limit this application.

[0019] The technical solutions in the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only a part of the embodiments of this application, and not all of the embodiments. Based on the embodiments of this application, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the scope of protection of this application.

[0020] It should be noted that the terms "comprising," "including," and "having," and any variations thereof, in the specification, claims, and accompanying drawings of this application, are intended to cover non-exclusive inclusion. For example, a process, method, system, product, or apparatus that includes a series of steps or units is not limited to the listed steps or units, but may optionally include steps or units not listed, or may optionally include other steps or units inherent to these processes, methods, products, or apparatuses. Terms such as "first" and "second" in the claims, specification, and accompanying drawings of this application, as well as relational terms, are used merely to distinguish one entity / operation / object from another entity / operation / object, and do not necessarily require or imply any such actual relationship or order between these entities / operations / objects.

[0021] In this document, the term "embodiment" means that a particular feature, structure, or characteristic described in connection with an embodiment may be included in at least one embodiment of this application. The appearance of this phrase in various places throughout the specification does not necessarily refer to the same embodiment, nor is it a mutually exclusive, independent, or alternative embodiment. It will be explicitly and implicitly understood by those skilled in the art that the embodiments described herein can be combined with other embodiments.

[0022] Reference Appendix Figure 1 This is an exploded view of the structure of a three-core aviation connector in one embodiment of this application;

[0023] A three-core aviation connector includes a male socket with rubber coating 1, a male socket plastic shell, a female inner core 6, a grounding pin 3, a male socket female pin 4, a female male pin 9, a female female pin 8, a locking element 10, a wire clamp 14, and a female socket with rubber coating 15.

[0024] One side of the male connector rubber cover 1 is the input side, and the other side is the mating side. The mating side is adapted to one side of the female connector inner core 6. The male connector plastic shell 5 is located at the connection between the male connector rubber cover 1 and the female connector inner core 6. The female connector inner core 6 is nested in the locking member 10. The two ends of the grounding pin 3 and the male connector female pin 4 are respectively connected to the male connector rubber cover 1 and the female connector inner core 6. The female connector male pin 9 and the female connector female pin 8 are respectively connected to the male connector female pin 4 and the grounding pin 3. One end of the female connector male pin 9 and the female connector female pin 8 is inserted into the female connector inner core 6, and the other end of the female connector male pin 9 and the female connector female pin 8 is housed in the wire clamp 14. The wire clamp 14 is wrapped around the female connector inner core 6 and is housed in the female connector rubber cover 15.

[0025] In this embodiment, the male seat rubber cover 1, the female head inner core 6, and the locking fastener 10 all have internal spaces.

[0026] The grounding pin 3, male and female pins 4, female and female head pins 8, and female and male head pins 9 are all located within the space.

[0027] The grounding pin 3 is compatible with the female head pin 8.

[0028] The number of male-pin female 4 and female-pin male 9 are both 2, and the male-pin female 4 and female-pin male 9 are compatible.

[0029] Specifically, by using a grounding pin 3 and a female connector pin 8 for adaptation, and two male connector pins 4 and a female connector pin 9 for adaptation, the transmission stability between signals is improved.

[0030] It also includes a waterproof cover plate 2 and a waterproof rubber ring 7. The waterproof cover plate 2 is fitted onto the plastic shell of the male seat, and the waterproof rubber ring 7 is fitted onto the outer wall of the inner core 6 of the female head.

[0031] Specifically, it is fixed to the rubber cover 1 of the public seat to serve as a waterproof and dustproof measure.

[0032] The locking component 10 also includes a torsion spring 11, a snap button 12, and a pin 13;

[0033] The buckle button 12 is mounted on the locking member 10, and the pin 13 passes through the torsion spring 11 and engages with the buckle button 12 and the locking member 10.

[0034] Specifically, the locking element 10, along with the buckle button 12, torsion spring 11, and pin 13, allows the user to easily control the connection and separation of the male plastic shell 5 and the female inner core 6.

[0035] Although embodiments of this application have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of this application, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A three-core aviation connector, characterized in that, This includes the male connector with rubber coating, the male connector with plastic shell, the female connector with inner core, the grounding pin, the male connector with female pin, the female connector with male pin, the female connector with female pin, the locking mechanism, the wire clamp, and the female connector with rubber coating. One side of the male connector's rubber coating is the input side, and the other side is the mating side. The mating side is adapted to one side of the female connector's inner core. The male connector's plastic shell is located at the connection between the male connector's rubber coating and the female connector's inner core. The female connector's inner core is nested within the locking mechanism. The grounding pin and the male connector's female pin are respectively connected to the male connector's rubber coating and the female connector's inner core. The female connector's male pin and female pin are respectively connected to the male connector's female pin and the grounding pin. One end of the female connector's male pin and female pin is inserted into the female connector's inner core, and the other end of the female connector's male pin and female pin is housed in a wire clamp. The wire clamp is wrapped around the female connector's inner core and is housed within the female connector's rubber coating.

2. The three-core aviation connector according to claim 1, characterized in that, The male seat rubber coating, the female head inner core, and the locking components all have internal spaces.

3. The three-core aviation connector according to claim 2, characterized in that, The grounding pin, male and female pins, female and female heads, and female and male heads are all located within the space.

4. The three-core aviation connector according to claim 3, characterized in that, The grounding pin is compatible with the female head pin.

5. The three-core aviation connector according to claim 3, characterized in that, The number of male base female pins and female head male pins are both two, and the male base female pins and female head male pins are compatible.

6. The three-core aviation connector according to claim 1, characterized in that, It also includes a waterproof cover plate and a waterproof rubber ring, wherein the waterproof cover plate is fitted onto the plastic shell of the male seat, and the waterproof rubber ring is fitted onto the outer wall of the inner core of the female head.

7. The three-core aviation connector according to claim 1, characterized in that, The locking component also includes a torsion spring, a snap button, and a pin; the snap button is mounted on the locking component, and the pin passes through the torsion spring and engages with the snap button and the locking component.

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