Aerial plug

Abstract

The utility model discloses an aviation plug, which comprises a shell, an aviation plug core arranged in the shell and a bus connected with the aviation plug core, the aviation plug core comprises at least one core column, the bus comprises at least one branch line, the number of the branch lines does not exceed the number of the core columns, and each branch line is connected with each core column in a one-to-one correspondence manner. The outer surface of the bus is fixedly connected with a fastening sleeve, the shell also internally comprises a covering layer, and the covering layer wraps the fastening sleeve and one end, connected with the bus, of the aviation plug core. According to the utility model, the fastening sleeve is fixedly connected to the bus, and the covering layer which wraps the fastening sleeve and one end, connected with the bus, of the aviation insertion core is manufactured by adopting an injection molding process, so that after the bus is subjected to a tensile force, most of the tensile force is transferred to the fastening sleeve, and the tensile force of the connecting part of the bus and the aviation insertion core is reduced; the bus is effectively prevented from loosening and even falling off, and the stability and reliability of the whole circuit system are ensured.

Description

Technical Field

[0001] This utility model relates to the field of connector technology, and in particular to an aviation connector. Background Technology

[0002] In existing aviation connector designs, while the connection between the wire and the connector core should theoretically remain secure, in practice, the connection often loosens or even detaches when the wire is subjected to tension or external force. This not only affects the stability and reliability of the entire circuit system but may also pose a potential threat to the safe operation of the equipment. Therefore, improving the design of aviation connectors to ensure a secure connection between the wire and the connector core under tension has become an urgent problem to be solved. Utility Model Content

[0003] In view of the shortcomings of existing technology, the purpose of this utility model is to provide an aircraft plug.

[0004] To achieve the above objectives, the technical solution adopted by this utility model is as follows: an aviation connector, comprising a housing, an aviation connector core disposed within the housing, and a bus connected to the aviation connector core, wherein the aviation connector core includes at least one core post, and the bus includes at least one branch line, and the number of branch lines does not exceed the number of core posts, wherein each branch line is connected to each core post in a one-to-one correspondence, characterized in that a fastening sleeve is fixedly connected to the outer surface of the bus, and the housing further includes a covering layer, the covering layer enclosing the fastening sleeve and the end of the aviation connector core connected to the bus.

[0005] Preferably, the bus is covered with a shell cover, which is fitted to one end of the housing, and a rubber ring is provided between the two.

[0006] Preferably, each branch line is welded to each core post in a corresponding manner.

[0007] Preferably, the fastening sleeve is pressed against the outer surface of the bus.

[0008] Preferably, the fastening sleeve is made of copper.

[0009] Preferably, the cover layer is made using an injection molding process.

[0010] The beneficial effects of this utility model are as follows: By fixing a fastening sleeve on the bus and using injection molding to make a covering layer that wraps the fastening sleeve and the end of the aviation plug connected to the bus, most of the tension is transferred to the fastening sleeve when the bus is subjected to tension, reducing the tension at the connection between the bus and the aviation plug, effectively preventing the bus from loosening or even falling off, and ensuring the stability and reliability of the entire circuit system. Attached Figure Description

[0011] Figure 1 This is a schematic diagram of the structure of this utility model. Detailed Implementation

[0012] like Figure 1 As shown, an aviation connector includes a housing 1, an aviation connector core 2 disposed within the housing 1, and a bus 3 connected to the aviation connector core 2. The aviation connector core 2 includes at least one core post 4, and the bus 3 includes at least one branch line 5, wherein the number of branch lines 5 does not exceed the number of core posts 4. Each branch line 5 is connected one-to-one with each core post 4. The bus 3 is characterized by having a fastening sleeve 6 fixedly connected to its outer surface. The housing 1 also includes a covering layer 7, which is manufactured using injection molding. The covering layer 7 encloses the fastening sleeve 6 and the end of the aviation connector core 2 connected to the bus 3. The bus 3 is covered by a housing cover 8, which is fitted to one end of the housing 1, with a rubber ring 9 between them.

[0013] Each branch line 5 is welded to each core post 4 in a corresponding manner.

[0014] The fastening sleeve 6 is pressed against the outer surface of the bus 3.

[0015] The fastening sleeve 6 is made of copper.

[0016] This invention uses a fastening sleeve 6 fixedly connected to the bus 3 and a covering layer 7 made by injection molding to enclose the fastening sleeve 6 and the end of the aviation plug 2 connected to the bus 3. This allows most of the tension on the bus 3 to be transferred to the fastening sleeve 6, reducing the tension at the connection between the bus 3 and the aviation plug 2, effectively preventing the bus 3 from loosening or even falling off, and ensuring the stability and reliability of the entire circuit system.

[0017] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. Those skilled in the art should understand that this utility model is not limited to the above embodiments. The embodiments and descriptions in the specification are merely illustrative of the principles of this utility model. Simple modifications and substitutions made by those skilled in the art without departing from the spirit and scope of this utility model are within its protection scope.

Claims

1. An aircraft connector, comprising a housing, an aircraft connector core disposed within the housing, and a bus connected to the aircraft connector core, wherein the aircraft connector core includes at least one core post, and the bus includes at least one branch line, the number of branch lines not exceeding the number of core posts, wherein each branch line is connected one-to-one to each core post, characterized in that, A fastening sleeve is fixedly connected to the outer surface of the bus, and the housing also includes a covering layer that wraps the fastening sleeve and the end of the connector that is connected to the bus.

2. The aircraft insert as described in claim 1, characterized in that, The bus is covered with a shell cover, which is fitted to one end of the housing, and a rubber ring is provided between the two.

3. The aircraft insert as described in claim 1, characterized in that, Each branch line is welded to each core post in a corresponding manner.

4. The aircraft insert as described in claim 1, characterized in that, The fastening sleeve is pressed against the outer surface of the bus.

5. The aircraft insert as described in claim 4, characterized in that, The fastening sleeve is made of copper.

6. The aircraft insert as described in claim 1, characterized in that, The cover layer is made using an injection molding process.

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