CN219304077U

CN219304077U - Aviation plug convenient to break-make

Info

Publication number: CN219304077U
Application number: CN202320138549.1U
Authority: CN
Inventors: 胡杰
Original assignee: Shenzhen Benhangben Technology Co ltd
Current assignee: Zhuhai Benhang Technology Co ltd
Priority date: 2023-01-11
Filing date: 2023-01-11
Publication date: 2023-07-04
Anticipated expiration: 2033-01-11

Abstract

The utility model discloses an aviation plug convenient to turn on and off, which comprises an aviation plug, wherein a first insulating plate and a second insulating plate are arranged in an inserting cavity in front of the aviation plug, a plurality of first conductive columns are arranged on the first insulating plate, second conductive columns are arranged right opposite to the first conductive columns on the second insulating plate, a plurality of third conductive columns are arranged at the deepest part of the inserting cavity, first jacks are arranged at one ends of the first conductive columns, second jacks are arranged at one ends of the third conductive columns, one ends of the second conductive columns are inserted into the first jacks, the other ends of the second conductive columns are inserted into the second jacks, and a plurality of first springs are arranged between the second insulating plate and the inner wall of the inserting cavity. The utility model has simple structure, the sealing ring and the second insulating plate push the second conductive column leftwards through the rebound energy of the first spring, so that the second conductive column is pulled out of the second jack, and the power-off can be directly completed, otherwise, the power-on is completed again, and the aviation plug is not required to be detached from the aviation socket, thereby greatly improving the convenience.

Description

Aviation plug convenient to break-make

Technical Field

The utility model relates to the technical field of aviation plugs, in particular to an aviation plug convenient to turn on and off.

Background

Aviation plug is one kind of connector, and is derived from the military industry, so the aviation plug is called simply. Aviation plugs are electromechanical elements that connect electrical lines, and thus their own electrical parameters are a first concern in selecting an aviation plug. Proper selection and use of aviation plugs is an important aspect of ensuring circuit reliability.

At present, aviation plug and aviation socket are generally fixed through threaded connection's mode, and threaded connection's mode is dismantled difficultly, needs rotatory many circles, can't timely outage to after both dismantlements, follow-up reconnection has and needs rotatory many circles, serious influence efficiency.

Disclosure of Invention

The technical problem to be solved by the utility model is to provide the aviation plug convenient to turn on and off, the aviation plug is not required to be detached from the aviation socket, after the pull ring is pulled outwards, the sealing ring can move leftwards, the second insulating plate is driven by the movement of the sealing ring, the second conductive column is separated from the second jack, the power-off is directly completed, and the efficiency is greatly increased.

The utility model is realized by the following technical scheme: the utility model provides an aviation plug convenient to break the power supply, including aviation plug, be equipped with first insulation board and second insulation board in the grafting chamber in aviation plug the place ahead, the outer lane of first insulation board is installed on the internal face in grafting chamber, install many first conductive posts on the first insulation board, the second conductive post is just all installed to first conductive post department to the second insulation board, the third conductive post that is connected with aviation plug internal wire is all installed to the second conductive post department to the deepest in grafting chamber, the one end of first conductive post all is equipped with first jack, the one end of third conductive post all is equipped with the second jack, in second conductive post one end all inserts first jack, the other end all inserts in the second jack, aviation plug's outer lane just is equipped with a plurality of bar mouths in second insulation board department, a plurality of bar mouths are annular structure evenly distributed, aviation plug's outside cover is equipped with the sealing ring that seals the bar mouths, the inner circle face just all installs the connecting rod in bar mouths department, the connecting rod other end all installs on the second insulation board, install a plurality of first sealing rings between the inner wall in second insulation board and grafting chamber, first compression spring all is in a plurality of compression state.

As the preferred technical scheme, the setting element all includes locating lever, the locating piece, second spring and pull ring, be equipped with a plurality of first recesses on the inner circle face of sealing ring, aviation plug's outer wall face is just to first recess department all being equipped with the second recess, first recess and second recess combination form the cylinder chamber, the outer lane face of sealing ring just is just to first recess department all being equipped with the shaft hole, the internal diameter in shaft hole all is less than the internal diameter of first recess, locating lever one end all passes the shaft hole and inserts in the cylinder chamber, other end locating piece fixed connection, the locating piece all sets up in the second recess, the locating lever other end all sets up in the external world, and all be equipped with the mounting hole, the pull ring all passes the mounting hole and installs on the locating lever, the second spring all overlaps on the locating lever, second spring one end all is installed on the locating piece, the other end all is installed on the inner wall face of first recess.

As a preferred solution, both the first insulating plate and the second insulating plate are made of insulating plastic material.

As a preferable technical scheme, a space for the second insulating plate to move is formed between the connecting rod and the strip-shaped opening.

The beneficial effects of the utility model are as follows: the utility model has simple structure, the pull ring can drive the positioning rod and the positioning block after being pulled outwards, after the positioning block moves into the first groove from the second groove, the sealing ring and the second insulating plate can push the second conductive column leftwards through the rebound of the first spring, so that the second conductive column is pulled out of the second jack, the power-off can be directly completed, otherwise, when the sealing ring is pushed rightwards, the second conductive column can be inserted into the second jack, the power-on is completed again, the aviation plug is not required to be detached from the aviation socket, and the efficiency and the convenience are greatly improved.

Drawings

In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly described, it being obvious that the drawings in the following description are only some embodiments of the utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.

FIG. 1 is a schematic diagram of the overall structure of the present utility model;

fig. 2 is a partial enlarged view at a in fig. 1.

Detailed Description

Embodiments of the present utility model are described in detail below, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to like or similar elements or elements having like or similar functions throughout. The embodiments described below by referring to the drawings are illustrative only and are not to be construed as limiting the utility model.

All of the features disclosed in this specification, or all of the steps in a method or process disclosed, may be combined in any combination, except for mutually exclusive features and/or steps.

Any feature disclosed in this specification (including any accompanying claims, abstract and drawings), may be replaced by alternative features serving the same, equivalent or similar purpose, unless expressly stated otherwise. That is, each feature is one example only of a generic series of equivalent or similar features, unless expressly stated otherwise.

As shown in figures 1 and 2, the aviation plug convenient to turn on and off comprises an aviation plug 1, a first insulating plate 2 and a second insulating plate 3 are arranged in an inserting cavity in front of the aviation plug 1, an outer ring of the first insulating plate 2 is installed on the inner wall surface of the inserting cavity, a plurality of first conductive posts 6 are installed on the first insulating plate 2, second conductive posts 5 are installed at the positions, right opposite to the first conductive posts, of the second insulating plate 3, third conductive posts 4 connected with wires inside the aviation plug are installed at the positions, right opposite to the second conductive posts 5, of the deepest positions of the inserting cavity, first inserting holes 7 are formed in one end of the first conductive posts 6, second inserting holes are formed in one end of the third conductive posts 4, one end of the second conductive posts 5 is inserted into the first inserting holes 7, the other end of the second conductive posts are inserted into the second inserting holes, a plurality of strip-shaped openings 8 are formed in the position opposite to the second insulating plate, the plurality of strip-shaped openings are uniformly distributed in an annular structure, sealing rings 9 are installed on the outer side of the aviation plug 1 in a sleeved mode, sealing rings 9 are opposite to the positions opposite to the second insulating plates, sealing rings 13 are installed on the inner rings 13 are installed on the second insulating plates, sealing rings 11 are installed on the inner rings, and the sealing rings 11 are installed on the inner rings 11, and the sealing rings are in a plurality of the sealing rings 11 are installed on the second insulating plates, and are in a state, and the sealing rings are in a state.

In this embodiment, the setting element all includes locating lever 15, locating piece 14, second spring 16 and pull ring 12, be equipped with a plurality of first recesses on the inner circle face of sealing ring 9, aviation plug 1's outer wall face is just to first recess department all being equipped with the second recess, first recess and second recess combination form the cylinder chamber, sealing ring 9's outer circle face just is just to first recess department all being equipped with the shaft hole, the internal diameter in shaft hole all is less than the internal diameter of first recess, locating lever 15 one end all passes the shaft hole and inserts in the cylinder chamber, other end locating piece 14 fixed connection, locating piece 14 all sets up in the second recess, the locating lever 15 other end all sets up in the external world, and all be equipped with mounting hole 17, pull ring 12 all passes the mounting hole and installs on the locating lever, second spring 16 all overlaps and locates on locating lever 15, second spring 16 one end all installs on locating piece 14, the other end all installs on the inner wall face of first recess.

In this embodiment, the first insulating plate 2 and the second insulating plate 3 are made of insulating plastic materials, so that short circuit is avoided and safety is improved.

In this embodiment, a space for the second insulating plate to move is formed between the connecting rod 13 and the strip-shaped opening 8, so that the second insulating plate can move smoothly.

When the power is required to be cut off, the pull ring can be pulled, the positioning rod and the positioning block are driven by the movement of the pull ring, the positioning block is moved out of the second groove, after the positioning of the positioning rod and the positioning block is lost, the second insulating plate is pushed leftwards by the rebound energy of the second spring, the second conductive column is driven by the movement of the second insulating plate and can be directly pulled out of the second jack, so that the power-off operation is completed, otherwise, the second conductive column can be driven to be reinserted into the second jack after the sealing ring is pushed rightwards, so that the power-on operation is completed, and after the first groove and the second groove are communicated again, the positioning block can be reinserted into the second groove by the rebound energy of the second spring, and the sealing ring and the second insulating plate are positioned, so that the aviation plug is not required to be detached from the aviation socket, and convenience is greatly improved;

the positioning block is larger than the shaft hole, so that the positioning column can be separated from the sealing ring by pulling the positioning column, and the loss is avoided.

The foregoing is merely illustrative of specific embodiments of the present utility model, and the scope of the utility model is not limited thereto, but any changes or substitutions that do not undergo the inventive effort should be construed as falling within the scope of the present utility model. Therefore, the protection scope of the present utility model should be subject to the protection scope defined by the claims.

Claims

1. Aviation plug convenient to break-make, its characterized in that: including aviation plug (1), be equipped with first insulating board (2) and second insulation board (3) in the grafting chamber in aviation plug (1) the place ahead, the outer lane of first insulating board (2) is installed on the internal face in grafting chamber, install many first conductive posts (6) on first insulating board (2), second insulation board (3) are just to first conductive post department all install second conductive post (5), the third conductive post (4) that are connected with aviation plug internal wire are all installed to second conductive post (5) in the deepest of grafting chamber, the one end of first conductive post (6) all is equipped with first jack (7), the one end of third conductive post (4) all is equipped with the second jack, second conductive post (5) one end all inserts in first jack (7), the other end all inserts in the second jack, the outer lane face of aviation plug (1) just is equipped with a plurality of bar mouth (8) in second insulation board department, a plurality of bar mouth are annular structure evenly distributed, the outside cover of aviation plug (1) is equipped with mouth seal ring (9) just to second insulation board (13) are just to the connecting rod (13) of first compression spring (13) are all installed in the inner wall (13) between the first compression spring (13) and the other end all is in the state of installing on the first insulation board (13), a plurality of positioning pieces are arranged on the sealing ring (9).

2. The aircraft plug of claim 1, wherein the power on and off is facilitated by: the locating part all includes locating lever (15), locating piece (14), second spring (16) and pull ring (12), be equipped with a plurality of first recesses on the inner race face of sealing ring (9), aviation plug (1)'s outer wall face just is equipped with the second recess in first recess department, first recess and second recess combination form the cylinder chamber, the outer lane face of sealing ring (9) just is equipped with the shaft hole in first recess department, the internal diameter in shaft hole all is less than the internal diameter of first recess, locating lever (15) one end all passes the shaft hole and inserts in the cylinder chamber, other end locating piece (14) fixed connection, locating piece (14) all set up in the second recess, the locating lever (15) other end all sets up in the external world, and all be equipped with mounting hole (17), pull ring (12) all pass the mounting hole and install on the locating lever, second spring (16) all overlaps on locating lever (15), second spring (16) one end all installs on locating piece (14), the other end all installs on the inner wall face of first recess.

3. The aircraft plug of claim 1, wherein the power on and off is facilitated by: the first insulating plate (2) and the second insulating plate (3) are both made of insulating plastic material.

4. The aircraft plug of claim 1, wherein the power on and off is facilitated by: a space for the second insulating plate to move is formed between the connecting rod (13) and the strip-shaped opening (8).