CN211789858U

CN211789858U - Automatic insertion structure of aviation plug

Info

Publication number: CN211789858U
Application number: CN202020369236.3U
Authority: CN
Inventors: 施建昌; 钱毅; 徐东晓; 薛丹丹; 任玉伟; 刘珂; 尚迪
Original assignee: China North Computer Application Technology Research Institute
Current assignee: China North Computer Application Technology Research Institute
Priority date: 2020-03-21
Filing date: 2020-03-21
Publication date: 2020-10-27
Anticipated expiration: 2030-03-21

Abstract

The utility model discloses an automatic insertion structure is inserted by plane, include: a bottom plate provided with at least one through hole; the plug component is fixed on the bottom plate and is matched with the through holes, and one plug component is fixed in each through hole; and at least one vibration motor component fixed on the bottom plate. The utility model discloses an automatic insertion structure is inserted by plane can eliminate to insert by plane plug and insert by plane and have the butt joint error between the socket, operates labour saving and time saving.

Description

Automatic insertion structure of aviation plug

Technical Field

The utility model relates to an aviation plug socket technical field particularly, relates to an aviation plug automatic insertion structure.

Background

At present, when an aviation plug socket of an electronic product is detected, an aviation plug is directly screwed on the aviation plug socket to be detected generally in a manual screwing mode. When a plurality of aerial plug interfaces are arranged on the aerial plug socket, the aerial plug socket can be tested only after the aerial plug connectors are manually screwed one by one, and time and labor are wasted in operation. In the process of manually twisting the aviation plug by hands, the aviation plug and the aviation socket are easily damaged because the aviation plug and the aviation socket have butt joint errors and the manual twisting force cannot be reasonably controlled.

SUMMERY OF THE UTILITY MODEL

In order to solve the problems, the utility model aims to provide an automatic insertion structure is inserted to boat can eliminate to boat and insert and have the butt joint error between plug and the boat socket, operates labour saving and time saving.

The utility model provides an automatic insertion structure is inserted by plane, include:

a bottom plate provided with at least one through hole;

the plug component is fixed on the bottom plate and is matched with the through holes, and one plug component is fixed in each through hole; and

at least one vibration motor component secured to the base plate.

As a further improvement of the present invention, the plug member includes a plug, a base and at least one sleeve, an inner circular hole and at least one outer circular hole are provided on the base, the plug is inserted into the inner circular hole, the sleeve is inserted into the outer circular hole, and the screw passes through the sleeve will the plug member is fixed on the bottom plate.

As a further improvement, the plug is glued through the welding and is laminated in the inner round hole.

As a further improvement of the utility model, the sleeve with the rubber circle is established to the cover between the outer round hole.

As a further improvement of the utility model, three outer round holes are arranged on the base.

As a further improvement of the present invention, the vibration motor part includes a fixing base and a vibration motor, the fixing base is fixed on the bottom plate, and the vibration motor is fixed on the fixing base.

As a further improvement of the utility model, the bottom of the vibrating motor is pasted with EVA foam.

As a further improvement of the present invention, the vibration motor is locked to the fixing base by a screw.

As a further improvement of the utility model, the fixing seat is locked on the bottom plate through a screw.

As a further improvement of the utility model, at least three plug parts are fixed on the bottom plate, and a vibration motor part is fixed on the bottom plate between two adjacent plug parts.

The utility model has the advantages that:

1. the plug is removed from a thread locking shell, and the plugging action is single when the plug is connected with the socket;

2. the rubber ring is deformed irregularly continuously to ensure that the plug swings irregularly to ensure accurate butt joint and eliminate the error of the plug and the socket;

3. the slight vibration of the whole structure is caused by the polarization of the vibration motor in different directions, so that the plug swings along with the deformation of the rubber ring, and the contact pin can be automatically inserted into the jack.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below. It is obvious that the drawings in the following description are only some embodiments of the invention, and that for a person skilled in the art, other drawings can be derived from them without inventive faculty.

Fig. 1 is a schematic structural diagram of an automatic aerial plug-in structure according to an embodiment of the present invention;

fig. 2 is a schematic structural diagram of a plug component according to an embodiment of the present invention;

FIG. 3 is a schematic view of FIG. 2 taken along line D-D;

fig. 4 is a schematic structural diagram of a vibration motor component according to an embodiment of the present invention;

fig. 5 is a schematic view of an automatic inserting structure for aviation plug according to an embodiment of the present invention.

In the figure, the position of the upper end of the main shaft,

01. an automatic aerial plug-in structure; 02. a square tray socket assembly; 1. a base plate; 2. a plug member; 201. a plug; 202. a base; 203. a sleeve; 204. a rubber ring; 205. an inner circular hole; 206. an outer circular hole; 3. a vibration motor component; 301. a vibration motor; 302. a fixed seat; 303. and (3) soaking the EVA in cotton.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.

It should be noted that, if directional indications (such as up, down, left, right, front, and back … …) are involved in the embodiment of the present invention, the directional indications are only used to explain the relative positional relationship between the components, the movement situation, and the like in a specific posture (as shown in the drawing), and if the specific posture is changed, the directional indications are changed accordingly.

In addition, in the description of the present invention, the terms used are for illustrative purposes only and are not intended to limit the scope of the present invention. The terms "comprises" and/or "comprising" are used to specify the presence of stated elements, steps, operations, and/or components, but do not preclude the presence or addition of one or more other elements, steps, operations, and/or components. The terms "first," "second," and the like may be used to describe various elements, not necessarily order, and not necessarily limit the elements. In addition, in the description of the present invention, "a plurality" means two or more unless otherwise specified. These terms are only used to distinguish one element from another. These and/or other aspects will become apparent and those skilled in the art will more readily appreciate the description of the embodiments of the present invention presented in conjunction with the following drawings. The drawings are only for purposes of illustrating the described embodiments of the invention. One skilled in the art will readily recognize from the following description that alternative embodiments of the structures and methods illustrated in the present application may be employed without departing from the principles of the invention.

The embodiment of the utility model provides an automatic insertion structure is inserted to boat, as shown in figure 1, include: a bottom plate 1 provided with at least one through hole; at least one plug component 2 fixed on the bottom plate 1 and matched with at least one through hole, and one plug component 2 is fixed in each through hole; and at least one vibration motor part 3 fixed on the base plate 1. For example, the bottom plate 1 is provided with three through holes, and a plug member 2 is fixed in each through hole.

In an alternative embodiment, as shown in fig. 2, the plug member 2 includes a plug 201, a base 202 and at least one sleeve 203, the base 202 defines an inner circular hole 205 and at least one outer circular hole 206, the plug 201 is inserted into the inner circular hole 205, the sleeve 203 is inserted into the outer circular hole 206, and a screw passes through the sleeve 203 to fix the plug member 2 to the base plate 1. After the sleeve 203 is fixed to the bottom plate 1, the plug 201 is fixedly connected to the base 202, and the sleeve 203 is fixedly connected to the bottom plate 1.

In an alternative embodiment, the plug 201 is fitted into the inner circular hole 205 by means of a welding glue. The plug 201 can be obtained by disassembling the aviation plug and removing the external thread locking shell, and when the plug is connected with the socket, the plugging action is single, and the thread locking shell does not need to be screwed by hands.

In an alternative embodiment, a rubber ring 204 is disposed between the sleeve 203 and the outer circular hole 206. The rubber ring 204 is respectively extruded and sleeved on the sleeve 203 at two sides of the base 202, a gap is formed between the sleeve 203 and the excircle hole 206 of the base 202, and the plug 201 is fixedly connected with the base 202 and is continuously and slightly swung through irregular stress deformation of the rubber ring 204. The rubber ring 204 HAs a thickness slightly larger than the height of the space between the sleeve 203 and the outer circular hole 206 of the base, the rubber ring 204 HAs a slight amount of deformation when the plug member 2 is in a free state, and the hardness of the rubber ring 204 is selected to be between shore 20HA and shore 30 HA.

In an alternative embodiment, the base 202 defines three outer circular apertures 206, and a sleeve 203 is inserted into each of the outer circular apertures 206. For example, as shown in fig. 2, the base 202 is designed like a triangular arc, and three outer circular holes are designed, so that three sleeves are fixed on the bottom plate through three screws, and the base is more stable.

In an alternative embodiment, the vibration motor part 3 includes a fixing base 302 and a vibration motor 301, the fixing base 302 is fixed on the base plate 1, and the vibration motor 301 is fixed on the fixing base 302.

In an alternative embodiment, the bottom of the vibration motor 301 is adhered with EVA foam 303. The polarization of the vibration motor 301 can be directly transmitted to the bottom plate 1 through the fixed seat 302, a gap is formed between the plane of the bottom of the vibration motor 301 and the plane of the fixed seat 302, and the EVA foam 303 is adhered to the bottom of the vibration motor 301 and the fixed seat 302 through double-sided adhesive to fill the gap. The thickness of the EVA foam 303 is slightly larger than the gap between the vibration motor 301 and the fixing seat 302, and the EVA foam 303 has a certain deformation amount after installation, so that support is provided for the vibration motor 301, and noise generated by periodic collision of the vibration motor 301 and the fixing seat 302 is avoided.

In an alternative embodiment, the vibration motor 301 is locked to the holder 302 by screws. For example by 2 screws in fig. 4.

In an alternative embodiment, the fixing base 302 is locked to the base plate 1 by screws. For example by 4 screws in fig. 4.

In an alternative embodiment, as shown in fig. 1, at least three plug members 2 are fixed to the base plate 1, and one vibration motor member 3 is fixed to the base plate 1 between two adjacent plug members 2. A vibration motor part 3 is respectively arranged between two adjacent plug parts 2, and the whole structure is driven to vibrate by the polarization of the vibration motor part 3, so that the rubber ring 204 on the plug part 2 adjacent to the vibration motor generates elastic deformation.

Aviation plug automatic insertion structure when using, as shown in fig. 5, can insert automatic insertion structure 01 and square plate socket subassembly 02 with aviation and combine the use, square plate socket subassembly 02 is as being surveyed the piece, automatic insertion structure 01 is as detecting the piece. The specific structure of the detection piece can be adaptively designed according to the specific structure of the detected piece, for example, three sockets are arranged on the square-disc socket assembly 02, the automatic insertion structure 01 is correspondingly designed into three plug parts 2 corresponding to the three sockets, and one vibration motor part 3 is respectively designed between two adjacent plug parts 2. When the plug part 2 is automatically butted with the socket, the contact pin on the plug part 2 and the jack on the socket as well as the key position on the plug part 2 and the key position on the socket have slight contraposition errors, the whole structure is driven to vibrate by the work of the vibration motor part 3, so that the rubber ring 204 generates elastic deformation, and the plug swings along with the deformation of the rubber ring, so that the contact pin can be automatically inserted into the jack.

In the description provided herein, numerous specific details are set forth. It is understood, however, that embodiments of the invention may be practiced without these specific details. In some instances, well-known methods, structures and techniques have not been shown in detail in order not to obscure an understanding of this description.

Furthermore, those of ordinary skill in the art will appreciate that while some embodiments described herein include some features included in other embodiments, rather than other features, combinations of features of different embodiments are meant to be within the scope of the invention and form different embodiments. For example, in the claims, any of the claimed embodiments may be used in any combination.

It will be understood by those skilled in the art that while the invention has been described with reference to exemplary embodiments, various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.

Claims

1. An automatic insertion structure for an aerial plug, comprising:

a bottom plate (1) provided with at least one through hole;

at least one plug component (2) which is fixed on the bottom plate (1) and is matched with at least one through hole, and one plug component (2) is fixed in each through hole; and

at least one vibration motor component (3) fixed on the base plate (1).

2. An automatic inserting structure for aviation plug according to claim 1, wherein the plug member (2) comprises a plug (201), a base (202) and at least one sleeve (203), the base (202) is provided with an inner circular hole (205) and at least one outer circular hole (206), the plug (201) is inserted into the inner circular hole (205), the sleeve (203) is inserted into the outer circular hole (206), and a screw penetrates through the sleeve (203) to fix the plug member (2) on the bottom plate (1).

3. Aerial automatic insertion structure according to claim 2, characterised in that said plug (201) is applied inside said internal circular hole (205) by means of a welding glue.

4. An automatic inserting structure for aviation plug according to claim 2, wherein a rubber ring (204) is sleeved between the sleeve (203) and the outer circular hole (206).

5. The automatic aerial plug-in structure of claim 2, characterized in that said base (202) is provided with three external circular holes (206).

6. An automatic aerial plug-in structure as claimed in claim 1, characterized in that said vibrating motor part (3) comprises a fixed seat (302) and a vibrating motor (301), said fixed seat (302) being fixed to said base plate (1), said vibrating motor (301) being fixed to said fixed seat (302).

7. The aerial automatic insertion structure according to claim 6, wherein EVA foam (303) is adhered to the bottom of the vibration motor (301).

8. Aerial automatic insertion structure according to claim 6, characterized in that said vibrating motor (301) is locked to said fixed seat (302) by means of screws.

9. An automatic aerial plug-in structure as claimed in claim 6, characterized in that said fixing seat (302) is locked to said base plate (1) by means of screws.

10. An automatic plug-in structure for aviation plug according to claim 1, wherein at least three plug members (2) are fixed on said base plate (1), and a vibration motor member (3) is fixed on said base plate (1) between two adjacent plug members (2).