CN218648221U - Aviation connecting device fast wires - Google Patents
Aviation connecting device fast wires Download PDFInfo
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- CN218648221U CN218648221U CN202223414358.8U CN202223414358U CN218648221U CN 218648221 U CN218648221 U CN 218648221U CN 202223414358 U CN202223414358 U CN 202223414358U CN 218648221 U CN218648221 U CN 218648221U
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- female
- male
- head
- rubber core
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Abstract
The utility model discloses a quick wiring aviation connecting device, which comprises a male head component, a female head component, a first rubber core and a plurality of connecting terminals, wherein the front end of the male head component is detachably connected with the female head component; the female head assembly comprises a female head shell which is a hollow cavity; a female body detachably connected in the female housing; the second rubber core is detachably connected to the female head main body through a second connecting piece; female first binding post's a plurality of connecting terminal respectively fixed the setting be in the core is glued to the second and runs through female first casing. The utility model discloses a public female binding post is fixed respectively to be set up in corresponding gluey core, passes through the connecting piece to two gluey cores again and can dismantle respectively to connect on public head and female head, realizes public head and the convenient connection of female head effectively.
Description
Technical Field
The utility model relates to a connecting device technical field, in particular to quick wiring aviation connecting device.
Background
The connector has various functions, and the aviation connector is one of the connectors, and can be called aviation plug for short; aerospace connectors are used primarily as mating interface elements for various systems and locations to provide transmission of signals and energy. The aviation connector in the prior art generally adopts a screw locking mode for wiring, the structure is single, two metal contact pieces are respectively and fixedly connected to a male head and a female head, and a cable is fixedly connected to the corresponding metal contact pieces in a screw locking mode, so that the connection mode is inconvenient to use; the event provides a quick wiring aviation connecting device for solve the inconvenient problem of aviation connector's public head and female head connection among the prior art.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a quick wiring aviation connecting device to inconvenient problem is connected to public head and female head of aviation connector among the solution prior art.
The utility model relates to a quick wiring aviation connecting device can realize through following technical scheme:
the utility model relates to a rapid wiring aviation connecting device, which comprises a male head component and a female head component which is detachably and electrically connected with the male head component; the public projection assembly comprises a public head main body, a first rubber core, a public head wiring terminal and a first connecting piece, wherein the front end of the public head main body is detachably connected to the female head assembly, the first rubber core is detachably connected to the public head main body through the first connecting piece, and a plurality of connecting terminals of the public head wiring terminal are respectively and fixedly arranged in the first rubber core; the female head assembly comprises a female head shell, a female head main body, a second rubber core, a female head wiring terminal and a second connecting piece, wherein the female head shell is a hollow cavity and is detachably connected with the male head main body; the female head main body is detachably connected in the female head shell; the second rubber core is detachably connected to the female head main body through the second connecting piece; a plurality of connecting terminals of the female terminal connecting terminal are respectively and fixedly arranged in the second rubber core and penetrate through the female terminal shell.
In one embodiment, a first buckle is arranged at the front end of the male head main body, and the male head main body is detachably connected with the female head assembly through the first buckle.
In one embodiment, the female housing includes a main housing and a tailpipe that is removably attached to the main housing, both of which form a hollow cavity.
In one of the embodiments, the upper end of the main casing body is provided with a clamping cavity, a movable buckle is arranged above the clamping cavity, and the first buckle is matched with the movable buckle through the clamping cavity.
In one embodiment, the main housing is detachably connected to the female body and the tail pipe respectively through a thread structure.
In one embodiment, a plurality of first clamping grooves are formed in the rear end of the male head main body in a penetrating mode, a plurality of second buckles are arranged on the first connecting piece and are respectively matched with the corresponding first clamping grooves, and the first rubber core is detachably connected to the male head main body.
In one embodiment, the male terminal comprises a plurality of male plug tubes and a male cable, and a plurality of wire cores on the male cable are electrically connected with the corresponding male plug tubes respectively in a riveting manner; the male plug insertion tube is provided with at least one first elastic sheet, and the at least one first elastic sheet is matched with an elastic sheet hole in the inner wall of the first rubber core.
In one embodiment, a plurality of second clamping grooves are formed in the female head main body in a penetrating mode, a plurality of third clamping buckles are arranged on the second connecting piece and are respectively matched with the corresponding second clamping grooves, and the second rubber core is detachably connected to the female head main body.
In one embodiment, the inner side of the second rubber core is provided with a spring piece cavity; the female terminal connecting terminal comprises a plurality of female contact pins and a female cable, and a plurality of wire cores on the female cable are electrically connected with the corresponding female contact pins in a riveting manner respectively; at least one second elastic sheet is arranged on the female head contact pin, and the at least one second elastic sheet is matched with the elastic sheet cavity.
In one embodiment, a protective sleeve is arranged at the front end of the female contact pin, and the protective sleeve is made of an insulating material.
Compared with the prior art, the utility model relates to a quick wiring aviation connecting device's beneficial effect does:
the utility model relates to a quick wiring aviation connecting device is respectively matched with a spring plate cavity in a corresponding rubber core through spring plates on a male connecting terminal and a female connecting terminal, so that the male connecting terminal and the female connecting terminal are respectively and fixedly arranged in the corresponding rubber core, then the two rubber cores are respectively detachably connected on a male assembly and a female assembly through connecting pieces, and the male assembly and the female assembly are detachably connected, so that the male connecting terminal and the female connecting terminal are electrically connected, the aviation connecting device is electrically conducted without the help of other tools through screw locking connection, and the connection can be carried out without tools, thereby effectively solving the problem that the male connector and the female connector of an aviation connector in the prior art are inconvenient to connect;
the utility model relates to a quick wiring aviation connecting device has ensured safe touch distance through set up insulating external member on female first binding post, has effectively avoided the problem of protection against electric shock, has also guaranteed moreover that the metal contact does not subtract the weak point, with the area of public first contact, has solved the problem of generating heat to a certain extent.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required for the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present invention, and therefore should not be considered as limiting the scope, and that those skilled in the art can also obtain other related drawings based on these drawings without inventive efforts.
Fig. 1 is a schematic perspective view of a quick-wiring aviation connection device of the present invention;
fig. 2 is a schematic diagram showing a separated structure of the quick wiring aviation connection device shown in fig. 1, which includes a male assembly and a female assembly;
fig. 3 is a schematic cross-sectional structure view of the quick-connection aerial connecting device shown in fig. 1;
fig. 4 is an exploded view of the male connection unit of the aerial quick-connect connection device of fig. 2;
fig. 5 is an exploded view of the female head assembly of the quick-connect aerial connection device of fig. 2;
fig. 6 is a schematic structural view of another view angle of the female head assembly of the aerial connection device for quick wiring shown in fig. 2.
The figures are marked by: 10, a male component; 11, a male body; 111, a first buckle; 112, a first card slot; 12, a first rubber core; 13, a male terminal; 131, a male cannula; 1311, a first spring sheet; 132, male cable; 14, a first connecting member; 141, a second buckle; 20, a female component; 21, a female housing; 211, a main housing; 2111, a clamping cavity; 2112, a movable buckle; 212, a tail pipe; 22, a female body; 221, a second card slot; 23, a second rubber core; 231, a spring plate cavity; 24, a female terminal; 241, inserting a pin by a female head; 2411, a second elastic sheet; 2412, protecting the sleeve; 242, a female cable; 25, a second connecting piece; 251, and a third buckle.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some embodiments of the present invention, but not all embodiments. The components of embodiments of the present invention generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations.
Thus, the following detailed description of the embodiments of the present invention, presented in the figures, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. All other embodiments, which can be obtained by a person skilled in the art without making any creative effort based on the embodiments in the present invention, belong to the protection scope of the present invention.
Referring to fig. 1 and fig. 2, the aviation connection device for quick connection of the present invention mainly includes a male assembly 10 and a female assembly 20, wherein the male assembly 10 is detachably and electrically connected to the female assembly 20; specifically, in this embodiment, the male assembly 10 is detachably and electrically connected to the female assembly 20 by a snap-fit manner.
Referring to fig. 2-4, in the present embodiment, the male projection assembly 10 includes a male body 11, a first rubber core 12, a male terminal 13 and a first connector 14; the front end of the male head main body 11 is detachably connected to the female head assembly 20; the first rubber core 12 is a split rubber core and has elasticity, the first rubber core 12 is detachably connected to the male head main body 11 through the first connecting piece 14, and the first rubber core mainly plays a role in insulating and fixing the male head wiring terminal 13; a plurality of connecting terminals of the male terminal 13 are respectively and fixedly arranged in the first rubber core 12.
Referring to fig. 4, in the present embodiment, a first buckle 111 is disposed at a front end of the male body 11, and is detachably connected to the female assembly 20 through the first buckle 111; a plurality of first slots 112 are formed in the rear end of the male body 11 in a penetrating manner, and the first slots 112 are matched with the first connecting member 14 to fix the first rubber core 12 on the male body 11. In this embodiment, the male connection terminal 13 includes a plurality of male insertion tubes 131 and a male cable 132, and a plurality of cores on the male cable 132 are electrically connected to the corresponding male insertion tubes 131 by riveting; the male cannula 131 is provided with at least one first elastic sheet 1311, and the at least one first elastic sheet 1311 is matched with an elastic sheet hole (not shown) on the inner wall of the first rubber core 12, so that the male cannula 131 is respectively and fixedly arranged in the first rubber core 12.
Referring to fig. 4, in this embodiment, a plurality of second fasteners 141 are disposed on the first connecting member 14, and the plurality of second fasteners 141 are respectively matched with the corresponding first locking slots 112 on the male body 11, so as to detachably connect the first rubber core 12 to the male body 11.
Referring to fig. 2, 3 and 5, in the present embodiment, the female assembly 20 includes a female housing 21, a female body 22, a second rubber core 23, a female terminal 24 and a second connector 25; the female head shell 21 is a hollow cavity and is detachably connected with the male head main body 11; the female body 22 is detachably connected in the female housing 21; the second rubber core 23 is a split rubber core and has elasticity, and the second rubber core 23 is detachably connected to the female terminal main body 22 through the second connecting piece 25 and mainly plays a role in insulating and fixing the female terminal 24; female binding post 24's a plurality of connecting terminal respectively fixed the setting in the second is glued the core 23 and is run through female first casing 21.
Referring to fig. 5, in the present embodiment, the female housing 21 includes a main housing 211 and a tail tube 212, the tail tube 212 is detachably connected to the main housing 211, and both of them form a hollow cavity, specifically, the main housing 211 is detachably connected to the female main body 22 and the tail tube 212 respectively through a screw structure; main casing body 211's upper end is provided with joint chamber 211, the top in joint chamber 211 is provided with movable buckle 2112, public first main part 11 is last first buckle 111 passes through joint chamber 211 with the cooperation of activity buckle 2112 realizes public first subassembly 10 with female first subassembly 20 can dismantle the connection.
Referring to fig. 5, in this embodiment, a plurality of second slots 221 are formed in the female body 22 in a penetrating manner, and the second slots 221 are respectively matched with the second connectors 25 to fix the second rubber core 23 on the female body 22.
Referring to fig. 3, 5 and 6, in the present embodiment, an elastic piece cavity 231 is disposed inside the second rubber core 23; the female terminal 24 comprises a plurality of female pins 241 and a female cable 242, a plurality of wire cores on the female cable 242 are electrically connected with the corresponding female pins 241 in a riveting manner, and when the male assembly 10 is connected with the female assembly 20, the plurality of female pins 241 are electrically connected with the corresponding male insertion tubes 131 in a contact manner, so that the electrical conduction of the aeronautical connection device is realized; the female pin 241 is provided with at least one second elastic piece 2411, and the at least one second elastic piece 2411 is matched with the elastic piece cavity 231, so that the plurality of female pins 241 are respectively and fixedly arranged in the second rubber core 23. In this embodiment, a protective cover 2412 made of an insulating material is disposed at the front end of the female pin 241, and the safe touch distance is ensured by the protective cover 2412.
Referring to fig. 5, in this embodiment, a plurality of third fasteners 251 are disposed on the second connecting member 25, and the plurality of third fasteners 251 are respectively matched with the corresponding second fastener grooves 221 on the female main body 22, so as to detachably connect the second rubber core 23 to the female main body 22.
It should be noted that the utility model relates to a quick wiring aviation connecting device passes through the riveting mode respectively the public first cable 132 with a plurality of public first intubate 132 female first cable 242 with a plurality of female first contact pin 241 electrical connection forms public first binding post 13 with female first binding post 24, then through the shell fragment handle public first binding post 13 with female first binding post 24 is fixed respectively in corresponding gluey core, and rethread corresponding connecting piece fixes two gluey cores respectively public first main part 11 female first main part 22 is last, female first casing 21 is installed female first main part 22 is last, last through first buckle 111 with the cooperation of activity buckle 2112 makes public first subassembly 10 with female first subassembly 20 is connected, thereby makes public first binding post 13 with female first binding post 24 electrical connection realizes aviation connecting device's electrical conduction.
The above-mentioned embodiments only represent some embodiments of the present invention, and the description thereof is specific and detailed, but not to be construed as limiting the scope of the present invention. It should be noted that, for those skilled in the art, without departing from the spirit of the present invention, several variations and modifications can be made, which are within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the appended claims.
Claims (10)
1. The aviation connecting device capable of quickly wiring is characterized by comprising a male head assembly and a female head assembly which is detachably and electrically connected with the male head assembly; the male head assembly comprises a male head main body, a first rubber core, a male head wiring terminal and a first connecting piece, wherein the front end of the male head main body is detachably connected to the female head assembly, the first rubber core is detachably connected to the male head main body through the first connecting piece, and a plurality of connecting terminals of the male head wiring terminal are respectively and fixedly arranged in the first rubber core; the female head assembly comprises a female head shell, a female head main body, a second rubber core, a female head wiring terminal and a second connecting piece, wherein the female head shell is a hollow cavity and is detachably connected with the male head main body; the female head main body is detachably connected in the female head shell; the second rubber core is detachably connected to the female head main body through the second connecting piece; a plurality of connecting terminals of the female terminal connecting terminal are respectively and fixedly arranged in the second rubber core and penetrate through the female terminal shell.
2. The aerial quick-connection device as claimed in claim 1, wherein a first snap is provided at a front end of the male body, and the male body is detachably connected to the female body through the first snap.
3. A quick connect aerial connection device as in claim 2 wherein said female housing includes a main housing and a tailpiece removably connected to said main housing, said tailpiece defining a hollow chamber.
4. The aerial connection device of claim 3, wherein a clamping cavity is formed in the upper end of the main casing, a movable buckle is arranged above the clamping cavity, and the first buckle is matched with the movable buckle through the clamping cavity.
5. The aerial quick connect connector assembly of claim 3 wherein said main housing is removably connected to said female body and said tailpipe, respectively, by a threaded connection.
6. The quick-connect aircraft connection device of claim 1, wherein a plurality of first slots are provided through the rear end of the male body; the first connecting piece is provided with a plurality of second buckles, the second buckles are matched with the corresponding first clamping grooves respectively, and the first rubber core is detachably connected to the male head main body.
7. The aviation connection device with the quick wiring function as claimed in claim 1, wherein the male wiring terminal comprises a plurality of male insertion tubes and a male cable, and a plurality of wire cores on the male cable are electrically connected with the corresponding male insertion tubes in a riveting manner respectively; the male plug is provided with at least one first elastic sheet, and the at least one first elastic sheet is matched with the elastic sheet hole in the inner wall of the first rubber core.
8. The quick-connection aviation connection device according to any one of claims 1 to 7, wherein a plurality of second clamping grooves are formed in the female head main body in a penetrating manner; and a plurality of third buckles are arranged on the second connecting piece and are respectively matched with the corresponding second clamping grooves, and the second rubber core is detachably connected to the female head main body.
9. The quick wiring aviation connection device according to any one of claims 1 to 7, wherein a spring plate cavity is arranged on the inner side of the second rubber core; the female terminal wiring terminal comprises a plurality of female contact pins and a female cable, and a plurality of wire cores on the female cable are electrically connected with the corresponding female contact pins in a riveting mode respectively; at least one second elastic sheet is arranged on the female head contact pin, and the at least one second elastic sheet is matched with the elastic sheet cavity.
10. The aerial connection device of claim 9, wherein a protective sleeve is arranged at the front end of the female pin, and the protective sleeve is made of an insulating material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223414358.8U CN218648221U (en) | 2022-12-20 | 2022-12-20 | Aviation connecting device fast wires |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223414358.8U CN218648221U (en) | 2022-12-20 | 2022-12-20 | Aviation connecting device fast wires |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218648221U true CN218648221U (en) | 2023-03-17 |
Family
ID=85502177
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223414358.8U Active CN218648221U (en) | 2022-12-20 | 2022-12-20 | Aviation connecting device fast wires |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218648221U (en) |
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2022
- 2022-12-20 CN CN202223414358.8U patent/CN218648221U/en active Active
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