CN218602814U - Injection molding type female wire harness - Google Patents

Injection molding type female wire harness Download PDF

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Publication number
CN218602814U
CN218602814U CN202221297874.4U CN202221297874U CN218602814U CN 218602814 U CN218602814 U CN 218602814U CN 202221297874 U CN202221297874 U CN 202221297874U CN 218602814 U CN218602814 U CN 218602814U
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China
Prior art keywords
female
wire harness
injection molding
screw thread
moulding plastics
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CN202221297874.4U
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Chinese (zh)
Inventor
梁劲松
熊鹏程
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Shenzhen Xinghuida Science & Technology Co ltd
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Shenzhen Xinghuida Science & Technology Co ltd
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Priority to CN202221297874.4U priority Critical patent/CN218602814U/en
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Abstract

The utility model provides a female first pencil of formula of moulding plastics, include female first, cable and the female first external mold of moulding plastics, female first includes cylindrical shell, is located the socket hole of cylindrical shell front end and is located the terminal of cylindrical shell rear end, the one end of cable is skinned the back and is connected on the terminal, the female first external mold of moulding plastics is for wrapping up the cylindrical shell of female first and the colloid structure in the terminal outside, the tail end of the female first of moulding plastics sets up the screw thread section, install the screw thread lid in the screw thread section, the center of screw thread lid is provided with the through wires hole. The female head in the injection molding type female head wiring harness is selected from a structure formed by cutting a rectangular flange of a traditional universal fixed assembly type aviation socket, then a shell is molded based on the female head, a binding post and a cable are partially wrapped in the shell, and the product is formed after the thread is configured.

Description

Injection molding type female wire harness
Technical Field
The utility model relates to a connector, wire rod, LED display screen technical field, specific theory has related to a female first pencil of formula of moulding plastics.
Background
In summary, the connection between the LED display screen and the power supply is mainly divided into a fixed assembly type and an air-docking type, and the main reasons why the air-docking type becomes a large component part include the following two aspects:
1. the cost can be reduced, after an original LED box body adopts a fixed installation mode, two sets of aviation plugs are needed, and an aerial butt joint mode is changed, one end of a wiring harness can be directly connected with a circuit board, and only one end of the wiring harness is connected through an aviation head, so that only one set of aviation head is needed;
2. install fast, the LED display screen is mostly rented the use temporarily in outdoor application, for example, hold the concert of singing, this just requires that the LED display screen can build fast, and the assembly can be accomplished to a pair of aviation head of aerial butt joint mode through the aerial operation of both hands, and the assembly can be accomplished to a pair of torsion, and fixed Assembly formula then need look for aviation socket's position, still can increase the installation degree of difficulty because of the space restriction.
Air butt joint, as the name suggests, just hang the aircraft nose aloft through the cable, based on this kind of butt joint demand, in the traditional connector selection type of LED display screen, can adopt NEUTRIK company's connector usually, but NEUTRIK company's connector is mostly based on fixed assembly mode design, and waterproof, lead to its structural more unnecessary structure that has, and because of there is always hidden danger in no waterproof design, need increase extra outer protecting product, if tie up isolated rainwater of modes such as sticky tape.
Some connectors with waterproof functions adopt brand-new sealing designs, but the corresponding scenes of the connectors far exceed the industrial requirements of the LED display screen, so that the manufacturing cost is too high, and the cost can be greatly increased when the connectors are applied to the field of LED display screens.
Based on the above problems, those skilled in the art need to modify the conventional aircraft head without waterproof design to obtain relatively good waterproof effect at low cost.
SUMMERY OF THE UTILITY MODEL
The utility model aims at the not enough of prior art to a female first pencil of formula of moulding plastics that waterproof performance is good, low in manufacturing cost, be fit for butt joint in air is provided.
In order to realize the purpose, the utility model discloses the technical scheme who adopts is: the utility model provides a female first pencil of formula of moulding plastics, includes female head, cable and the female first external mold of moulding plastics, female head includes cylindrical shell, is located the socket hole of cylindrical shell front end and is located the terminal of cylindrical shell rear end, the one end of cable is skinned the back and is connected on the terminal, the female first external mold of moulding plastics is for the parcel is in the cylindrical shell of female head and the colloid structure in the terminal outside, the tail end of the female head of moulding plastics sets up the screw thread section, install the screw thread lid in the screw thread section, the center of screw thread lid is provided with the through wires hole.
The female head is a structure formed by cutting a rectangular flange of a universal fixed assembly type aviation socket.
Basically, the female first external mold of moulding plastics is based on the integrative injection moulding structure of female first setting.
Basically, the surface one side of female first external mold of moulding plastics is provided with and aims at the boss.
Basically, the other side of the surface of the injection molding female head outer die is provided with a handshake boss.
Basically, the material of the injection molding female die and the injection molding outer die is PVC.
The type of the universal fixed assembly type aviation socket is one of NAC3MPA-1, NAC3MPB-1 and NAC3 MPX.
Basically, the threaded cover is selected from fittings on universal fixed assembly type aviation sockets with one of the models of NAC3MPA-1, NAC3MPB-1 and NAC3 MPX.
The specification of the cable is RVV3 × 2.5 or RVV3 × 1.5.
The utility model discloses relative prior art has substantive characteristics and progress, specific theory, the utility model discloses there is following advantage:
1. the cylindrical female head is adopted, the wiring terminal and the socket are configured, a flange structure for assembly is not arranged, then an injection molding female head outer mold is arranged on the outer layer, the tail end is provided with the thread and the thread cover, the product consistency is better, the hollow butt joint mode is completely adapted, the structure is free of waste, and the waterproof performance is good due to tight wrapping, and at least reaches IP65.
2. Because the female head is obtained after cutting off the rectangular flange based on traditional aviation socket, and the screw cap is also obtained from the accessory of traditional aviation socket, only need purchase an aviation socket aftertreatment processing of not taking waterproof function in the cost can, the high automation of injection molding process can further reduce cost when batch production for this product cost based on that traditional fixed assembled aviation socket transformation obtained reduces by a wide margin, more is fit for the use in LED display screen field.
3. An alignment boss and a handshake boss are arranged on the outer side of the injection molding female head outer mold and correspond to the corresponding structure box on the plug, and blind plugging operation in the air butt joint process is facilitated.
4. The cable is wrapped up in the screw thread section, and screw cap locking screw thread section, and then with cable locking, avoid the cable to break away from easily, promote product strength.
Drawings
Fig. 1 is a schematic view of the whole structure of the injection molded female wire harness of the present invention.
Fig. 2 is the structure schematic diagram of the utility model discloses the screw cap is got rid of to female first pencil of injection molding formula.
Fig. 3 is a schematic structural diagram of the female head of the present invention.
Fig. 4 is the structure schematic diagram of the universal fixed assembly type aviation socket of the present invention.
Fig. 5 is a schematic view of an application state of the injection molded female harness of the present invention.
In the figure: 1. a female head; 2. a cable; 3. injection molding a female die and an outer die; 4. a universal fixed assembly type aviation socket; 5. a rectangular flange; 6. a binding post; 7. aligning the boss; 8. a handshake boss; 9. a threaded section; 10. a threaded cap; 11. injection molding the female wire harness; 12. injection molding a male wire harness A;13. a control box; 14. an AC to DC power supply; 15. an alternating current electrode; 16. and (4) an injection molding type male wire harness B.
Detailed Description
The technical solution of the present invention will be described in further detail through the following embodiments.
As shown in fig. 1-4, taking as an example a commonly used universal fixed assembly aircraft receptacle 4 of type NAC3MPA-1 from netrik, having a diameter of 23.8mm for the aircraft receptacle body, a rectangular flange 5 of size 31mm 26mm, and a 3 x 2.5rvv circular cable, typically 10.5mm in diameter, for mating with a plug body of 22.8mm.
The manufacturing method comprises the steps of cutting off a rectangular flange 5, leaving a cylindrical shell, a socket hole and a binding post 6 of a female head 1, connecting one end of a cable 2 to the binding post 6 after peeling, integrally molding the cylindrical shell outside the socket hole to one side of the binding post 6 to form the injection molding female head outer mold 3 made of PVC, forming a thread section 9 at the tail end of the injection molding female head to wrap a part of the cable, designing the size of the thread section 9 according to the size of a thread cover at the tail part of an aviation plug NAC3FCA paired with an aviation plug NAC3MPA-1, so that the thread cover 10 can be directly obtained from accessories without manufacturing, screwing the thread cover 10 on the thread section 9 for decoration to form a pairing effect with the aviation plug, and arranging a threading hole in the center of the thread cover 10 for enabling the cable to pass through.
In order to realize blind insertion with an aviation plug, an alignment boss 7 is integrally formed on one side of the surface of the injection molding female head outer mold 3 in an injection molding mode and used for indicating the insertion direction of the plug, and a handle boss 8 is arranged on the other side of the surface of the injection molding female head outer mold and is convenient to push, pull and rotate.
The working principle is as follows:
as shown in fig. 5, the injection-molded female harness 11 and the injection-molded male harness a12, to which the lug is already fitted, are respectively fitted to the control box 13, and the lug is fitted to the ac electrode 15 of the ac-dc power supply 14.
And (3) connecting a plug at one side of the manufactured injection molding type male wiring harness B16 into the injection molding type female wiring harness 11, and connecting the other end into a distribution box.
External current from the block terminal gets into on the female first pencil 11 of formula of moulding plastics through the public first pencil B16 of formula of moulding plastics, and on the electric current passed through the lug and transmitted to exchanging to DC power supply 14 on one side, then directly get into the LED display screen through the inside circuit of box, light this LED display screen.
The other side of the wire bundle enters the connected injection molding type male wire bundle A12, and the next LED box body is prepared to enter in this way, and so on.
Finally, it should be noted that the above detailed description of the preferred embodiments of the present patent application is not limited to the above embodiments, and that various changes and modifications can be made within the knowledge of those skilled in the art without departing from the spirit of the present patent application.

Claims (9)

1. The utility model provides a female first pencil of formula of moulding plastics which characterized in that: including female first (1), cable (2) and the female first external mold (3) of moulding plastics, female first (1) includes cylindrical shell, is located the socket hole of cylindrical shell front end and is located terminal (6) of cylindrical shell rear end, the one end of cable (2) is skinned the back and is connected on terminal (6), the female first external mold (3) of moulding plastics is in for the parcel the cylindrical shell of female first (1) and the colloid structure in terminal (6) outside, the tail end of the female head of moulding plastics sets up screw thread section (9), install screw thread lid (10) on screw thread section (9), the center of screw thread lid (10) is provided with the through wires hole.
2. The injection molded female wire harness of claim 1, wherein: the female head (1) is a structure formed by cutting a rectangular flange (5) of a universal fixed assembly type aviation socket (4).
3. The injection molded female wire harness of claim 2, wherein: the injection molding female head outer mold (3) is an integrated injection molding structure based on the female head (1).
4. An injection molded female wire harness according to any one of claims 1 to 3, wherein: an alignment boss (7) is arranged on one side of the surface of the injection molding female head outer mold (3).
5. The injection molded female wire harness of claim 4, wherein: and a handle boss (8) is arranged on the other side of the surface of the injection molding female head outer mold (3).
6. An injection molded female wire harness according to claim 1, 2, 3 or 5, wherein: the injection molding female head outer mold (3) is made of PVC.
7. The injection molded female wire harness according to claim 2, wherein: the type of the universal fixed assembly type aviation socket (4) is one of NAC3MPA-1, NAC3MPB-1 and NAC3 MPX.
8. The injection molded female wire harness according to claim 7, wherein: the threaded cover (10) is selected from fittings on a universal fixed assembly type aviation socket (4) with one of the models of NAC3MPA-1, NAC3MPB-1 and NAC3 MPX.
9. An injection molded female wire harness according to claim 1, 2, 3 or 5, wherein: the cable has a specification RVV3 x 2.5 or RVV3 x 1.5.
CN202221297874.4U 2022-05-26 2022-05-26 Injection molding type female wire harness Active CN218602814U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202221297874.4U CN218602814U (en) 2022-05-26 2022-05-26 Injection molding type female wire harness

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202221297874.4U CN218602814U (en) 2022-05-26 2022-05-26 Injection molding type female wire harness

Publications (1)

Publication Number Publication Date
CN218602814U true CN218602814U (en) 2023-03-10

Family

ID=85394749

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202221297874.4U Active CN218602814U (en) 2022-05-26 2022-05-26 Injection molding type female wire harness

Country Status (1)

Country Link
CN (1) CN218602814U (en)

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