Wing lamp wire harness butt joint device

Abstract

The utility model discloses a wing lamp wire harness butt joint device which comprises a wing lamp wire harness interface and a wing lamp wire harness plug, the wing lamp wire harness plug is inserted into the side wall of the wing lamp wire harness interface, and buckling structures are symmetrically arranged on the outer walls of the wing lamp wire harness interface and the wing lamp wire harness plug. After butt joint of the wing lamp wire harness is completed, the inner buckle plate and the outer buckle plate can be completely buckled, firm is kept through the inclined protrusions, then reinforcement is conducted through the reinforcing structures, operation is more convenient during disassembly, meanwhile, the reinforcing structures are arranged for reinforcement, butt joint installation of the wing lamp wire harness is firmer, and the wing lamp wire harness is not prone to falling off. The signal is prevented from being interrupted or distorted in the transmission process through double fixation, and normal work of the wing lamp is prevented from being affected.

Description

Technical Field

[0001] The utility model relates to the technical field of wing lamp harness installation, and specifically relates to a wing lamp harness docking device. Background Art

[0002] With the development of the automotive industry, vehicle safety, comfort, and aesthetics are gaining increasing attention, and the role of automotive lighting is becoming increasingly important. As a key component of automotive exterior lighting, wing lights require signal transmission and control via wiring harnesses. Their function is to control the transmission of signals, causing the vehicle's lights to flash and change, alerting the driver and other vehicles to traffic conditions.

[0003] Wing light wiring harnesses must withstand the vibration and impact of driving, requiring high durability. A loose connection can cause signal interruption or distortion during transmission, impacting proper operation of the wing lights. The lights may flash incorrectly or at an erratic rate, affecting the driver's perception of other vehicles and increasing the risk of accidents. Therefore, we propose a wing light wiring harness docking device to ensure a secure and stable connection. Utility Model Content

[0004] The purpose of the present invention is to provide a wing lamp harness docking device to solve the problems raised in the above background technology.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solution: a wing light wiring harness docking device, comprising a wing light wiring harness interface and a wing light wiring harness plug, the side wall of the wing light wiring harness interface is plugged with the wing light wiring harness plug, and the outer walls of the wing light wiring harness interface and the wing light wiring harness plug are symmetrically provided with a snap-fit structure.

[0006] Preferably, the snap-fit structure includes an outer snap plate, one end of which is fixedly connected to the side wall of the wing light wiring harness interface, an inclined protrusion is provided on the inner side of the outer snap plate, an inner snap plate is snapped together at the inclined protrusion of the outer snap plate, and the end of the inner snap plate is fixedly connected to the side wall of the wing light wiring harness plug.

[0007] Preferably, a reinforcement structure is further included, which is assembled on the front side wall of the wing light harness interface, and the two sides are in contact with the side walls of the inner panel.

[0008] Preferably, the reinforcement structure includes side blocks, and the number of the side blocks is two and they are symmetrically arranged. The rear side wall of the side block is fixedly connected to the front side wall of the wing light harness interface. A concave frame is inserted between the inner sides of the two side blocks, and screws are inserted into the side walls of the side blocks. The side blocks are threadedly connected to the concave frame through the screws, and the inner side walls of the concave frame are fitted with the outer wall of the wing light harness interface. Strip blocks are provided at both ends of the side walls of the concave frame, and the side walls of the strip blocks are fixedly connected to the side walls of the inner buckle plate, and the strip blocks and the concave frame are clearance-fitted.

[0009] Compared with the prior art, the beneficial effect of the present invention is that when the wing light harness is docked and installed, a snap-fit structure is provided on the outside, the snap-fit structure is made of flexible plastic material, the outer wall of the inner buckle plate is provided with an inclination angle, and the inner side of the outer buckle plate is also provided with an inclination angle. When the two are fitted together, the inner buckle plate will be completely bent. When the wing light harness is docked, the inner buckle plate and the outer buckle plate will also be completely snapped together, and will be kept firm by the inclined protrusions, and then reinforced by the reinforcement structure, which makes it more convenient to operate during disassembly. At the same time, a reinforcement structure is provided for reinforcement, so that the docking installation of the wing light harness is more secure. The double fixation avoids interruption or distortion of the signal during transmission, thereby preventing the normal operation of the wing light from being affected. BRIEF DESCRIPTION OF THE DRAWINGS

[0010] Figure 1 It is a structural diagram of the utility model;

[0011] Figure 2 for Figure 1 Detailed three-dimensional view of the concave frame;

[0012] Figure 3 for Figure 1 Enlarged detail of the inner gusset plate;

[0013] Figure 4 for Figure 1 Enlarged detail of the medial and lateral masses;

[0014] In the figure: 1. Wing light wiring harness interface; 2. Wing light wiring harness plug; 3. Snap-fit structure; 31. Outer buckle plate; 32. Inner buckle plate; 4. Reinforcement structure; 41. Side block; 42. Concave frame; 43. Bar block; 44. Screw. DETAILED DESCRIPTION

[0015] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0016] See also Figure 1-4 The utility model provides a wing light wiring harness docking device, including a wing light wiring harness interface 1 and a wing light wiring harness plug 2. The side wall of the wing light wiring harness interface 1 is plugged with the wing light wiring harness plug 2, and the outer walls of the wing light wiring harness interface 1 and the wing light wiring harness plug 2 are symmetrically provided with a snap-fit structure 3.

[0017] The snap-fit structure 3 includes an outer snap plate 31, one end of which is fixedly connected to the side wall of the wing light harness interface 1, and an inclined protrusion is provided on the inner side of the outer snap plate 31. An inner snap plate 32 is snapped together at the inclined protrusion of the outer snap plate 31, and the end of the inner snap plate 32 is fixedly connected to the side wall of the wing light harness plug 2.

[0018] It also includes a reinforcement structure 4, which is assembled on the front side wall of the wing light harness interface 1, and has two sides that fit with the side walls of the inner buckle plate 32.

[0019] The reinforcement structure 4 includes side blocks 41. There are two side blocks 41 and they are symmetrically arranged. The rear side wall of the side block 41 is fixedly connected to the front side wall of the wing light harness interface 1. A concave frame 42 is inserted between the inner sides of the two side blocks 41. Screws 44 are inserted into the side walls of the side blocks 41. The side blocks 41 are threadedly connected to the concave frame 42 through the screws 44. The inner side wall of the concave frame 42 fits with the outer wall of the wing light harness interface 1. Strip blocks 43 are provided at both ends of the side wall of the concave frame 42. The side wall of the strip block 43 is fixedly connected to the side wall of the inner buckle plate 32, and the strip block 43 and the concave frame 42 are clearance-fitted.

[0020] Working principle: When the wing light harness is docked and installed, the wing light harness interface 1 and the wing light harness plug 2 are fitted together. Due to the external buckle structure 3, when the wing light harness interface 1 and the wing light harness plug 2 are buckled together, the wing light harness plug 2 drives the inner buckle plate 32 to move. The inner buckle plate 32 is made of plastic flexible material. Since the outer wall of the inner buckle plate 32 is provided with an inclination angle, the inner side of the outer buckle plate 31 is also provided with an inclination angle. When the two are fitted together, the inner buckle plate 32 will bend to a certain extent. When the wing light harness is docked, the inner buckle plate 32 and the outer buckle plate 31 will also be completely buckled together. , and then reinforced by the reinforcement structure 4. Now insert the concave frame 42 from the outside of the buckled wing lamp harness, first fit with the side block 41 on the outer wall of the wing lamp harness interface 1, the side blocks 41 are symmetrically arranged, and the concave frame 42 can be clamped between the side blocks 41. At the same time, it fits with the side wall of the inner buckle plate 32 with a strip block 43 to maintain the limit of the inner buckle plate 32, and then the screws 44 pass through the side block 41 and are threadedly connected to the concave frame 42. Through the external buckling structure 3, it is more convenient to operate during disassembly. At the same time, the reinforcement structure 4 is set for reinforcement, so that the docking installation of the wing lamp harness is more secure.

[0021] Although the embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations may be made to these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A wing light harness docking device, characterized by: The invention comprises a wing light harness interface (1) and a wing light harness plug (2); the side wall of the wing light harness interface (1) is plugged with the wing light harness plug (2); and the outer walls of the wing light harness interface (1) and the wing light harness plug (2) are symmetrically provided with buckle structures (3).

2. The wing light harness docking device according to claim 1, characterized in that: The buckling structure (3) includes an outer buckle plate (31), one end of which is fixedly connected to the side wall of the wing light harness interface (1), an inclined protrusion is provided on the inner side of the outer buckle plate (31), an inner buckle plate (32) is buckled at the inclined protrusion of the outer buckle plate (31), and an end of the inner buckle plate (32) is fixedly connected to the side wall of the wing light harness plug (2).

3. The wing light harness docking device according to claim 2, characterized in that: It also includes a reinforcement structure (4), which is assembled on the front side wall of the wing light harness interface (1), and has two sides that are in contact with the side walls of the inner buckle plate (32).

4. The wing light harness docking device according to claim 3, characterized in that: The reinforcement structure (4) includes side blocks (41), the number of the side blocks (41) is two and they are symmetrically arranged, the rear side wall of the side block (41) is fixedly connected to the front side wall of the wing light harness interface (1), a concave frame (42) is inserted between the inner sides of the two side blocks (41), a screw (44) is inserted into the side wall of the side block (41), the side block (41) is threadedly connected to the concave frame (42) through the screw (44), the inner side wall of the concave frame (42) is in contact with the outer wall of the wing light harness interface (1), and strip blocks (43) are provided at both ends of the side wall of the concave frame (42), the side wall of the strip block (43) is fixedly connected to the side wall of the inner buckle plate (32), and the strip block (43) and the concave frame (42) are clearance-matched.

Images