A wiring device for electronic equipment of a model aircraft
By employing a sliding mechanism and limiting groove design in the wiring device for electronic equipment in model aircraft, the problem of multiple wires getting tangled was solved, improving the neatness and practicality of the wires.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- SKYWALKER TECH CO LTD
- Filing Date
- 2025-07-09
- Publication Date
- 2026-06-30
AI Technical Summary
Existing wiring devices for electronic equipment on model aircraft can only fix one wire at a time. When dealing with multiple wires, they are prone to tangling, which reduces the organization and practicality of the wiring.
The wiring device employs two fixed plates and a limiting rod. Through the design of the sliding mechanism and the limiting groove, the slider slides on the limiting rod and is retracted by the spring to fix the wire in the limiting groove. The cooperation of the sliding mechanism and the limiting groove prevents the wire from getting tangled, improving the neatness and practicality of the wiring.
It enables the effective fixing and wiring of multiple sets of wires, avoids tangling, improves the orderliness and neatness of wiring, and enhances practicality.
Smart Images
Figure CN224438371U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the technical field of electronic equipment wiring, specifically to a wiring device for electronic equipment in a model aircraft. Background Technology
[0002] Model airplanes are dynamic aircraft models with flight capabilities. They are usually equipped with a power system (such as an electric motor or a fuel engine) and can be controlled by remote control. Model airplanes are mainly used for display, teaching or experimentation, emphasizing their dynamic functions and flight performance. The electronic equipment inside model airplanes, like that of airplanes, requires wiring.
[0003] For example, Chinese utility model patent CN209658785U discloses a support and fixing device for aircraft electronic wiring, including a lower fixed plate, an upper fixed plate, a lower supporting arc clamping plate, an upper movable arc clamping plate, a slider, and a lifting mechanism. The lower fixed plate and the upper fixed plate are arranged facing each other, and a first sliding groove and a second sliding groove are respectively formed on the facing end faces of the lower fixed plate and the upper fixed plate. The inner arc surfaces of the lower supporting arc clamping plate and the upper movable arc clamping plate are arranged facing each other, and the lower supporting arc clamping plate and the upper movable arc clamping plate are located between the lower fixed plate and the upper fixed plate. The lower supporting arc clamping plate is connected to the lower fixed plate by a slider, one end of which is connected to the outer arc surface of the lower supporting arc clamping plate, and the other end extends into the first sliding groove. The upper movable arc clamping plate is connected to the upper fixed plate by a lifting mechanism, one end of which is connected to the outer arc surface of the upper movable arc clamping plate, and the other end extends into the second sliding groove. This utility model has a simple structure, is easy to operate, has high construction efficiency, is stable and reliable, and is easy to inspect and maintain.
[0004] However, the existing devices can only fix one point of a single wire. When dealing with a large number of wires, repeated installation operations are required. After installation, multiple wires are easily tangled together, which reduces the device's organizedness when wiring and makes it less practical. Utility Model Content
[0005] To solve the above-mentioned technical problems, this utility model provides a wiring device for electronic equipment of a model aircraft that facilitates the wiring and fixing of multiple sets of wires, avoids tangling between wires, improves the orderliness and neatness of wiring, and enhances practicality.
[0006] This utility model discloses a wiring device for electronic equipment on a model aircraft, comprising two fixed plates and a limiting rod. The two fixed plates are fixedly connected by the limiting rod, and multiple wiring mechanisms are provided on the limiting rod. Each wiring mechanism includes two sliders, the outer walls of which are slidably connected to the limiting rod, and each slider is provided with a limiting mechanism.
[0007] The limiting mechanism includes a partition plate, a limiting groove is opened at the top of the slider, the partition plate is rotatably connected to the outer wall of the slider through two rotating plates, the partition plate is located inside the limiting groove, a fixing groove is fixedly installed at the bottom of the limiting groove, and the bottom of the partition plate is fixedly connected to the inner wall of the limiting groove through a spring.
[0008] A sliding mechanism is provided between the two sliders. This model aircraft electronic equipment wiring device uses the sliding mechanism to slide the two opposing sliders under the limit of the limiting rod. The distance between the two sliders is set for different wire lengths. By pressing the partition, the spring is simultaneously driven to retract, and the wire is discharged into the limiting groove through the gap between the partition and the limiting groove. Then, through the opening on the fixing groove, the wire is discharged into the fixing groove for fixing. This facilitates the wiring and fixing of multiple sets of wires, avoids the wires from getting tangled, improves the orderliness and neatness of the wiring, and enhances practicality.
[0009] Preferably, the sliding mechanism includes a bidirectional screw, and multiple vertical plates are fixedly installed on the outer side wall of each fixed plate. The bidirectional screw is rotatably installed between two vertical plates and screwed onto two opposing sliders. Rotary disks are fixedly installed at both ends of the bidirectional screw. By rotating the rotary disks, the bidirectional screw is simultaneously rotated, which in turn drives the sliders to move in opposite directions under the limit of the limiting rod, thereby facilitating the adjustment and fixing of wires of different lengths.
[0010] Preferably, a fixing plate is fixedly installed in the middle area of each of the limiting rods. By installing the fixing plate, the stability of each limiting rod during support operations is improved.
[0011] Preferably, two fixing seats are symmetrically fixedly installed on the outer side wall of the fixing plate, and each fixing seat is fixedly installed with a fixing bolt. The installation of the fixing seats and fixing bolts makes it easy to fix the device on the model airplane.
[0012] Preferably, a baffle is fixedly installed on the outer wall of each of the fixing slots. By installing the baffle, the wires inside the fixing slot are limited to prevent them from coming off inside the fixing slot.
[0013] Preferably, multiple connecting slots are symmetrically provided on the outer side wall of the fixing plate. By providing connecting slots, it is convenient to guide and conceal the wires fixed by the slider.
[0014] Preferably, a top plate is fixedly installed at the top of each of the limiting grooves. By installing the top plate, it is convenient to limit the top of the partition during rotation.
[0015] Compared with the prior art, the beneficial effects of this utility model are as follows: This model aircraft electronic equipment wiring device uses a sliding mechanism to slide two opposing sliders under the limit of a limiting rod. The distance between the two sliders is set for different wire lengths. By pressing the partition, the spring is simultaneously driven to retract, allowing the wire to pass through the gap between the partition and the limiting groove into the limiting groove and through the opening on the fixing groove, thus allowing the wire to be fixed inside the fixing groove. This facilitates the wiring and fixing of multiple sets of wires, avoids tangling between wires, improves the orderliness and neatness of the wiring, and enhances practicality. Attached Figure Description
[0016] Figure 1 This is a three-dimensional structural diagram of the present invention;
[0017] Figure 2 This is a schematic cross-sectional view of the present invention.
[0018] Figure 3 This utility model Figure 2 Enlarged structural diagram of section A in the middle;
[0019] Figure 4 This is a schematic diagram of the connection structure of the limiting rod and slider of this utility model.
[0020] The following are labels in the attached diagram: 1. Fixed plate; 2. Limiting rod; 3. Slider; 4. Limiting groove; 5. Rotating plate; 6. Partition plate; 7. Spring; 8. Fixed groove; 9. Vertical plate; 10. Bidirectional screw; 11. Rotating disk; 12. Fixed disk; 13. Fixed seat; 14. Fixing bolt; 15. Baffle; 16. Connecting groove; 17. Top plate. Detailed Implementation
[0021] To facilitate understanding of this utility model, a more complete description will be given below with reference to the accompanying drawings. This utility model can be implemented in many different forms and is not limited to the embodiments described herein. Rather, these embodiments are provided to make the disclosure of this utility model more thorough and complete.
[0022] The present invention relates to a wiring device for electronic equipment of a model aircraft, comprising two fixed plates 1 and a limiting rod 2. The two fixed plates 1 are fixedly connected by the limiting rod 2, and multiple wiring mechanisms are provided on the limiting rod 2. The wiring mechanism includes two sliders 3, the outer walls of the two sliders 3 are slidably connected to the limiting rod 2, and each slider 3 is provided with a limiting mechanism.
[0023] The limiting mechanism includes a partition 6, a limiting groove 4 is opened at the top of the slider 3, the partition 6 is rotatably connected to the outer wall of the slider 3 through two rotating plates 5, the partition 6 is located inside the limiting groove 4, a fixing groove 8 is fixedly installed at the bottom of the inner side of the limiting groove 4, and the bottom of the partition 6 is fixedly connected to the inner side wall of the limiting groove 4 through a spring 7.
[0024] A sliding mechanism is provided between the two sliders 3. The sliding mechanism includes a bidirectional screw 10. Multiple vertical plates 9 are fixedly installed on the outer side wall of each fixed plate 1. The bidirectional screw 10 is rotatably installed between the two vertical plates 9. The bidirectional screw 10 is screwed to the two opposing sliders 3. Rotary disks 11 are fixedly installed at both ends of the bidirectional screw 10. A fixed disk 12 is fixedly installed in the middle area of each limiting rod 2. Two fixed seats 13 are symmetrically fixedly installed on the outer side wall of the fixed disk 12. A fixing bolt 14 is fixedly installed on each fixed seat 13. A baffle 15 is fixedly installed on the outer side wall of each fixed groove 8. Multiple connecting grooves 16 are symmetrically opened on the outer side wall of the fixed disk 12. A top plate 17 is fixedly installed at the top of each limiting groove 4.
[0025] like Figures 1 to 4 As shown, this utility model discloses a wiring device for electronic equipment on a model aircraft. During operation, rotating the rotating disk 11 simultaneously drives the bidirectional screw 10 to rotate, which in turn drives the slider 3 to move in opposite directions under the limitation of the limiting rod 2. This facilitates adjustment and fixing of wires of different lengths. The distance between the two sliders 3 is set according to the length of different wires. Pressing the partition 6 simultaneously drives the spring 7 to retract, guiding the wire through the gap between the partition 6 and the limiting groove 4 into the limiting groove 4 and through the opening on the fixing groove 8, thus fixing the wire inside the fixing groove 8. The installation of the baffle 15 limits the wire inside the fixing groove 8, preventing the wire from detaching. The installation of the fixing disk 12 improves the stability of each limiting rod 2 during support operations, facilitating the guidance and concealment of the wires fixed by the sliders 3. The installation of the fixing seat 13 and fixing bolts 14 facilitates the fixing of the device onto the model aircraft.
[0026] The above description is only a preferred embodiment of the present utility model. It should be noted that for those skilled in the art, several improvements and modifications can be made without departing from the technical principles of the present utility model, and these improvements and modifications should also be considered within the protection scope of the present utility model.
Claims
1. A model airplane electronic device wiring device, comprising two fixed plates (1) and a limiting rod (2), the two fixed plates (1) are fixedly connected through the limiting rod (2), and a plurality of wiring mechanisms are arranged on the limiting rod (2), characterized in that: The wiring mechanism includes two sliders (3), the outer walls of the two sliders (3) are slidably connected to the limiting rod (2), and each slider (3) is provided with a limiting mechanism; The limiting mechanism includes a partition (6), a limiting groove (4) is opened at the top of the slider (3), the partition (6) is rotatably connected to the outer wall of the slider (3) through two rotating plates (5), the partition (6) is located inside the limiting groove (4), a fixing groove (8) is fixedly installed at the bottom of the inner side of the limiting groove (4), and the bottom of the partition (6) is fixedly connected to the inner side wall of the limiting groove (4) through a spring (7); A sliding mechanism is provided between the two sliders (3).
2. The wiring device for electronic equipment of a model aircraft according to claim 1, characterized in that: The sliding mechanism includes a bidirectional screw (10), and multiple vertical plates (9) are fixedly installed on the outer side wall of each fixed plate (1). The bidirectional screw (10) is rotatably installed between two vertical plates (9). The bidirectional screw (10) is screwed to two opposing sliders (3). Rotary disks (11) are fixedly installed at both ends of the bidirectional screw (10).
3. The wiring device for electronic equipment of a model aircraft according to claim 1, characterized in that: Each of the limiting rods (2) has a fixing plate (12) fixedly installed in the middle area.
4. The wiring device for electronic equipment of a model aircraft according to claim 3, characterized in that: Two fixing seats (13) are symmetrically fixed on the outer side wall of the fixing plate (12), and each fixing seat (13) is fixedly installed with a fixing bolt (14).
5. The wiring device for electronic equipment of a model aircraft according to claim 1, characterized in that: A baffle (15) is fixedly installed on the outer wall of each of the fixed slots (8).
6. The wiring device for electronic equipment of a model aircraft according to claim 3, characterized in that: Multiple connecting grooves (16) are symmetrically opened on the outer side wall of the fixed plate (12).
7. The wiring device for electronic equipment of a model aircraft according to claim 1, characterized in that: Each of the limiting grooves (4) has a top plate (17) fixedly installed at its top.