Solar powered aeronautical obstruction light for power transmission towers

Abstract

The utility model discloses a solar aviation obstruction light for power transmission tower relates to aviation obstruction light technical field, including aviation obstruction light, fixed in aviation obstruction light's machine case, fixed in the base and solar panel of machine case lower extreme, solar panel fixed connection is in the inclined plane of right angle's triangle frame, and the right angle side of triangle frame is fixedly connected with the top plate and connecting rod respectively in the lower extreme, and the top plate and connecting rod respectively adhere the upper and lower surface of machine case, and the one end of connecting rod is away from triangle frame and is fixedly connected with first half ring, and the one end of first half ring is away from connecting rod and is fixedly connected with second half ring through bolt, and first half ring and second half ring form the space for the space of the cylindrical barrel of the socket in base. The utility model discloses, through the cooperation setting between triangle frame, horizontal plate, connecting rod, top plate, side plate, first half ring and second half ring, can reduce the amount of bolt installation, is more convenient, stable.

Description

Technical Field

[0001] This utility model relates to the field of aviation obstruction light technology, and more specifically to a solar-powered aviation obstruction light for power transmission towers. Background Technology

[0002] As towering structures, power transmission towers are required by regulations to be equipped with aviation obstruction lights at night or in low-visibility conditions to ensure flight safety. Traditional aviation obstruction lights typically draw power from the power grid, resulting in complex wiring, high installation and maintenance costs, and are difficult to implement in remote areas or locations with inconvenient power supply.

[0003] To address these issues, solar-powered aviation obstruction lights have emerged. In existing technologies, the solar panels of solar-powered aviation obstruction lights are typically mounted by directly fixing them to the top or side of the light body, or by connecting them to the light body via simple brackets. This often requires installing multiple bolts to mount the solar panel brackets, which is rather cumbersome.

[0004] Therefore, it is necessary to propose a solar-powered aviation obstruction light for power transmission towers to solve the above problems. Utility Model Content

[0005] The purpose of this utility model is to solve the problems mentioned in the background art.

[0006] To achieve the above objectives, this utility model specifically adopts the following technical solution:

[0007] A solar-powered aviation obstruction light for power transmission towers includes an aviation obstruction light, a housing fixed under the aviation obstruction light, a base fixed to the lower end of the housing, and a solar panel. The solar panel is fixedly connected to the inclined surface of a right-angled triangular frame. A top plate and a connecting rod are fixedly connected to the upper and lower ends of the right-angled side of the triangular frame, respectively. The top plate and the connecting rod are respectively attached to the upper and lower surfaces of the housing. A first semi-circular ring is fixedly connected to the end of the connecting rod away from the triangular frame. A second semi-circular ring is fixedly connected to the end of the first semi-circular ring away from the connecting rod by bolts. The first and second semi-circular rings form a space for fitting onto a cylindrical tube of the base.

[0008] Furthermore, a horizontal plate is fixedly connected between the triangular frames.

[0009] Furthermore, a side plate is fixedly connected to the end of the triangular frame away from the horizontal plate, and the side plate fits against the side of the chassis.

[0010] Furthermore, the side panel and top panel form a triangular area that fits the corner of the chassis.

[0011] Furthermore, an arc-shaped extension block is fixedly connected to one end of the second semicircular ring facing the first semicircular ring, and an arc-shaped groove is provided on the first semicircular ring for the arc-shaped extension block to be inserted.

[0012] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0013] This utility model, through the cooperative arrangement of the triangular frame, horizontal plate, connecting rod, top plate, side plate, first semicircular ring and second semicircular ring, can reduce the amount of bolt installation, making it more convenient and stable. Attached Figure Description

[0014] Figure 1 This is a three-dimensional schematic diagram of the structure of this utility model.

[0015] Figure 2 This is a three-dimensional schematic diagram of the connection structure excluding the solar panel in this utility model.

[0016] Figure 3 This is a three-dimensional schematic diagram of the connection structure at the triangular frame in this utility model.

[0017] Reference numerals: 1. Aviation obstruction light; 2. Chassis; 3. Base; 4. Solar panel; 5. Triangular frame; 6. Horizontal plate; 7. Connecting rod; 8. Top plate; 9. Side plate; 10. First semicircular ring; 11. Second semicircular ring; 12. Arc-shaped extension block. Detailed Implementation

[0018] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0019] Please see Figures 1 to 3 The aviation obstruction light 1 typically incorporates built-in LED light-emitting units, control circuitry, etc., to emit warning light signals. The housing 2 is fixed below the aviation obstruction light 1 and houses a battery, solar charging controller, drive circuitry, etc., providing stable power and control for the aviation obstruction light 1. The base 3 is fixed to the lower end of the housing 2 and typically has a cylindrical structure for easy installation on the support rod of a power transmission tower or other cylindrical components. The above are all prior art; this application does not improve upon its circuitry and will not describe it further.

[0020] The core of this invention lies in the installation structure of the solar panel 4. The solar panel 4 is fixedly connected to the inclined surface of a right-angled triangular frame 5. The triangular frame 5 is typically made of metal profiles such as aluminum alloy or stainless steel, welded or screwed together. Its right-angled side design allows the solar panel 4 to be installed at a preset fixed tilt angle, which can be optimized according to the geographical latitude of the installation site to maximize the amount of solar radiation received.

[0021] To securely connect the solar panel assembly to the housing 2, a top plate 8 and a connecting rod 7 are fixedly connected to the top and bottom ends of the right-angled sides of the triangular frame 5, respectively. The top plate 8 and the connecting rod 7 are designed to fit tightly against the top and bottom of the housing 2, respectively, and the right-angled sides of the triangular frame 5 also fit against the housing 2. This fitted connection method further increases the stability of the triangular frame 5 and effectively resists wind loads.

[0022] To further enhance the structural strength of the solar panel assembly, preferably, a horizontal plate 6 is fixedly connected between the triangular frames 5. When multiple triangular frames 5 are used to support one or more solar panels, the horizontal plate 6 can connect these triangular frames 5 to form a more robust overall frame, effectively preventing deformation and improving wind resistance.

[0023] To ensure a tighter and more secure fit between the solar panel assembly and the casing 2, preferably, a side plate 9 is fixedly connected to the end of the triangular frame 5 furthest from the horizontal plate 6. The side plate 9 is designed to fit snugly against the side of the casing 2. In this way, in addition to the top plate 8 and connecting rod 7 fitting against the upper and lower surfaces of the casing 2, the side plate 9 provides additional support and positioning, further improving the assembly's shock and wind resistance. Furthermore, the side plate 9 and the top plate 8 together form a triangular area that fits snugly against the corners of the casing 2, suitable for square or rectangular casings, thus achieving a wraparound, tight connection. This makes the combination of the solar panel assembly and the casing 2 more stable and the appearance more streamlined.

[0024] When the triangular frame 5 is installed onto the base 3 of the transmission tower, a convenient and reliable semi-circular ring structure is adopted. A first semi-circular ring 10 is fixedly connected to the end of the connecting rod 7 away from the triangular frame 5. A second semi-circular ring 11 is fixedly connected to the end of the first semi-circular ring 10 away from the connecting rod 7 by bolts. The first semi-circular ring 10 and the second semi-circular ring 11 together form a circular installation space that can fit onto the cylindrical tube of the base 3. By tightening the bolts connecting the first semi-circular ring 10 and the second semi-circular ring 11, the semi-circular ring assembly can tightly grip the cylindrical tube of the base 3, achieving quick and secure installation.

[0025] To further improve the reliability and anti-rotation capability of the semi-circular ring connection, preferably, an arc-shaped extension block 12 is fixedly connected to the end of the second semi-circular ring 11 facing the first semi-circular ring 10, while the first semi-circular ring 10 has an arc-shaped groove for the arc-shaped extension block 12 to be inserted into. During installation, the arc-shaped extension block 12 is inserted into the arc-shaped groove, which ensures that the relative horizontal displacement of the first semi-circular ring 10 and the second semi-circular ring 11 is restricted, thereby achieving pre-installation. Then, the first semi-circular ring 10 and the second semi-circular ring 11 are fixed with bolts to limit their vertical position.

[0026] In practical applications, the aviation obstruction light 1 is connected to the battery and solar charge controller inside the chassis 2 via a cable. The solar panel 4 converts solar energy into electrical energy, which is transmitted to the solar charge controller inside the chassis 2 via the cable. The controller charges the battery and provides a stable power supply to the aviation obstruction light 1. When there is insufficient sunlight, the aviation obstruction light 1 is powered by the battery.

[0027] In terms of material selection, the metal structural components such as the triangular frame 5, horizontal plate 6, connecting rod 7, top plate 8, side plate 9, and semicircular rings 10 and 11 can be made of corrosion-resistant aluminum alloy, stainless steel, or corrosion-resistant carbon steel to adapt to the harsh outdoor environment of high-altitude power transmission towers. The solar panel 4 is selected from high-efficiency crystalline silicon or amorphous silicon solar panels.

[0028] The above are merely preferred embodiments of this utility model and are not intended to limit this utility model. The scope of patent protection of this utility model shall be determined by the claims. Similarly, any equivalent structural changes made based on the description and drawings of this utility model shall also be included within the scope of protection of this utility model.

Claims

1. A solar-powered aviation obstruction light for power transmission towers, comprising an aviation obstruction light, a housing fixed under the aviation obstruction light, a base fixed to the lower end of the housing, and a solar panel, characterized in that: The solar panel is fixedly connected to the inclined surface of a right-angled triangular frame. A top plate and a connecting rod are fixedly connected to the upper and lower ends of the right-angled side of the triangular frame, respectively. The top plate and the connecting rod are respectively attached to the upper and lower surfaces of the chassis. A first semi-circular ring is fixedly connected to the end of the connecting rod away from the triangular frame. A second semi-circular ring is fixedly connected to the end of the first semi-circular ring away from the connecting rod by bolts. The first semi-circular ring and the second semi-circular ring form a space for fitting onto the cylindrical tube of the base.

2. The solar-powered aviation obstruction light for power transmission towers according to claim 1, characterized in that: A horizontal plate is fixedly connected between the triangular frames.

3. A solar-powered aviation obstruction light for power transmission towers according to claim 2, characterized in that: A side plate is fixedly connected to the end of the triangular frame away from the horizontal plate, and the side plate fits against the side of the chassis.

4. A solar-powered aviation obstruction light for power transmission towers according to claim 3, characterized in that: The side panels and top panel form a triangular area that fits the corners of the chassis.

5. A solar-powered aviation obstruction light for power transmission towers according to claim 1, characterized in that: An arc-shaped extension block is fixedly connected to one end of the second semicircular ring facing the first semicircular ring, and an arc-shaped groove is provided on the first semicircular ring for the arc-shaped extension block to be inserted.

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