CN221172133U - Solar aviation warning ball - Google Patents

Abstract

The utility model discloses a solar aviation warning ball, and belongs to the technical field of aviation obstruction lights. The solar energy barrier lamp comprises a detachable sphere, wherein the outer surface of the sphere is provided with a reflecting strip and a solar panel, and the solar panel is used for providing power for the aviation barrier lamp. The aviation obstruction light is installed at the spheroid top, is equipped with battery, MCU module and lamp pearl in the aviation obstruction light, MCU module and battery, lamp pearl, solar panel electric connection. The horizontal axis of spheroid is equipped with the fastener that is used for the centre gripping circuit, is equipped with the protection wire cover in the fastener. Still be equipped with wireless communication module and MCU module electric connection in the aviation obstruction beacon, can carry out signal connection networking with a plurality of spheroids that are close apart from through wireless communication module, realize whole synchro control, spheroidal bottom is equipped with the counter weight in order to guarantee aviation obstruction beacon vertical on. The solar panel is used for supplying power, can be arranged on a high-voltage line, an optical cable and a ground wire, and has wide application range; the integral structure is simple, and accurate devices are concentrated in the navigation obstacle lamp, and waterproof performance is strong.

Description

Solar aviation warning ball

Technical Field

The utility model belongs to the technical field of aviation obstruction lights, and particularly relates to a solar aviation warning ball.

Background

At present, more and more aircrafts such as aircrafts, gliders, high-altitude parachuting, flying with luffing, unmanned aerial vehicles, agricultural aircrafts, helicopters and the like are worn, and circuits such as high-voltage wires, optical cables, ground wires and the like are thinner, so that flying objects are difficult to see in a long distance, and collision accidents are easy to occur. For this reason, chinese patent 2022105949506 discloses an induction night-light emitting power transmission line warning ball, as shown in fig. 1, which includes an iron core, a coil, a circuit module, a battery, an electric box, a spherical housing, and an LED light emitting lamp, and when an ac current passes through a power transmission wire, an induced current is generated in the coil of a closed loop; the coil is connected with a rectifying circuit in the circuit module through a lead wire, and charges the storage battery after rectifying and stabilizing voltage; the circuit module is internally provided with a flash MCU module, and the storage battery is connected with the LED luminescent lamp through the flash MCU module to emit pulse light; the LED light-emitting lamp irradiates the spherical shell from the inside to make the spherical shell emit light, so that a warning effect is achieved. The device has the following disadvantages: specific high-voltage wires are needed, and common wires are difficult to use; the installation is not firm and is easy to loosen; the structure is complex, easy to damage and difficult to maintain. Therefore, a solar aviation warning ball is provided to solve the problems.

Disclosure of utility model

The utility model aims to provide a solar aviation warning ball, which aims to solve the problems that the prior line warning ball in the background art needs to be arranged on a specific high-voltage line and is difficult to use in a common line; the installation is not firm and is easy to loosen; complicated structure, easy damage, difficult maintenance and the like. In order to achieve the purpose, the utility model adopts the following technical scheme: the solar aviation warning ball comprises a detachable ball body so as to be conveniently fixed on a cable, wherein a light reflecting strip and a solar panel are arranged on the outer surface of the ball body, and the solar panel is used for providing power for an aviation obstruction light. The aviation obstruction light is installed at the spheroid top, is equipped with battery, MCU module and lamp pearl in the aviation obstruction light, MCU module and battery, lamp pearl, solar panel electric connection. The technical scheme can be installed on lines such as high-voltage lines, optical cables, ground wires and the like, is wide in application, is simple in overall structure, and has strong waterproof performance and strong anti-vibration and anti-interference capabilities when precise devices are concentrated in the aviation obstruction lamp.

Further, the horizontal axis of the sphere is provided with a wire clamp for clamping the line, and a wire protection sleeve is arranged in the wire clamp to protect the line and ensure the fastening connection of the sphere and the line.

More preferably, the aviation obstruction lights are internally provided with a wireless communication module and an MCU module which are electrically connected, and a plurality of spheres with similar distances can be connected and networked through the wireless communication module, so that the integral synchronous control is realized.

Furthermore, the MCU module is electrically connected with the light sensor, and can automatically control the on and off of the aviation obstruction lights under the corresponding light intensity.

More preferably, the sphere is in a polyhedral design, the solar panel and the reflective strips are designed at intervals, and the sphere is in a transparent design so as to realize a multi-angle warning effect.

Further describing the foregoing solution, the aviation obstruction light is on top of a sphere, and a counterweight is provided at the bottom of the sphere to ensure that the aviation obstruction light is vertically up, reduce sway and ensure that the aviation obstruction light is on top.

Compared with the prior art, the solar panel is used for supplying power, can be arranged on lines such as high-voltage lines, optical cables, ground wires and the like, and is widely applicable; the integral structure is simple, the precise devices are concentrated in the navigation obstacle lamp, the waterproof performance is strong, and the anti-vibration and anti-interference capabilities are strong; the design of the multi-face sphere can realize multi-angle warning in the daytime and at night; a plurality of spheres with similar distances can be networked through the wireless communication module, so that the whole synchronous control is realized.

Drawings

FIG. 1 is a schematic diagram of the Chinese patent 2022105949506;

FIG. 2 is a schematic diagram of an embodiment of the present utility model;

FIG. 3 is an exploded view of an embodiment of the present utility model;

Fig. 4 is a schematic circuit diagram according to an embodiment of the present utility model.

Wherein, each reference sign in the figure:

1. A sphere; 11. a reflective strip; 2. a solar panel; 3. aviation obstruction lights; 4. a wire protecting sleeve; 41. a wire clamp; 5. an MCU module; 51. a storage battery; 52. a lamp bead; 53. a wireless communication module; 54. a light sensor.

Detailed Description

In order that the utility model may be readily understood, a more complete description of the utility model will be rendered by reference to the appended drawings. The drawings illustrate preferred embodiments of the utility model. This utility model may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.

The technical scheme of the patent is further described in detail below with reference to the specific embodiments.

As shown in fig. 2, 3 and 4, in order to effectively prevent an aircraft from colliding with high-voltage wires, optical cables and ground wires, the utility model provides a solar aviation warning ball, which comprises a detachable ball body 1 so as to be conveniently fixed on the cable, wherein a reflecting strip 11 and a solar panel 2 are arranged on the outer surface of the ball body 1, and the solar panel 2 is used for providing power for an aviation obstruction lamp 3. The aviation obstruction light 3 is installed at the top of spheroid 1, is equipped with battery 51, MCU module 5 and lamp pearl 52 in the aviation obstruction light 3, MCU module 5 and battery 51, lamp pearl 52, solar panel 2 electric connection. The horizontal axis of the sphere 1 is provided with a wire clamp 41 for clamping a line, and a wire protection sleeve 4 is arranged in the wire clamp 41 to protect the line and ensure that the sphere 1 is fixedly connected with the line. As shown in fig. 4, the aviation obstruction light 3 is further provided with a wireless communication module 53 electrically connected with the MCU module 5, and the wireless communication module 53 can perform signal connection networking on a plurality of spheres 1 with similar distances, so as to realize overall synchronous control. The MCU module 5 is electrically connected with the light sensor 54, and can automatically control the on/off of the aviation obstruction light 3 under the corresponding light intensity.

As shown in FIG. 2, the sphere 1 is in a polyhedral design, the solar panel 2 and the reflective strips 11 are designed at intervals, and the sphere 1 is in a transparent design so as to realize a multi-angle warning effect. Aviation obstruction light 3 is at spheroid 1 top, and the bottom of spheroid 1 is equipped with the counter weight in order to guarantee aviation obstruction light 3 vertical upward, reduces the swing and ensures aviation obstruction light 3 at the top.

The following further illustrates the principles of the present utility model in connection with a mode of use in order to provide a more thorough understanding of the present utility model.

When the wire protection sleeve 4 is installed, the wire protection sleeve 4 is sleeved on the wire, then the ball body 1 is combined, the wire protection sleeve 4 and the wire clamp 41 are locked by using screws, and the aviation obstruction lamp 3 automatically faces upwards because the ball body 1 is provided with a counterweight. After the installation, the aviation obstruction lights 3 are turned on, the solar panel 2 charges the storage battery 51, and when the light sensor 54 senses that the light is weak, the light beads 52 are automatically turned on. In another embodiment, the aviation obstruction lights 3 with the wireless communication module 53 can be remotely controlled through intelligent devices, and can be mutually networked, so that the overall control is convenient.

It will be understood that when an element is referred to as being "fixed to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. In contrast, when an element is referred to as being "directly on" another element, there are no intervening elements present. The terms "vertical," "horizontal," "left," "right," and the like are used herein for illustrative purposes only and are not meant to be the only embodiments, and the terms "upper," "lower," "left," "right," "front," "back," and the like are used herein with reference to the positional relationship of the drawings.

Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this utility model belongs. The terminology used herein in the description of the utility model is for the purpose of describing particular embodiments only and is not intended to be limiting of the utility model. The term "and/or" as used herein includes any and all combinations of one or more of the associated listed items.

The above embodiments are only for illustrating the present utility model, not for limiting the present utility model, and various changes and modifications may be made by one of ordinary skill in the relevant art without departing from the spirit and scope of the present utility model, and therefore, all equivalent technical solutions are also within the scope of the present utility model, and the scope of the present utility model is defined by the claims.

Claims (6)

1. Solar aviation warning ball, including detachable spheroid (1), its characterized in that: the solar energy lamp is characterized in that the outer surface of the sphere (1) is provided with a reflecting strip (11) and a solar panel (2), the top of the sphere (1) is provided with an aviation obstruction lamp (3), a storage battery (51), an MCU module (5) and a lamp bead (52) are arranged in the aviation obstruction lamp (3), and the MCU module (5) is electrically connected with the storage battery (51), the lamp bead (52) and the solar panel (2).

2. The solar aviation warning ball according to claim 1, characterized in that: the horizontal axis of spheroid (1) is equipped with fastener (41) that are used for centre gripping circuit, be equipped with in fastener (41) and protect line cover (4).

3. The solar aviation warning ball according to claim 1, characterized in that: and a wireless communication module (53) is further arranged in the aviation obstruction light (3) and is connected with the MCU module (5).

4. The solar aviation warning ball according to claim 1, characterized in that: the MCU module (5) is electrically connected with the light sensor (54).

5. The solar aviation warning ball according to claim 1, characterized in that: the sphere (1) is in a polyhedral design, the solar panel (2) and the reflective strips (11) are designed at intervals, and the sphere (1) is in a transparent design.

6. The solar aviation warning ball according to any one of claims 1 to 5, characterized in that: the aviation obstruction light (3) is arranged at the top of the sphere (1), and a counterweight is arranged at the bottom of the sphere (1) to ensure that the aviation obstruction light (3) is vertically arranged.