Aviation obstruction beacon assembly structure

Abstract

The utility model discloses an aviation obstruction light assembly structure, which relates to the technical field of aviation obstruction lights and comprises a narrow-beam spotlight assembly, a light guide assembly is arranged above the narrow-beam spotlight assembly, a light-gathering adapter is arranged above the light guide assembly, a light-isolating tube is arranged above the light-gathering adapter, and the light-isolating tube is arranged above the narrow-beam spotlight assembly. A light guide crystal assembly is arranged above the light insulation pipe, the light guide assembly is arranged through light guide fibers and a light guide pipe, the light guide crystal assembly is arranged through refraction light guide crystals, the condensation conversion head is made into a condensation assembly through light guide materials, and the narrow beam spotlight assembly is formed by combining condensation spotlights. The light guide crystal assembly adopts the refraction light guide crystal, the light condensation conversion head is made into the light condensation assembly through the light guide material, and the light condensation conversion head is convenient to install on high and large obstacles, small in light attenuation, high in brightness and good in warning effect.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation obstruction lights, in particular to an aviation obstruction light component structure. Background Art

[0002] Aviation obstruction lights are installed on high-rise buildings, mountain tops and other tall buildings and natural environment carriers. They are used to warn aircraft and aircraft at high altitudes at night to judge the distance. When aircraft fly at low altitudes, they may encounter invisible obstacles at low altitudes due to obstructed vision. Obstruction lights mainly serve as a warning of obstacles, and generally flash intermittently to achieve the warning purpose.

[0003] At present, the existing aviation obstruction lights generally use relatively simple lighting lamps with low brightness and poor warning effect. Therefore, we propose an aviation obstruction light component structure. Utility Model Content

[0004] The utility model aims to provide an aviation obstruction light assembly structure, which has the advantages of high brightness and good warning effect, and solves the problem that the existing aviation obstruction lights generally use relatively simple lighting lamps with low brightness and poor warning effect.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an aviation obstruction light assembly structure, including a narrow beam spotlight assembly, a light guide assembly is arranged above the narrow beam spotlight assembly, a focusing conversion head is arranged above the light guide assembly, a light isolation tube is arranged above the focusing conversion head, and a light guide crystal assembly is arranged above the light isolation tube.

[0006] Preferably, the narrow beam spotlight assembly is formed by combining spotlights.

[0007] Preferably, the light guide crystal assembly is configured using a refractive light guide crystal.

[0008] Preferably, the focusing conversion head is made of a light-guiding material to form a focusing component.

[0009] Preferably, the light guide assembly is provided by optical fibers and light guide tubes.

[0010] Compared with the prior art, the beneficial effects of the utility model are as follows:

[0011] 1. The narrow beam spotlight assembly of the utility model emits a light beam through a light guide assembly, so that the light passes through the light guide assembly into a focusing conversion head. Since the focusing conversion head is made of a focusing structure made of light guide material, the absorbed light is secondary focused and the light beam is emitted into the light isolation tube to ensure that the light beam is not dispersed. At this time, the emitted light beam enters the optical crystal assembly. The optical crystal assembly is made of a crystal with refracting light, so that the absorbed irradiated light is refracted, thereby improving the flashing brightness and area of ​​the aviation obstruction light, achieving a good obstacle warning effect and high recognition.

[0012] 2. The bottom position of the narrow beam spotlight assembly of the utility model can be adjusted according to the installation requirements. The narrow beam spotlight assembly emits a light beam which is adjusted through the light guide assembly and the light guide can be maintained after the position is adjusted. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 This is a schematic diagram of the structure of the first form of the utility model.

[0014] In the figure: 1. narrow beam spotlight assembly; 2. light guide assembly; 3. focusing conversion head; 4. light isolation tube; 5. light guide crystal assembly. DETAILED DESCRIPTION

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

[0016] In the description of the present invention, unless otherwise specified, "multiple" means two or more; the terms "upper", "lower", "left", "right", "inner", "outer", "front end", "rear end", "head", "tail" and the like indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention and simplifying the description, and does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operate in a specific orientation, and therefore cannot be understood as limiting the present invention. In addition, the terms "first", "second", "third" and the like are only used for descriptive purposes and cannot be understood as indicating or implying relative importance.

[0017] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "connected" and "connection" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0018] The narrow beam spotlight assembly 1, light guide assembly 2, focusing conversion head 3, light isolation tube 4 and optical crystal assembly 5 of the present application are all universal standard parts or parts known to those skilled in the art, and their structures and principles can be known to those skilled in the art through technical manuals or conventional experimental methods.

[0019] Embodiment 1

[0020] See also Figure 1 As shown, the utility model provides a technical solution: an aviation obstruction light assembly structure, comprising a narrow beam spotlight assembly 1, a light guide assembly 2 is arranged above the narrow beam spotlight assembly 1, a focusing conversion head 3 is arranged above the light guide assembly 2, a light isolation tube 4 is arranged above the focusing conversion head 3, and a light guide crystal assembly 5 is arranged above the light isolation tube 4;

[0021] The narrow beam spotlight assembly 1 is formed by combining spotlights;

[0022] The light guide crystal component 5 is configured by using a refractive light guide crystal;

[0023] The focusing conversion head 3 is made of a light-guiding material to form a focusing component.

[0024] The technical solution is set up through the above technical solution. Through the setting of the optical waveguide crystal component 5, the absorbed irradiated light is refracted, and the flashing brightness and area of ​​the aviation obstruction light are improved, so as to achieve a good obstacle warning effect with high recognition. Through the setting of the focusing conversion head 3, since the focusing conversion head 3 is made of a focusing structure through light-guiding material, the absorbed light is secondary focused and the light beam is emitted into the light-isolating tube 4 to ensure that the light beam is not dispersed.

[0025] Embodiment 2

[0026] On the basis of embodiment 1, the present invention is as follows Figure 1 As shown, it is disclosed that the light guide component 2 is arranged by optical fibers and light guide tubes.

[0027] The technical solution can adjust the bottom position of the narrow beam spotlight assembly 1 according to the installation requirements through the arrangement of the light guide assembly 2, and the light guide can be maintained after the position is adjusted.

[0028] Working principle: The narrow beam spotlight component 1 is powered on to emit light, and the light beam is guided to the focusing conversion head 3 through the light guide component 2. The focusing conversion head 3 forms a secondary light beam after guiding and focusing the light at the speed of absorption. The light beam passes through the light isolation tube 4 and shines on the optical crystal component 5. The illumination brightness is improved and diffused through the illumination and refraction on the crystal surface, so as to achieve a good warning effect, which is suitable for high installation flexibility.

[0029] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An aviation obstruction light assembly structure, comprising a narrow beam spotlight assembly (1), characterized in that: A light guide assembly (2) is arranged above the narrow beam spotlight assembly (1), a focusing conversion head (3) is arranged above the light guide assembly (2), a light isolation tube (4) is arranged above the focusing conversion head (3), and a light guide crystal assembly (5) is arranged above the light isolation tube (4).

2. The aviation obstruction light assembly structure according to claim 1, characterized in that: The narrow beam spotlight assembly (1) is formed by combining spotlights.

3. The aviation obstruction light assembly structure according to claim 1, characterized in that: The light guide crystal component (5) is arranged using a refractive light guide crystal.

4. The aviation obstruction light assembly structure according to claim 1, characterized in that: The light focusing conversion head (3) is made of a light guiding material to form a light focusing component.

5. The aviation obstruction light assembly structure according to claim 1, characterized in that: The light guide component (2) is arranged by means of optical fibers and light guide tubes.

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