WO2022215769A1 - Aviation obstruction light comprising multi-functional light-emitting module - Google Patents

Abstract

Provided is an aviation obstruction light. The aviation obstruction light comprises: a base support structure having a curved portion; and a plurality of light-emitting modules coupled to the base support structure, wherein the light-emitting modules each comprise: a first housing in which a light source is seated; a second housing which is coupled to one end of the first housing and includes a lens for condensing light emitted from the light source; and a connector having one end coupled to the other end of the first housing and the other end coupled to the base support structure, so that the first housing is fixed to the base support structure. The base support structure can be divided into a first region in which the curved portion starts and which has a first curvature, a second region in which the curved portion is finished and which has a second curvature, and a third region which is arranged between the first region and the second region and has a third curvature that is greater than the first curvature and the second curvature.

Description

Aviation obstacle light including multifunctional light emitting module

The present invention relates to an aviation obstacle, and more particularly, to an aviation obstacle in which a plurality of light emitting modules are disposed on a base support.

Aviation obstruction lights are intended to notify the presence of high buildings or dangerous objects that may impede flight at night, and are mainly installed in transmission towers, etc.

For safe operation of aircraft, in accordance with Article 83 of the Aviation Act (Installation of Aviation Obstacle Indicators, etc.) Buildings or structures 150 m or more from the distance, overhead lines crossing rivers, valleys or highways 90 m or more, cables, overhead lines, cables, etc. A tower supporting overhead lines and cables installed in the vicinity of a river, valley or highway, or an object with a height of 60 m or more above the surface or water surface, for example, a chimney, a steel tower, a column-shaped object, a frame-type structure, an additional installation on top of a building, or a structure Aviation obstruction lights should be installed on one pylon, transmission tower, tower supporting overhead line, mooring mechanism for mooring at night and when visibility is less than 5 km during the daytime.

For example, in the Republic of Korea Patent Registration No. 10-0903803, all components such as aviation obstacles are accommodated in a single housing, so manufacturing and installation of aviation obstacle lamps is simplified, as well as providing effects such as cost reduction. Aviation obstacles, etc. are disclosed.

In addition, as another example, in Korea Utility Model Registration Publication No. 20-0473501, the installation work is easy and simple because it is installed on the structure by putting it on the structure. Because it is simplified, there is disclosed an aviation obstacle which reduces the risk of an operator.

One technical problem to be solved by the present invention is to provide a high-efficiency aviation obstacle, etc.

Another technical problem to be solved by the present invention is to provide a high-brightness aviation obstacle.

Another technical problem to be solved by the present invention is to provide an aviation obstacle with improved heat dissipation characteristics.

Another technical problem to be solved by the present invention is to provide an aviation obstacle that is easy to maintain and repair.

The technical problem to be solved by the present invention is not limited to the above.

In order to solve the above technical problems, the present invention provides an aviation obstacle, etc.

According to an embodiment, in an aviation obstacle including a base support structure, and a plurality of light emitting structures coupled to the base support, the light emitting structure includes a first housing on which a light source is mounted, and from the light source A light emitting module including a lens for condensing emitted light and including a second housing coupled to the first housing, and a support module coupled to the first housing of the light emitting module, wherein the first housing comprises: a coupling groove recessed from one end of the first housing toward the second housing; , a coupling line disposed between the first guide groove and the second guide groove, wherein the coupling line of the support module is inserted into the coupling groove of the first housing, so that the first housing and the support module are coupled may include being

According to an embodiment, the support module includes first and second sidewalls extending from both sides of the support module in a longitudinal direction of the support module and in a vertical direction of a lower surface of the support module, wherein the first sidewall and between the second sidewalls, the first guide groove, the coupling line, and the second guide groove are sequentially disposed and exposed in the direction of the first guide groove, the coupling line, and the second guide groove The inner side of the first sidewall and the second sidewall may include an inclined shape.

According to an embodiment, the first housing has a tapered shape that increases in diameter from one end to the other end, and when the first housing and the support module are combined, the outside of the first housing is the support module supported by the first sidewall and the second sidewall of

According to an embodiment, the support module includes a fastener protruding from a lower surface of the support module in opposite directions of the first and second sidewalls, and a heat dissipation member, and includes a light emitting structure and a heat dissipation member through the fastener. It may include that the base support is screwed.

According to an embodiment, the fastener includes a first fastener that protrudes in a direction opposite to the first sidewall from a lower surface of the support module, and a first fastener that protrudes in a direction opposite to the second sidewall from a lower surface of the support module. A second fastener may be included, and the heat dissipation member may be disposed between the first fastener and the second fastener.

According to another embodiment, in an aviation obstacle including a base support structure having a curved portion, and a plurality of light emitting modules coupled to the base support, the light emitting module includes a first housing on which a light source is mounted, the A second housing coupled to one end of the first housing and including a lens for condensing light emitted from the light source, and one end coupled to the other end of the first housing, and the other end coupled to the base support, A connector for fixing the first housing to the base support may be included.

According to another embodiment, the base support has a curved portion, wherein the base support includes a first region where the curved portion starts, a second region where the curved portion ends, and a third region disposed between the first region and the second region. The luminance of the light emitting module divided into regions and disposed in the third region may include a luminance higher than that of the light emitting module disposed in the first region and the second region.

According to another embodiment, the light emitting module further includes a reflecting plate disposed in the first housing to surround the light source, wherein the light emitted from the light source is condensed by the reflecting plate and then provided to the lens can do.

According to another embodiment, the other end of the first housing has a multi-step structure in which the size of the diameter decreases as the distance from one end of the first housing increases, and a tapered shape is formed by the multi-step structure. may include having.

According to another embodiment, the connector has a hollow cylindrical shape, a connector housing having a 'U'-shaped opening in a direction from one end to the other end, and one end is coupled to the first housing and the other end is and a connecting member coupled to the connector housing, wherein the connecting member is coupled to rotate from a first direction that is a longitudinal direction of the connecting member to a second direction that is perpendicular to the first direction. .

According to another embodiment, the connection member may include a screw thread coupling with the first housing.

In the aviation obstacle light comprising a base support structure having a curved portion, and a plurality of light emitting modules coupled to the base support, the light emitting module includes a first housing on which a light source is mounted, one end of the first housing and A second housing coupled to and including a lens for condensing the light emitted from the light source, and one end coupled to the other end of the first housing, and the other end coupled to the base support, to form the first housing a connector for securing to a base support, the base support comprising: a first region at which the curvature begins and has a first curvature; a second region at which the curvature ends and has a second curvature; and the first region and the second region. It is disposed between and divided into a third area having a third curvature greater than the first and second curvatures, and the luminance of the light emitting module disposed in the third area is in the first area and the second area. It may include a luminance higher than the luminance of the light emitting module to be disposed. Accordingly, it is easy to maintain and repair, and it is possible to provide an aviation obstacle, etc. having high efficiency and high brightness.

1 is a view for explaining the configuration of a light emitting structure included in the aviation obstacle light according to a first embodiment of the present invention.

2 is a view for explaining a light emitting module included in the aviation obstacle light according to the first embodiment of the present invention.

3 is a view for explaining a support module included in the aviation obstacle light according to the first embodiment of the present invention.

4 is a view for explaining a state in which the support module and the light emitting module included in the aviation obstacle light according to the first embodiment of the present invention are combined.

5 is a view for explaining a state in which the light emitting structure is coupled to the base support included in the aviation obstacle light according to the first embodiment of the present invention.

6 is a view for explaining the lower portion of the base support included in the aviation obstacle light according to the first embodiment of the present invention.

7 is a view for explaining the rear surface of the base support included in the aviation obstacle light according to the first embodiment of the present invention.

8 is a view for explaining aviation obstacles according to a second embodiment of the present invention.

9 is a combined perspective view of a light emitting module included in an aviation obstacle light according to a second embodiment of the present invention.

10 is an exploded perspective view of a light emitting module included in an aviation obstacle light according to a second embodiment of the present invention.

11 is a perspective view of the first housing included in the aviation obstacle light according to the second embodiment of the present invention.

12 is a perspective view of a light source included in an aviation obstacle light according to a second embodiment of the present invention.

13 is a view showing a modified example of the light source included in the aviation obstacle light according to the second embodiment of the present invention.

14 is a perspective view of a reflector included in an aviation obstacle light according to a second embodiment of the present invention.

15 is a view showing a state in which the first housing, the light source, and the reflector included in the aviation obstacle light according to the second embodiment of the present invention are coupled.

16 is a combined perspective view of a connector included in an aviation obstacle light according to a second embodiment of the present invention.

17 is an exploded perspective view of a connector included in an aviation obstacle light according to a second embodiment of the present invention.

18 is a view showing a state in which the first housing and the connector included in the aviation obstacle light according to the second embodiment of the present invention are coupled.

19 is a view showing the movement of the connector included in the aviation obstacle light according to the second embodiment of the present invention.

20 is a view showing a modified example of the ring included in the connector according to the second embodiment of the present invention.

21 is a view illustrating lighting including a light emitting module according to a second embodiment of the present invention.

22 is a view showing a base module and a light emitting module included in the aviation obstacle light according to the first modification of the present invention.

23 is a view showing an aviation obstacle according to a first modified example of the present invention.

24 is a view showing a light emitting module included in an aviation obstacle light according to a second modification of the present invention.

25 is a view showing a light emitting module included in an aviation obstacle light according to a third modified example of the present invention.

26 is a view showing a light emitting module included in an aviation obstacle light according to a fourth modification of the present invention.

27 is a view showing another embodiment of the light emitting module included in the aviation obstacle light according to the first modification of the present invention.

28 is a view showing another embodiment of the light emitting module included in the aviation obstacle light according to the first modification of the present invention.

29 and 30 are views showing another embodiment of an aviation obstacle, etc. according to a first modified example of the present invention.

Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings. However, the technical spirit of the present invention is not limited to the embodiments described herein and may be embodied in other forms. Rather, the embodiments introduced herein are provided so that the disclosed content may be thorough and complete, and the spirit of the present invention may be sufficiently conveyed to those skilled in the art.

In this specification, when a component is referred to as being on another component, it may be directly formed on the other component or a third component may be interposed therebetween. In addition, in the drawings, the thicknesses of the films and regions are exaggerated for effective description of technical contents.

Also, in various embodiments of the present specification, terms such as first, second, third, etc. are used to describe various components, but these components should not be limited by these terms. Accordingly, what is referred to as a first component in one embodiment may be referred to as a second component in another embodiment.

Each embodiment described and illustrated herein also includes a complementary embodiment thereof. In addition, in this specification, 'and/or' is used in the sense of including at least one of the elements listed before and after.

In the specification, the singular expression includes the plural expression unless the context clearly dictates otherwise. In addition, terms such as "comprise" or "have" are intended to designate that a feature, number, step, element, or a combination thereof described in the specification exists, and one or more other features, numbers, steps, or configurations It should not be construed as excluding the possibility of the presence or addition of elements or combinations thereof.

In addition, in the following description of the present invention, if it is determined that a detailed description of a related well-known function or configuration may unnecessarily obscure the gist of the present invention, the detailed description thereof will be omitted.

1 is a view for explaining the configuration of a light emitting structure included in the aviation obstacle light according to the first embodiment of the present invention, Figure 2 is a view for explaining the light emitting module included in the aviation obstacle light according to the first embodiment of the present invention 3 is a view for explaining the support module included in the aviation obstacle light according to the first embodiment of the present invention, and FIG. 4 is the support module included in the aviation obstacle light according to the first embodiment of the present invention; It is a view for explaining the state in which the light emitting module is coupled, and FIG. 5 is a view for explaining the state in which the light emitting structure is coupled to the base support including the aviation obstacle light according to the first embodiment of the present invention, FIG. 6 is this It is a view for explaining the lower part of the base support including the aviation obstacle light according to the first embodiment of the present invention, Figure 7 is a view for explaining the rear surface of the base support including the aviation obstacle light according to the first embodiment of the present invention to be.

Referring to FIG. 1 , the aviation obstacle light according to the first embodiment of the present invention may include a light emitting structure in which a light emitting module 1000 and a supporting module 2000 are combined. Hereinafter, each configuration will be specifically described.

Referring to FIG. 2 , the light emitting module 1000 includes a first housing 1100 on which a light source (not shown) is mounted, and a lens 1200 for condensing the light emitted from the light source, and the first housing ( It may include a second housing coupled to 1100). According to an embodiment, as shown in FIG. 2A , a coupling groove 1100h is formed at one end of the first housing 1100 in a direction from one end of the first housing 110 to the second housing. can be According to an embodiment, the first housing 1100 may have a tapered shape in which a diameter increases from one end to the other.

Referring to FIG. 3 , the support module 2000 includes a first guide groove 2100a and a second guide groove 2100b that extend in the longitudinal direction of the support module 2000 and are spaced apart from each other, and the first guide. A coupling line 2200 disposed between the groove 2100a and the second guide groove 2100b may be included. The coupling line 2200 may be inserted into the coupling groove 1100h of the first housing 1100 . Accordingly, the first housing 1100 and the support module 2000 may be coupled.

According to an embodiment, a plurality of holes may be formed in the coupling line 2200 . For example, as shown in FIGS. 1 and 3 , a first through hole 2000a and a second through hole 2000b may be formed in the coupling line 2200 . The first through hole 2000a may be used to take out a wire connected to the light emitting module 1000 when the light emitting module 1000 and the support module 2000 are coupled. Alternatively, the second through hole 2000b may be used for inserting a screw for more strongly coupling the first housing 1100 to the support module 2000 .

The support module 2000 includes a first sidewall 2500a and a first sidewall 2500a extending from both sides of the support module 2000 in the longitudinal direction of the support module 2000 and in the vertical direction of the lower surface of the support module 2000 . It may include two sidewalls 2500b. Between the first sidewall 2500a and the second sidewall 2500b, the first guide groove 2100a, the coupling line 2200, and the second guide groove 2100b may be sequentially disposed. .

The first sidewall 2500a and the second sidewall 2500b may be divided into inner and outer sides, respectively. The inner side of the first sidewall 2500a and the second sidewall 2500b may be a portion exposed in the direction of the first guide groove 2100a, the coupling line 2200, and the second guide groove 2100b. have. Alternatively, the outside of the first sidewall 2500a and the second sidewall 2500b may be a portion facing the inside and exposed to the outside of the support module 2000 .

According to an embodiment, inner sides of the first sidewall 2500a and the second sidewall 2500b may have an inclined shape. Accordingly, when the first housing 1100 and the support module 2000 are coupled, the outside of the first housing 1100 is the first sidewall 2500a of the support module 2000 and the second It may be supported by the sidewall 2500b.

The support module 2000 may further include first and second fasteners 2300a and 2300b and first and second heat dissipation members 2400a and 2400b. Specifically, the first fastener 2300a may protrude from the lower surface of the support module 2000 in a direction opposite to the first sidewall 2500a. Alternatively, the second fastener 2300b may protrude from the lower surface of the support module 2000 in a direction opposite to the second sidewall 2500b. Through the first and second fasteners 2300a and 2300b, the light emitting structure and a base support to be described later may be screw-coupled to each other.

The first and second heat dissipation members 2400a and 2400b may be disposed between the first and second fasteners 2300a and 2300b. Specifically, for example, the first heat dissipation member 2400a may protrude from the lower surface of the support module 2000 in a direction opposite to the first guide groove 2100a. Alternatively, the second heat dissipation member 2400b may protrude from the lower surface of the support module 2000 in a direction opposite to the second guide groove 2100b. As the surface area of the support module 2000 is increased by the first and second heat dissipating members 2400a and 2400b, the heat dissipation efficiency of the light emitting structure may be improved.

According to an embodiment, the shape of the light emitting structure 1000 may be implemented in various shapes such as a triangle, a square, a pentagon, a cylinder, and a cone, as well as a circle or a sphere. In addition, the light emitting structure 1000 may be composed of various stages such as one stage and three stages as well as two stages, and may be manufactured at one time not by prefabrication but by extrusion. In addition, according to an embodiment, in the case of the lens, a lens in the form of a long band rather than a spherical lens may be implemented in various lens types.

4 to 7 , the light emitting structure to which the light emitting module 1000 and the support module 2000 are coupled may be coupled to the base support 3000 . The base support 3000 is coupled to a power transmission tower, etc., and may be used as an aviation obstacle. According to an embodiment, the base support 3000 may have a coupling part 3100 for being coupled to a power transmission tower, and may be disposed below or above the base support 3000 . In addition, a control box 3200 may be disposed on the rear surface of the base supporter 3000 .

Above, the aviation obstacle according to the first embodiment of the present invention has been described. Hereinafter, an aviation obstacle according to a second embodiment of the present invention will be described.

8 is a view for explaining an aviation obstacle according to a second embodiment of the present invention.

Referring to FIG. 8 , the aviation obstacle light according to the second embodiment of the present invention may include a base support structure (BS), and a plurality of light emitting modules (LM). The plurality of light emitting modules LM may be coupled to the base support BS. That is, the flight obstacle light may be a structure in which the plurality of light emitting modules LM are coupled to the base support BS. As described in the background technology of the invention, the aviation obstacle light can be installed in buildings and structures with a height of 60 m to 150 m or more. For a specific example, the aviation obstacle, etc. may be installed on the top of a building or at the top of a power transmission tower, etc., to notify the presence of a dangerous object that may be an obstacle to aviation.

Hereinafter, with reference to FIGS. 9 to 20, the light emitting module included in the aviation obstacle light according to the first embodiment of the present invention will be described.

9 is a combined perspective view of a light emitting module included in an aviation obstacle light according to an embodiment of the present invention, FIG. 10 is an exploded perspective view of a light emitting module included in an aviation obstacle light according to an embodiment of the present invention, and FIG. A perspective view of a first housing included in an aviation obstacle light according to an embodiment, FIG. 12 is a perspective view of a light source included in an aviation obstacle lamp according to an embodiment of the present invention, and FIG. 13 is an aviation obstacle lamp according to an embodiment of the present invention. 14 is a perspective view of a reflector included in an aviation obstacle light according to an embodiment of the present invention, and FIG. 15 is a first housing including an aviation obstacle lamp according to an embodiment of the present invention, a light source , and a view showing a state in which the reflector is coupled, FIG. 16 is a combined perspective view of a connector included in an aviation obstacle light according to an embodiment of the present invention, and FIG. 17 is a connector included in an aviation obstacle lamp according to an embodiment of the present invention. An exploded perspective view, FIG. 18 is a view showing a state in which the first housing and the connector including the aviation obstacle light according to an embodiment of the present invention are coupled, and FIG. 19 is a connector including the aviation obstacle light according to the embodiment of the present invention It is a view showing movement, and FIG. 20 is a view showing a modified example of a ring included in a connector according to an embodiment of the present invention.

9 and 10 , the light emitting module LM may include a first housing 100 , a second housing 200 , a connector 300 , a reflector 400 , and a light source L . . Hereinafter, each configuration will be described.

11 to 15 , the first housing 100 may include an empty space therein. The reflective plate 400 and the light source L, which will be described later, may be seated in the empty space. That is, the reflecting plate 400 and the light source L, which will be described later, may be seated inside the first housing 100 . One end of the first housing 100 may be coupled to a second housing 200 to be described later. On the other hand, the other end of the first housing 100 may be coupled to a connector 300 to be described later.

According to an embodiment, the other end of the first housing 100 may have a multi-step structure. For example, as shown in FIG. 4 , the other end of the first housing 100 may have a structure in which first to fifth stages 110 , 120 , 130 , 140 , and 150 are stacked. . The diameters of the first to fifth stages 110 , 120 , 130 , 140 , and 150 may be different from each other. Specifically, the diameter of the second end 120 may be larger than the diameter of the first end 110 . A diameter of the third end 130 may be greater than a diameter of the second end 120 . A diameter of the fourth end 140 may be greater than a diameter of the third end 130 . A diameter of the fifth end 150 may be greater than a diameter of the fourth end 140 .

The diameter of the other end of the first housing 100 may decrease as the distance from one end of the first housing 100 increases. That is, in a direction away from one end of the first housing 100 , the fifth end 150 , the fourth end 140 , the third end 130 , the second end 120 , and the first end 110 may have a sequentially stacked structure. Accordingly, the other end of the first housing 100 may have a tapered shape due to the multi-stage structure. In this case, the connector 300 to be described later may be coupled to the first end 110 .

As the other end of the first housing 100 has a multi-stage structure as described above, heat generated by the light source L disposed inside the first housing 100 may be effectively dissipated. Due to this, durability and reliability of the light source L disposed inside the first housing 100 may be improved.

More specifically, although the LED (Light Emitting Diode) lamp is mainly used as the light source (L) used for aviation obstacles, the LED lamp has a disadvantage in that it is vulnerable to heat. However, as described above, since the other end of the first housing 100 has a heat dissipation structure through a multi-stage structure, heat generated from the light source L disposed inside the first housing 100 is effectively dissipated. can be dissipated. Accordingly, durability and reliability of the light source L disposed inside the first housing 100 may be improved.

As described above, the light source L may include an LED lamp and be disposed in the first housing 100 . According to an embodiment, the light source L may include a plurality of LED lamps as shown in FIG. 6 .

According to an embodiment, an electric wire (not shown) is connected to one side of the light source L, and power may be supplied through the electric wire. In addition, when the light source L is disposed in the first housing 100 , a through hole (not shown) is formed in the first housing 100 so that the electric wire connected to the light source L exits to the outside. can be formed.

The reflector 400 may be disposed in the first housing 100 and surround the light source L. Accordingly, the light emitted from the light source L may be condensed by the reflective plate 400 .

Unlike the above, according to another embodiment, the reflection plate 400 may be excluded from the configuration included in the light emitting module LM. That is, the light source L may be disposed in the first housing 100 without the reflection plate 400 . In this case, the light condensing degree of the light emitting module 400 may be improved.

More specifically, the light emitted from the light source L may be condensed through a lens included in the second housing 200 to be described later. However, when the reflective plate 400 is seated in the first housing 100 , the light emitted from the light source L is condensed by the reflective plate 400 and then the second housing 200 to be described later is It can be condensed again through the containing lens. In this case, there may be a problem in that the condensing degree of the light emitted from the light source L is reduced. According to an embodiment, the lens may be provided in various shapes, such as a circular shape or a rectangular shape. That is, the shape of the lens is not limited.

On the other hand, when the light source L is seated in the first housing 100 without the reflection plate 400 , the light emitted from the light source L includes a lens included in the second housing 200 to be described later. It can be condensed through In this case, compared to the case in which the light condensed through the reflective plate 400 is condensed again through the lens, the condensing degree of the light emitted from the light source L may be improved.

The second housing 200 may include a lens (not shown). According to an embodiment, the lens may be disposed at one end of the second housing 200 . In this case, the other end of the second housing 200 may be coupled to the first housing 100 . In addition, in a state in which the light source L and the reflector 400 are seated in the first housing 100 , the first housing 100 and the second housing 200 may be coupled. Accordingly, the light source L and the reflection plate 400 may be protected from external physical and chemical damage by the first housing 100 and the second housing 200 . In addition, the light emitted from the light source L may be condensed through the lens.

16 to 19 , the connector 300 may include a connector housing 310 , a connection member 320 , a ring 330 , and an elastic member 340 .

The connector housing 310 may have a hollow cylindrical shape. Through the hollow of the connector housing 310 , an electric wire protruding to the outside of the first housing 100 may pass through.

According to an embodiment, an opening may be formed at one end of the connector housing 310 . For example, the opening may be formed in a direction from one end of the connector housing 310 to the other end, and may have a 'U' shape. That is, the opening may have a shape in which a valley is formed between sidewalls spaced apart from each other. In this case, the inside of the connector housing 310 may be exposed to the outside through the valley. Alternatively, a screw thread is formed at the other end of the connector housing 310 and may be coupled to the base support BS through this.

The connection member 320 may be coupled to the connector housing 310 and the first housing 100 . According to an embodiment, one end of the connection member 320 may be connected to the connector housing 310 , and the other end of the connection member 320 may be coupled to the first housing 100 .

According to an embodiment, one end of the connection member 320 may be coupled to the opening of the connector housing 310 . More specifically, the connecting member 320 may have a branched shape from a branch as shown in FIG. 10 , and the branched portion may be coupled to a sidewall of the opening. For example, the sidewall of the opening may be coupled to surround the diverging portion of the connecting member 320 . In this case, the connecting member 320 may be rotated from the first direction to the second direction through the opening. The first direction may be a longitudinal direction of the connecting member 320 . For example, the first direction may be the X-axis direction of FIG. 10 . Alternatively, the second direction may be a direction perpendicular to the first direction. For example, the second direction may be the Y-axis direction of FIG. 10 .

The ring 330 and the elastic member 340 may be disposed inside the connector housing 310 . More specifically, the ring 330 may be disposed between the connecting member 320 and the elastic member 340 . For example, the elastic member 340 may be a spring.

When the connection member 320 is rotated from the first direction (X-axis direction) to the second direction (Y-axis direction), pressure may be applied to the elastic member 340 by the connection member 320 . have. That is, the elastic member 340 may be pressed by the connecting member 320 . Accordingly, the elastic member 340 may be contracted. Alternatively, when the connecting member 320 is not rotated, the elastic member 340 may provide an elastic force to the connecting member 320 . Accordingly, the connection member 320 may be maintained in a fixed state without being rotated.

The ring 330 may serve to increase the contact area between the connection member 320 and the elastic member 340 . That is, when the connecting member 320 and the elastic member 340 are in direct contact without the ring 330 , the contact area between the connecting member 320 and the elastic member 340 may be relatively narrow. have. Accordingly, when the connecting member 320 is rotated, the elastic member 340 is separated from the connecting member 320 while pressure is applied to the elastic member 340 from the connecting member 320 . phenomenon may occur. However, by disposing the ring 330 between the connecting member 320 and the elastic member 340, the separation phenomenon of the elastic member 340 in the process of the connecting member 320 being rotated can be prevented. have.

According to an embodiment, the ring 330 may include a plurality of grooves GV as shown in FIG. 20 . In this case, the connecting member 320 may be coupled to the groove GV. Accordingly, the connecting member 320 may be more stably coupled to the ring 330 , and in a state in which the connecting member 320 is not rotated, the position may be more stably fixed.

That is, the connector 300 may connect the first housing 100 and the base structure BS. In this case, as the connection member 320 is rotated from the first direction (X-axis direction) to the second direction (Y-axis direction) as described above, the first housing 100 is also the first It may rotate in the second direction (Y-axis direction) from the direction (X-axis direction). In addition, as the connector 300 is threadedly coupled to the base structure BS, the connector 300 may rotate in the first direction (X-axis direction) in a clockwise or counterclockwise direction. Accordingly, the first housing 100 may also be rotated clockwise or counterclockwise in the first direction (X-axis direction).

As a result, when the light emitting module LM is coupled to the base support BS, it may be rotated in various directions by the connector 300 . Accordingly, the range in which the light emitted from the light emitting module LM is irradiated can be variously controlled.

Referring back to FIG. 8 , the base support BS may have a curved portion. In this case, the base support BS may be divided into a first area A ₁ , a second area A ₂ , and a third area A ₃ . According to an embodiment, the first area A ₁ may be an area where the curved part starts. Alternatively, the second area A ₂ may be an area where the curved portion ends. On the other hand, the third area A ₃ may be an area disposed between the first area A ₁ and the second area A ₂ .

The luminance of the light emitting module LM disposed in the first area A ₁ and the second area A ₂ is different from the brightness of the light emitting module LM disposed in the third area A ₃ . can Specifically, the luminance of the light emitting module LM disposed in the third area A ₃ is the brightness of the light emitting module LM disposed in the first area A ₁ and the second area A ₂ . It may be higher than the luminance. That is, the light emitting module LM of relatively low luminance is disposed in the first area A ₁ and the second area A ₂ , and the light emitting module of relatively high brightness is disposed in the third area A ₃ . (LM) may be deployed. Accordingly, the aviation obstacle light can maintain a constant brightness value.

Specifically, when a plurality of light emitting modules having the same luminance are disposed on a base support having a curved portion, different brightness values may appear depending on the viewing angle of the aerial obstacle light. However, as described above, the light emitting module LM having a relatively low luminance is disposed in the first area A ₁ and the second area A ₂ , and the light emitting module LM having a relatively low luminance is disposed in the third area A ₃ . When the light emitting module (LM) of luminance is disposed, a constant brightness value may be maintained regardless of the viewing angle of the aerial obstacle light.

Conventional aviation obstacle lights were used in a structure in which a plurality of LED lights are arranged on a base support. In the case of these conventional aviation obstacle lights, a plurality of LED lights cannot be individually controlled, so the range to which the light emitted from the LED lights is irradiated is limited. There was a difficult problem.

However, as described above, in the case of an aviation obstacle according to an embodiment of the present invention, each of the plurality of light emitting modules (LM) coupled to the base structure (BS) can be controlled in various directions, so that light is emitted. There is an advantage of being able to control the range in which the light is irradiated in various ways. In addition, since the light emitting module LM is individually coupled, only the light emitting module in which a failure occurs needs to be replaced, so that repair and maintenance are easy.

In addition, although it has been described as having a curved portion in describing the base support (BS) included in the aviation obstacle according to an embodiment of the present invention, the base support (BS) may have various shapes such as a flat surface. That is, the shape of the base support BS is not limited. In addition, since the brightness of each of the plurality of light emitting modules LM disposed on the base support BS is controllable, the light emitting module disposed in the first to third regions A ₁ , A ₂ , A ₃ . The luminance of (LM) may be set to be the same.

Above, aviation obstacles according to an embodiment of the present invention have been described. Unlike the above, the light emitting module LM according to the embodiment may be used for various types of lighting as well as aviation obstacles. Hereinafter, an example of lighting including the light emitting module LM will be described with reference to FIG. 21 .

21 is a view illustrating lighting including a light emitting module according to a second embodiment of the present invention.

Referring to FIG. 21 , the lighting may include a first base support ( BS ₁ ), a second base support ( BS ₂ ), a third base support ( BS ₃ ), and a plurality of light emitting modules. The first to third base supports (BS ₁ , BS ₂ , BS ₃ ) may have disk shapes having different diameters. According to one embodiment, the first base support (BS ₁ ) may have a larger diameter than the second base support (BS ₂ ). The second base support BS ₂ may have a larger diameter than the third base support BS ₃ .

The first to third base supports (BS ₁ , BS ₂ , BS ₃ ) are arranged to be spaced apart from each other, and the first to third base supports (BS ₁ , BS ₂ , BS ₃ ) are formed by a bridge (BR). can be connected According to one embodiment, the first base support (BS ₁ ) is disposed at the bottom, the second base support (BS ₂ ) and the third base support (BS ₃ ) above the first base support (BS ₁ ) are sequentially arranged, the first to third base supports (BS ₁ , BS ₂ , BS ₃ ) may represent a cake shape.

A plurality of light emitting modules LM may be disposed on the first to third base supports BS ₁ , BS ₂ , and BS ₃ , respectively. According to an embodiment, the light emitting module LM may be the same as the light emitting module LM according to the second embodiment of the present invention described with reference to FIGS. 9 to 18 . Accordingly, a detailed description is omitted.

As a result, the lighting in which the plurality of light emitting modules LM are disposed on the first to third base supports BS ₁ , BS ₂ , BS ₃ can individually control each light emitting module LM Accordingly, there are advantages in that repair and maintenance are easy, and the direction and range of emitted light can be variously controlled. Accordingly, the lighting can be applied to various industrial fields.

Above, an example of an aviation obstacle light and lighting according to an embodiment of the present invention has been described. Hereinafter, an aviation obstacle according to a modified example of the present invention will be described.

22 is a view showing the base module and the light emitting module included in the aviation obstacle light according to the first modification of the present invention, Figure 23 is a view showing the aviation obstacle light according to the first modification of the present invention.

22 and 23, the aviation obstacle light according to the first modification of the present invention may include a base module (base module, BM), and a plurality of light emitting modules (LM). The plurality of light emitting modules BM may be coupled to the base module BM. In addition, the plurality of light emitting modules BM may be coupled to each other to form a single body. For example, the plurality of light emitting modules BM may be coupled to each other to form the base structure BS described with reference to FIG. 8 .

According to an embodiment, the plurality of light emitting modules BM may be coupled to each other at a predetermined angle. As a specific example, the nine light emitting modules BM may be coupled side by side side by side. In this case, each of the light emitting modules BM arranged to the right around the light emitting module BM arranged in the center is +10°, +20°, +30 compared to the light emitting module BM arranged in the center. °, +40° angle can be achieved. In contrast, each of the light emitting modules BM arranged to the left with the light emitting module BM arranged in the center is -10°, -20°, -30 compared to the light emitting module BM arranged in the center. °, -40° angle can be achieved.

According to an embodiment, the manufacturing method of the aviation obstacle light according to the first modified example includes the steps of putting an ELD in a housing and assembling a lens after connecting the wiring to manufacture the light emitting module, and the four Assembling and fixing the light emitting module, manufacturing a base structure by combining the nine base modules to which the light emitting module is fixed, and coupling the upper plate and the lower plate to the upper and lower sides of the base structure, left and It may include the step of coupling the left plate and the right plate to the right.

24 is a view showing a light emitting module included in an aviation obstacle light according to a second modification of the present invention.

Referring to FIG. 24 , in the light emitting module LM included in the aviation obstacle light according to the second modified example of the present invention, the position of the light source L disposed in the housing may be variously modified. For example, as shown in (a) to (c) of FIG. 24 , the light source L may be variously disposed along an inclination inside the housing. Accordingly, the lighting angle of the light emitting module (LM) itself is adjusted, it is possible to control the angle of the aviation obstacle in a simpler way.

25 is a view showing a light emitting module included in an aviation obstacle light according to a third modified example of the present invention.

Referring to FIG. 25 , the light emitting module LM included in the aviation obstacle light according to the third modified example of the present invention may have a rectangular front surface and a rounded rear surface. In addition, the light emitting module LM may include a plurality of light sources L. According to an embodiment, the light source LM may be in the form of an LED chip. Although the light emitting module LM is illustrated as including four light sources L in FIG. 25 , the light emitting module LM may include a different number of light sources L. That is, the number of the light sources L is not limited. In the case of the light emitting module (LM) included in the aviation obstacle light according to the third modified example described above, it is advantageous in terms of high efficiency because the light illuminance should be spread sideways due to the characteristics of the aviation light.

26 is a view showing a light emitting module included in an aviation obstacle light according to a fourth modified example of the present invention.

Referring to FIG. 26 , the light emitting module LM included in the aviation obstacle light according to the fourth modified example of the present invention may have an elliptical or circular shape in front. In addition, the light emitting module LM may include a plurality of light sources L, and each light source L may be disposed to be spaced apart from each other. For example, three light sources may be spaced apart from each other at an interval of about 3.5 mm on a metal PCB. The above-described light emitting module (LM) is measured at the illuminance sensor at a distance of 18 m during authentication, and is measured while rotating at -80 to +80°. In this case, the center chip faces the sensor front at 0°, the left chip faces the sensor front at +10°, and the right chip faces the sensor front at -10°.

27 is a view showing another embodiment of the light emitting module included in the aviation obstacle light according to the first modification of the present invention, Figure 28 is another embodiment of the light emitting module included in the aviation obstacle light according to the first modification of the present invention It is a view showing an example, and FIGS. 29 and 30 are views showing another embodiment of an aviation obstacle, etc. according to a first modified example of the present invention.

27 to 30 , the aviation obstacle light according to another embodiment of the first modified example of the present invention may include a base module and a plurality of light emitting modules. The plurality of light emitting modules may be coupled to the base module. In addition, the plurality of light emitting modules may be combined with each other to form an integral body.

According to an embodiment, the plurality of light emitting modules may be coupled to each other at a predetermined angle. As a specific example, the nine light emitting modules may be coupled side by side side by side. In this case, each of the light emitting modules arranged to the right around the light emitting module disposed in the center forms an angle of +10°, +20°, +30°, +40° compared to the light emitting module disposed at the center. can On the other hand, each of the light emitting modules arranged to the left around the light emitting module arranged in the center forms an angle of -10 °, -20 °, -30 °, -40 ° compared to the light emitting module arranged in the center. can

Aviation obstacle light according to an embodiment of the present invention, by excellent heat dissipation structure, it is possible to prevent the efficiency decrease and frequent fixing of the LED lamp due to heat. There is a difference between the use of a COB type and an individual LED chip as a cause of fixed occurrence and efficiency decrease due to overheating due to the mutual thermal synergism of the LED chip.

In addition, the aviation failure light according to the embodiment of the present invention is easy to repair in case of failure, so the hassle of replacing the entire PCB or having to separate the body for replacement is eliminated, and the module can be individually replaced and repaired, thereby saving repair costs and ease of repair may be added.

In addition, since the module and the module holder are integrated, the module may have a primary heat dissipation structure and secondarily have a heat dissipation structure function in the cradle to have a dual heat dissipation structure. As the PCB inside the module is fixed and assembled in one piece, it is easy to assemble and produce, and it is advantageous for mass production only when the module and the holder are assembled in one piece. Since the module and the cradle have an integrated structure, the PCB inside the module is always seated in the forward direction, and the angle is automatically adjusted, so it is convenient to set.

In the case of PCB, the internal structure of the chip and module is designed and built with the optimal PCB seating structure to make it a feature of high efficiency according to the characteristics of the aviation obstacle indicator that must satisfy the angle and illuminance by the front detector sensor according to the chip spacing.

In this case, it was designed and developed in a structure that does not cause loss with high efficiency while satisfying the condition of 100,000 candela for each angle that must be measured by 10° in both directions according to the spacing of the chips located in the PCB or by the aviation obstacle indicator.

In addition, in order to satisfy the average illuminance value of the horizontal and vertical angles, the PCB and LED chips are seated at respective positions in the module internal structure to satisfy the conditions according to the illuminance and to produce a structure without loss.

The advantage of the cradle is that it goes beyond the simple support on which the module is seated, and the module is seated in close contact with the cradle to circulate the high heat to the cradle in a heat dissipation structure, and the angle adjustment of the flight obstacle indicator light is automatically adjusted as the module is seated. There are additional features that become

Normally, when assembling, you have to check the lighting angles one by one, but since the module and the cradle are integrated, the angle is automatically adjusted, so there is an additional function that improves the ease of assembly and productivity.

For example, if the module has a + function checked and the holder has a groove with a - function, only when these grooves match, the module and the holder will come into close contact and the assembly will be perfect, so that there is no error of 1 mm. .

The lighting of this technology does not allow an error of 1mm, and when a deviation of 1mm occurs in the instrument, when viewed with the naked eye from a relatively long distance, the deviation of 1mm is not allowed because the deviation is significantly large.

Based on this, the highest efficiency is shown as a great advantage by minimizing the effect on the wind load of the pylon by installing the solar panel in the pylon with high efficiency suitable for the transmission tower, that is, the minimum capacity.

In particular, in the case of a transmission tower installed in a mountainous area, there is a condition that the solar panel must be installed in a small amount in a narrow area due to the problem that it should be installed only in the south, so in this case, there is a reason that it should have many advantages .

The relationship between the structure of the conventional aviation obstacle indicator or the similar structure developed so far and the PCB is a structure in which a number of PCBs and LED chips are seated by a simple structure and connected in a long band regardless of the angle. It is measured by irradiating the 90° angle of the obstacle indicator, and each angle must satisfy the illuminance of 100,000 candela (high luminance type B) and 200,000 candela (high luminance type A).

In this case, it is designed in a structure that continuously connects the LED chips to each PCB, and is automatically assembled by SMT, and a long strip-shaped lens is covered on the LED chip to produce lighting, and a backlight (backlight irradiation method) type A reflector is installed behind the furnace for irradiation.

However, in this case, since the illuminance is connected for a long time by maintaining the band shape, the illuminance leaks out where it is not necessary, thereby reducing efficiency or causing loss.

The problem with this technology is this. In order to overcome this, this technology maintains a certain distance between the PCB and the LED chip, uses only the illuminance that is absolutely necessary, and controls the light so as not to lose the rest. There is an advantage to

Three, four, or five LED chips can be seated on one PCB, but in the state that the angle is adjusted so that only the necessary illuminance has efficiency, the LED chip and the PCB are combined, and the combined PCB has a heat dissipation structure. By being seated in the optimized module, it can be manufactured as a high-efficiency aviation obstacle indicator with the features listed above.

In conclusion, the products of companies with existing technology are 0° (front), 10, 20, 30, 40, 50, 60, 70, 80, -10, -20, -30, -40, -50, -60 , -70, -80, regardless of the angle, the whole is displayed in illuminance. That is, loss occurs by illuminating the whole from 0° to 1 to 80° and -1 to -80°, and our advanced technology has high efficiency by controlling the illuminance by only 10° (1 to 9, 11 to 19). , 21-19, ~~ These angles are unnecessary and lossy). Light appears as a point in the vicinity, but when it goes out of a certain distance, it is gathered as a single light source and irradiated, so that the structure of the aviation obstacle indicator can be satisfied.

As mentioned above, although the present invention has been described in detail using preferred embodiments, the scope of the present invention is not limited to specific embodiments and should be construed according to the appended claims. In addition, those skilled in the art should understand that many modifications and variations are possible without departing from the scope of the present invention.

Aviation obstacle light including a multifunctional light emitting module according to an embodiment of the present invention can be used throughout the aviation industry.

1000: light emitting module

2000: support module

3000: base support

100: first housing

200: second housing

300: connector

400: reflector

L: light source

LM: light emitting module

BS: base support

Claims (14)

1. In the aviation obstacle light comprising a base support (base support structure), and a plurality of light emitting structures coupled to the base support,

   The light emitting structure,

   a light emitting module including a first housing on which a light source is mounted, and a second housing including a lens for condensing the light emitted from the light source and coupled to the first housing; and

   Comprising a support module coupled to the first housing of the light emitting module,

   The first housing includes a coupling groove recessed from one end of the first housing toward the second housing,

   The support module includes a first guide groove and a second guide groove extending in a longitudinal direction of the support module and spaced apart from each other, and a coupling line disposed between the first guide groove and the second guide groove, ,

   Aviation obstacle light comprising a coupling line of the support module is inserted into the coupling groove of the first housing, and the first housing and the support module are coupled.
2. The method of claim 1,

   The support module includes first and second sidewalls extending from both sides of the support module in a longitudinal direction of the support module and in a vertical direction of a lower surface of the support module,

   Between the first sidewall and the second sidewall, the first guide groove, the coupling line, and the second guide groove are sequentially disposed,

   The first guide groove, the coupling line, and the inside of the first sidewall and the second sidewall exposed in the direction of the second guide groove, aviation obstacles including those having an inclined shape.
3. 3. The method of claim 2,

   The first housing has a tapered shape that increases in diameter from one end to the other end,

   When the first housing and the support module are combined, the outside of the first housing is supported by the first sidewall and the second sidewall of the support module.
4. 3. The method of claim 2,

   The support module includes a fastener protruding from a lower surface of the support module in opposite directions of the first and second sidewalls, and a heat dissipation member,

   Aviation obstruction lights comprising the light emitting structure and the base support screw-coupled through the fastener.
5. 5. The method of claim 4,

   The fastener includes a first fastener protruding from a lower surface of the support module in a direction opposite to the first sidewall, and a second fastener protruding from a lower surface of the support module in a direction opposite to the second sidewall. do,

   The heat dissipation member, Aviation obstruction light including being disposed between the first fastener and the second fastener.
6. In an aviation obstacle including a base support structure, and a plurality of light emitting modules coupled to the base support,

   The light emitting module,

   a first housing on which the light source is mounted;

   a second housing coupled to one end of the first housing and including a lens for condensing the light emitted from the light source; and

   One end is coupled to the other end of the first housing, the other end is coupled to the base support, aviation obstacle including a connector for fixing the first housing to the base support.
7. 7. The method of claim 6,

   The base support has a curved portion,

   The base support includes a first region where the curved portion starts, a second region where the curved portion ends, and a third region that is disposed between the first region and the second region.
8. 7. The method of claim 6,

   The light emitting module,

   A reflective plate disposed in the first housing to surround the light source,

   The light emitted from the light source is condensed by the reflector and then provided to the lens.
9. 7. The method of claim 6,

   The other end of the first housing has a multi-step structure in which the size of the diameter decreases as the distance from the one end of the first housing decreases,

   Aviation obstacles including those having a tapered shape by the multi-stage structure.
10. 10. The method of claim 9,

    The connector is

    a connector housing having a hollow cylindrical shape and having an opening in a 'U' shape from one end to the other end; and

    A connection member having one end coupled to the first housing and the other end coupled to the connector housing,

    The connecting member, from a first direction that is the longitudinal direction of the connecting member, aviation obstacles, etc. comprising a coupling to be rotated in a second direction perpendicular to the first direction.
11. 11. The method of claim 10,

    The connecting member is an aviation obstacle including a screw thread coupling with the first housing.
12. 7. The method of claim 6,

    The base support includes a plurality of cradles, and the plurality of light emitting modules are coupled to each cradle,

    The plurality of cradles and the plurality of light emitting modules are all made of a concave-convex structure, and the plurality of cradles and the plurality of light emitting modules are coupled through the concave-convex structure.
13. 13. The method of claim 12,

    The light source is integrated with the PCB and is located at any one of the top, middle, and bottom inside the module, 4 modules are coupled without a rotating body, and the remaining part is an aviation comprising 3 modules coupled to a cradle without a rotating body disability, etc.
14. 7. The method of claim 6,

    A reflective film inside the module is vacuum-deposited by CVD and sputtering, and the reflective film is an aviation obstacle including silver, aluminum, and chromium.

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