Easy to install, stably installed, easy to maintain and repair, and focal length-adjustable high-efficiency aircraft warning light providing 360-degree omni-directional illumination and operating efficiently

Abstract

Provided is an aircraft warning light comprising: a body unit including a columnar shape that is empty on the inside; and illumination units radially arranged on the outer circumferential surface of the body unit. The illumination units each include: a cylindrical housing that is empty on the inside and open at both ends; a lens coupled to one end of the housing; an inner member inserted into the empty interior of the housing; and a light-emitting member that is fixed on the inner member and emits light toward the lens. Accordingly, the aircraft warning light is stably installed, easy to maintain, and adjustable in focal length.

Description

High-efficiency aviation obstacle warning light that is easy to install, stable, easy to maintain, has an adjustable focal length, and operates efficiently with a 360-degree all-round illumination.

[0001] The present application relates to an aviation obstacle warning light, and more specifically, to a body part including a columnar shape with an interior that is hollow, a plurality of lighting units radially arranged on an outer surface of the body part, a lighting control unit connecting the body part to the lighting units, and a plate to which the plurality of lighting units are fixed and attached on the outer surface of the body part, wherein the plurality of lighting units include a cylindrical housing with an interior that is hollow and open at both ends, a lens coupled to one end of the housing, an internal member inserted into the hollow interior of the housing, and a lighting member fixed on the internal member and emitting light toward the lens, and includes a first lighting unit fixed at a first height on the outer surface of the body part, a second lighting unit fixed at a second height on the outer surface of the body part, and a third lighting unit fixed at a third height on the outer surface of the body part, wherein a direction of the first lighting unit fixed at the first height is arranged differently from a direction of the second lighting unit fixed at the second height, and a direction of the second lighting unit fixed at the second height is different from a direction of the third lighting unit fixed at the third height. The third lighting unit is arranged differently from the direction of the lighting unit, and the direction of the third lighting unit fixed at the third height is arranged differently from the direction of the first lighting unit fixed at the first height, so that the plurality of lighting units emit light in different directions from the center of the body, thereby being easy to install, stably installed, easy to maintain, having an adjustable focal length, and operating efficiently by irradiating in all 360 degrees.

[0002]

[0003] Generally, tall structures such as power lines or high-rise buildings between transmission towers pose a significant threat to low-flying aircraft. Therefore, to mark them as aviation obstacles, aircraft obstruction markers, which function as aviation obstruction lights, are installed on the overhead ground wires between transmission towers in accordance with the Civil Aviation Organization (ICAO) Annex 14-Aerodrom Design Manual and Article 83 of the Civil Aviation Act (Installation of Aircraft Obstruction Markers, etc.). These aircraft obstruction markers are installed at regular intervals on the overhead ground wires of transmission towers during the day to prevent aircraft from approaching and ensure visibility.

[0004] For nighttime use, improved versions of these conventional obstruction signs have been developed, featuring LED lamps that function as obstruction indicators. However, these conventional obstruction signs only illuminate at a constant brightness, making it difficult for pilots to intuitively perceive the expected collision distance, making it difficult to prevent collisions.

[0005]

[0006] The technical problem that this application seeks to solve is to provide an aviation obstacle warning light with easy focus distance adjustment.

[0007] Another technical challenge that this application seeks to address is to provide an aviation obstacle warning light that can be stably installed.

[0008] Another technical challenge that this application seeks to address is to provide an aircraft obstacle warning light that is easy to maintain.

[0009] Another technical challenge that this application seeks to address is to provide an aviation obstacle warning light with improved construction convenience.

[0010] Another technical challenge that the present application seeks to address is to provide an aviation obstacle warning light with reduced installation and maintenance costs.

[0011] Another technical challenge that this application seeks to solve is to provide an aviation obstacle indicator that is easy to operate.

[0012] The technical problems that this application seeks to solve are not limited to those described above.

[0013]

[0014] To solve the above technical problem, the present application provides an aviation obstacle indicator.

[0015] According to one embodiment, the aviation obstacle warning light includes a body part having a hollow column shape, and a lighting part radially arranged on an outer surface of the body part, wherein the lighting part may include a cylindrical housing having a hollow interior and open at both ends, a lens coupled to one end of the housing, an inner member inserted into the hollow interior of the housing, and a lighting part fixed on the inner member and emitting light toward the lens.

[0016] According to one embodiment, the lighting unit further includes a power supply unit electrically connected to the light-emitting member, wherein the power supply unit may include a solar cell panel disposed on an upper surface of the body unit and generating and storing electric energy from sunlight.

[0017] According to one embodiment, the power supply unit may further include an energy conversion unit that is disposed adjacent to the transmission line and on a lower surface of the body unit, and converts electromagnetic waves generated from the transmission line into electrical energy.

[0018] According to one embodiment, the lighting control unit may further include a lighting control unit connecting the body unit and the lighting unit, wherein the lighting control unit includes a first fixture having one end fixed to the body unit and the other end including a receiving space, and a second fixture having one end fixed to the lighting unit and the other end rotating within the receiving space of the first fixture, such that an angle of the lighting unit is adjusted from the body unit.

[0019] According to one embodiment, the device further comprises a pair of fixed connectors spaced apart from each other and surrounding at least a portion of the processing line, a pair of support rods extending downward from each of the pair of fixed connectors, a plate connecting the pair of support rods, a ground connector positioned between the pair of fixed connectors and surrounding at least a portion of the processing line, and a ground line connected to the processing line through the ground connector and extending downward from the ground connector, wherein the body portion may be disposed on the plate, and the light-emitting member of the lighting portion may be electrically connected to the ground line.

[0020] According to one embodiment, the body part may further include a base having a hemispherical shape with an interior that is hollow and is attached to an existing aviation obstacle marker, wherein the body part may include a body part installed on the base.

[0021]

[0022] According to an embodiment of the present application, an aviation obstacle warning light includes a body part having a hollow interior and a pillar shape, and a lighting part radially arranged on an outer surface of the body part, wherein the lighting part may include a cylindrical housing having a hollow interior and open at both ends, a lens coupled to one end of the housing, an internal member inserted into the hollow interior of the housing, and a lighting part fixed on the internal member and emitting light toward the lens. Accordingly, the focal length can be easily adjusted.

[0023] In addition, the lighting unit may further include a power supply unit electrically connected to the light-emitting member, wherein the power supply unit includes a solar cell panel disposed on an upper surface of the body unit and generating and storing electric energy from sunlight, and may further include an energy conversion unit disposed adjacent to a power transmission line and disposed on a lower surface of the body unit and converting electromagnetic waves generated from the power transmission line into electric energy. Accordingly, energy efficiency may be improved and maintenance costs may be reduced.

[0024] In addition, the lighting control unit may further include a lighting control unit that connects the body part and the lighting unit, wherein the lighting control unit includes a first fixture having one end fixed to the body part and an accommodation space at the other end, and a second fixture having one end fixed to the lighting unit and the other end rotatable within the accommodation space of the first fixture, such that the angle of the lighting unit is adjusted from the body part. Accordingly, operation is convenient and construction convenience can be improved.

[0025] In addition, the device may further include a pair of fixed connectors spaced apart from each other and wrapping around at least a portion of the processing line, a pair of support rods extending downward from each of the pair of fixed connectors, a plate connecting the pair of support rods, a ground connector positioned between the pair of fixed connectors and wrapping around at least a portion of the processing line, and a ground wire connected to the processing line through the ground connector and extending downward from the ground connector, wherein the body portion may be disposed on the plate, and the light-emitting member of the lighting portion may be electrically connected to the ground wire. Accordingly, the device may be stably installed on the processing line.

[0026] The device has a hemispherical shape with an empty interior and further includes a base that is attached to an existing aviation obstacle indicator, wherein the body portion may include a part installed on the base. Accordingly, maintenance can be easily performed.

[0027]

[0028] Figure 1 is a drawing for explaining an aviation obstacle indicator light according to an embodiment of the present application.

[0029] FIGS. 2 to 5 are drawings for explaining the lighting unit of an aviation obstacle warning light according to an embodiment of the present application.

[0030] FIG. 6 is a drawing for explaining a lighting control unit of an aviation obstacle warning light according to an embodiment of the present application.

[0031] FIG. 7 is a drawing for explaining the housing and internal components of the lighting unit of the aviation obstacle warning light according to the first modified example of the present application.

[0032] Figure 8 is a cross-sectional view taken along line A-A' of Figure 7.

[0033] FIG. 9 is a cross-sectional view illustrating rotation of an internal member within a housing of an aviation obstacle warning light according to a first modified example of the present application.

[0034] Fig. 10 is a cross-sectional view taken along line B-B' of Fig. 7.

[0035] Fig. 11 is a cross-sectional view illustrating a sliding groove inside the housing of an aviation obstacle warning light according to a second modified example of the present application.

[0036] FIGS. 12 and 13 are cross-sectional views illustrating rotation of an internal member within a housing of an aviation obstacle warning light according to a third modified example of the present application.

[0037] Fig. 14 is a cross-sectional view taken along line C-C' of Fig. 13.

[0038] Fig. 15 is a drawing for explaining an aviation obstacle indicator light according to a fourth modified example of the present application.

[0039] Fig. 16 is a drawing for explaining an aviation obstacle indicator light according to a fifth modified example of the present application.

[0040] Figures 17 to 19 are drawings for explaining an aviation obstacle indicator light according to a sixth modified example of the present application.

[0041] Fig. 20 is a drawing for explaining a processing line on which an aviation obstacle warning light is installed according to the seventh modified example of the present application.

[0042] FIGS. 21 to 23 are drawings for explaining an aviation obstacle indicator light according to the seventh modified example of the present application.

[0043] Fig. 24 is a drawing for explaining an aviation obstacle indicator light according to the eighth modified example of the present application.

[0044] Fig. 25 is a drawing for explaining an aviation obstacle indicator light according to the ninth modified example of the present application.

[0045] Fig. 26 is a drawing for explaining an aviation obstacle indicator light according to the 10th modified example of the present application.

[0046] Figure 27 is a drawing for explaining an aviation obstacle indicator light according to the 11th modified example of the present application.

[0047] Fig. 28 is a drawing for explaining an existing aviation obstacle indicator in which an aviation obstacle indicator is installed according to the 12th modified example of the present application.

[0048] Fig. 29 is a drawing for explaining an aviation obstacle indicator light according to the 12th modified example of the present application.

[0049] Fig. 30 is a drawing for explaining an aviation obstacle indicator light according to the 13th modified example of the present application.

[0050] Figure 31 is a drawing for explaining an aviation obstacle indicator light according to the 14th modified example of the present application.

[0051] FIG. 32 and FIG. 33 are drawings for explaining an aviation obstacle indicator light according to the 15th modified example of the present application.

[0052] FIGS. 34 and 35 are drawings for explaining an aviation obstacle indicator light according to the 16th modified example of the present application.

[0053] Fig. 36 is a drawing for explaining a lighting unit of an aviation obstacle warning light according to the 17th modified example of the present application.

[0054] Figure 37 is a drawing for explaining a support according to the 17th modified example of the present application.

[0055] Fig. 38 is a perspective view for explaining a support plate according to the 17th modified example of the present application.

[0056] Fig. 39 is a drawing for explaining the combination of multiple supports according to the 17th modified example of the present application.

[0057] Fig. 40 is a perspective view for explaining a support according to the 17th modified example of the present application.

[0058] FIG. 41 and FIG. 42 are perspective views illustrating the angle adjustment of the lighting unit according to the 17th modified example of the present application.

[0059] Fig. 43 is a plan view for explaining a support part of an aviation obstacle indicator light according to the 18th modified example of the present application.

[0060] FIG. 44 and FIG. 45 are drawings for explaining how the angle of the lighting unit is adjusted according to the 19th modified example of the present application.

[0061] Figure 46 is a drawing for explaining an aviation obstacle indicator light according to the 20th modified example of the present application.

[0062] Figure 47 is a drawing for explaining an aviation obstacle indicator light according to the 21st modified example of the present application.

[0063]

[0064] Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the attached drawings. However, the technical concept 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 to ensure that the disclosed content is thorough and complete and to sufficiently convey the spirit of the present invention to those skilled in the art.

[0065] Also, although terms such as first, second, and third have been used to describe various components in various embodiments of this specification, these components should not be limited by these terms. These terms are only used to distinguish one component from another. Thus, 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 its complementary embodiments. Also, the term "and / or" has been used herein to mean including at least one of the components listed before and after.

[0066] In the specification, singular expressions include plural expressions unless the context clearly dictates otherwise. In addition, terms such as "comprise" or "have" are intended to indicate the presence of a feature, number, step, component, or combination thereof described in the specification, and should not be construed as excluding the possibility of the presence or addition of one or more other features, numbers, steps, components, or combinations thereof. In addition, in the following description of the present invention, if a detailed description of a related known function or configuration is determined to unnecessarily obscure the gist of the present invention, the detailed description thereof will be omitted.

[0067]

[0068] FIG. 1 is a drawing for explaining an aviation obstacle indicator according to an embodiment of the present application, FIGS. 2 to 5 are drawings for explaining a lighting unit of an aviation obstacle indicator according to an embodiment of the present application, and FIG. 6 is a drawing for explaining a lighting control unit of an aviation obstacle indicator according to an embodiment of the present application.

[0069] Referring to FIGS. 1 to 6, an aviation obstacle warning light according to an embodiment of the present application may be installed on a transmission line, an overhead line, etc. between buildings, structures, transmission towers, etc. The aviation obstacle warning light may include a body (100), a lighting unit (200), a lighting control unit (300), and a control unit (400).

[0070] The body portion (100) may include a hollow cylindrical shape or a hollow polygonal column shape. For example, the body portion (100) may include a first protrusion (110) and a first recessed portion (212). It may include a shape such as a cylinder, a triangular column, a square column, or a hexagonal column. Wires, circuits, batteries, etc. may be embedded inside the body portion (100).

[0071] The above lighting unit (200) may be fixed on the outer surface of the body portion. The lighting units (200) may be formed in multiples and arranged radially on the outer surface of the body portion (100). The lighting unit (200) may include a housing (210), a lens (215), an internal member (220), and a light-emitting member (225).

[0072] The housing (210) may have a cylindrical shape with an interior that is hollow and open at both ends. The housing (210) may include a first protrusion (211) and a first recessed portion (212).

[0073] The first protrusion (211) may be formed to protrude in a spiral shape on the inner wall (210a) of the housing (210). For example, the first protrusion (211) may include a screw thread formed on the inner wall (210a) of the housing (210).

[0074] The first recessed portion (212) may be formed to be spirally recessed so as not to overlap with the first protrusion (211). For example, the first recessed portion (212) may include a screw groove formed in the inner wall (210a) of the housing (210).

[0075] The lens (215) can be coupled with the open end of the housing (210). For example, the lens (215) may be a plano-convex lens having one side that is flat and the other side that is convex, but is not limited thereto.

[0076] The inner member (220) may be inserted into the interior of the housing (210). The inner member (220) may have a cylindrical shape having an outer diameter smaller than the inner diameter of the housing (210). The inner member (220) may include a second protrusion (221) and a second recessed portion (222).

[0077] The second protrusion (221) may be formed to protrude in a spiral shape on the outer surface of the inner member (220). For example, the second protrusion (221) may include a screw thread formed on the outside of the inner member (220).

[0078] The second recessed portion (222) may be formed to be spirally recessed so as not to overlap with the second protrusion (221). For example, the second recessed portion (222) may include a screw groove formed on the outer surface of the inner member (220).

[0079] The above light-emitting member (225) can be fixed on the inner member (220). The light-emitting member (225) can emit light toward the lens (215) from inside the housing (210). The light-emitting member (225) can be formed singly or in plurality, but is not limited thereto. The brightness of the light-emitting member (225) can be variably controlled through the control unit (400).

[0080] In other words, the first protrusion (211) of the housing (210) is inserted into the second recessed portion (222) of the inner member (220), and the second protrusion (221) of the inner member (220) can be inserted into the first recessed portion (212) of the housing (210). Accordingly, the second protrusion (221) of the inner member (220) can rotate inside the housing (210) along the first recessed portion (212) of the housing (210). Consequently, as the inner member (220) relatively rotates inside the housing (210), the inner member (220) can move in the longitudinal direction (z-axis direction) of the housing (210) inside the housing (210). For example, the focal length of the light-emitting member (225) can be set to 39 mm as shown in FIG. 5. Accordingly, the distance (d) between the lens (215) and the light-emitting member (225) can be adjusted, making it easy to adjust the focal length.

[0081] According to one embodiment, the light-emitting member (225) may selectively include one or more of a low-intensity LED, a medium-intensity LED, and a high-intensity LED. For example, the light-emitting member (225) may include at least one low-intensity LED and at least one medium-intensity LED. Alternatively, the light-emitting member (225) may include at least one low-intensity LED and at least one high-intensity LED. Alternatively, the light-emitting member (225) may include, but is not limited to, at least one medium-intensity LED and at least one high-intensity LED.

[0082] For example, the low-brightness LED may include a low-brightness A-type LED having a luminous intensity of 10 cd or more, and a low-brightness B-type LED having a luminous intensity of 32 cd or more. The medium-brightness LED may include a medium-brightness A-type LED having a luminous intensity of about 20,000 cd, a medium-brightness B-type LED that blinks with a luminous intensity of about 2,000 cd, and a medium-brightness C-type LED that is constantly on with a luminous intensity of about 2,000 cd. The high-brightness LED may include a high-brightness A-type LED having a luminous intensity of about 200,000 cd, and a high-brightness B-type LED having a luminous intensity of 100,000 cd.

[0083] The above lighting control unit (300) can connect the body part (100) and the lighting unit (200). The angle of the lighting unit (200) from the body part (100) can be adjusted through the lighting control unit (300). The lighting control unit (300) can include a first fixing member (311) and a second fixing member (321).

[0084] One end of the first fixture (311) may be fixed to the body part (100). For example, one end of the first fixture (311) may be coupled to the body part (100) via a bolt. The other end of the first fixture (311) may be connected to the second fixture (321). The other end of the first fixture (311) may include a receiving space (312).

[0085] One end of the second fixture (321) may be fixed to the lighting unit (200). For example, one end of the second fixture (321) may be coupled to the lighting unit (200) via a bolt. The other end of the second fixture (321) may be connected to the other end of the first fixture (311). The other end of the second fixture (321) may include a rotary member (322) having a sphere shape.

[0086] In other words, the rotary member (322) of the second fixture (321) can be inserted into the interior of the receiving space (312) of the first fixture (311). That is, as the rotary member (322) of the second fixture (321) rotates inside the receiving space (312) of the first fixture (311), the lighting unit (200) to which the first fixture (432) is fixed can relatively rotate from the body unit (100) to which the first fixture (311) is fixed. As a result, the angle of the lighting unit (200) is adjusted by the lighting control unit (300), so that the light-emitting directions of the light-emitting members (225) inside the plurality of lighting units (200) can be adjusted, respectively. Accordingly, the light-emitting efficiency of the lighting unit (200) is improved, and visibility can be greatly improved even at night.

[0087] The above control unit (400) may be built into the interior of the body unit (100). As described above, the control unit (400) may control the brightness of the light-emitting member (225). The control unit (400) may include a light sensor (CdS), a global positioning system (GPS), and a controller.

[0088] The above-mentioned light sensor (CdS) can measure the illuminance (the amount of light received per unit time per unit area) around the location where the above-mentioned aviation obstacle warning light is installed and output a signal. The above-mentioned light sensor (CdS) can transmit the measured illuminance value to the controller.

[0089] The GPS can calculate the location of the location where the aircraft obstacle warning light is installed and output a signal. The GPS can transmit the measured location to the controller.

[0090] The controller can adjust the brightness of the light-emitting member (225) based on the illuminance value received from the illuminance sensor (CdS). Alternatively, the controller can turn on the light-emitting member (225) when the illuminance value received from the illuminance sensor (CdS) is below a certain value, or turn off the light-emitting member (225) when the illuminance value is above a certain value. The controller can include an MPPT (Maximum Power Point Tracking) controller.

[0091] The above MPPT controller may include a maximum power point tracking control function. The MPPT controller can automatically track the maximum output, operating voltage, etc. of the solar panel according to changes in sunlight intensity or temperature. The MPPT controller can control the electrical energy output of the solar panel to its maximum value.

[0092] In other words, the control unit (400) can turn the light-emitting member (225) on / off according to the surrounding illuminance through the light sensor (CdS) and the controller. In addition, the control unit (400) can turn the light-emitting member (225) at a specific location on / off at a specific time using the GPS and the controller.

[0093] FIG. 7 is a drawing for explaining the housing and internal components of the lighting unit of the aviation obstacle warning light according to the first modified example of the present application, FIG. 8 is a cross-sectional view taken along line A-A' of FIG. 7, FIG. 9 is a cross-sectional view for explaining the rotation of the internal components inside the housing of the aviation obstacle warning light according to the first modified example of the present application, and FIG. 10 is a cross-sectional view taken along line B-B' of FIG. 7.

[0094] Referring to FIGS. 7 to 10, the lighting unit (200) of the aviation obstacle warning light according to the first modified example of the present application may include a housing (210), a lens (215), an internal member (220), and a light-emitting member (225).

[0095] The housing (210) may have a cylindrical shape with an interior that is hollow and open at both ends. The housing (210) may include a first protrusion (211) and a sliding groove (213).

[0096] The first protrusions (211) may be formed in pairs on the inner wall (210a) of the housing (210). A pair of the first protrusions (211) may be symmetrical with respect to an imaginary line that passes through the center of the housing (210) in the longitudinal direction. The first protrusions (211) may be formed in plurality and spaced apart from each other in the longitudinal direction (z-axis direction) of the housing (210).

[0097] The sliding groove (213) does not overlap with the first protrusion (211) and may be formed recessed in the longitudinal direction (z-axis direction) of the housing (210) on the inner wall (210a) of the housing (210). The sliding grooves (213) may be formed singly or in a pair symmetrically. As illustrated in FIG. 10, a pair of the sliding grooves (213) and a pair of the first protrusions (211) may be spaced apart from each other so as not to overlap on the same plane (xy plane). For example, a pair of the sliding grooves (213) and a pair of the first protrusions (211) may be spaced apart from each other by 90° on the inner wall (210a) of the housing (210). The depth of the sliding groove (213) may be formed shallower than the thickness of the inner wall (210a).

[0098] The lens (215) can be coupled with the open end of the housing (210). For example, the lens (215) may be a plano-convex lens in which one side coupled with the open end of the housing (210) is flat and the other side is convex, but is not limited thereto.

[0099] The inner member (220) may be inserted into the interior of the housing (210). The inner member (220) may have a cylindrical shape with an outer diameter smaller than the inner diameter of the housing (210). The inner member (220) may include a second protrusion (221).

[0100] The second protrusions (221) may be formed as a pair on the cylindrical outer surface of the inner member (220). The pair of second protrusions (221) may be symmetrical with respect to an imaginary line passing through the center of the inner member (220) in the longitudinal direction. The second protrusions (221) may be seated on the first protrusions (211) or may move in the longitudinal direction (z-axis direction) of the housing (210) within the sliding groove (213).

[0101] The above light-emitting member (225) can be fixed on the inner member (220). The light-emitting member (225) can emit light toward the lens (215) from inside the housing (210). The light-emitting member (225) can be formed singly or in plurality, but is not limited thereto.

[0102] According to one embodiment, the light-emitting member (225) may selectively include one or more of a low-intensity LED, a medium-intensity LED, and a high-intensity LED. For example, the light-emitting member (225) may include at least one low-intensity LED and at least one medium-intensity LED. Alternatively, the light-emitting member (225) may include at least one low-intensity LED and at least one high-intensity LED. Alternatively, the light-emitting member (225) may include, but is not limited to, at least one medium-intensity LED and at least one high-intensity LED.

[0103] For example, the low-brightness LED may include a low-brightness A-type LED having a luminous intensity of 10 cd or more, and a low-brightness B-type LED having a luminous intensity of 32 cd or more. The medium-brightness LED may include a medium-brightness A-type LED having a luminous intensity of about 20,000 cd, a medium-brightness B-type LED that blinks with a luminous intensity of about 2,000 cd, and a medium-brightness C-type LED that is constantly on with a luminous intensity of about 2,000 cd. The high-brightness LED may include a high-brightness A-type LED having a luminous intensity of about 200,000 cd, and a high-brightness B-type LED having a luminous intensity of 100,000 cd.

[0104] As a result, the inner member (220) can freely rotate inside the housing (210), and the inner member (220) can selectively move in the longitudinal direction (z-axis direction) of the outer member inside the housing (210). In other words, the second protrusion (221) of the inner member (220) can be seated on the first protrusion (211) of the housing (210), or can move along the sliding groove (213) of the housing (210). That is, when the second protrusion (221) of the inner member (220) is positioned on the first protrusion (211) of the housing (210), the distance (d) between the lens (215) and the light-emitting member (225) can be fixed. In addition, when the second protrusion (221) of the inner member (220) is located on the sliding groove (213) side of the housing (210), the second protrusion (221) moves along the sliding groove (213), and the distance (d) between the lens (215) and the light-emitting member (225) can be adjusted. Accordingly, by simply rotating the housing (210) or the inner member (220), the distance (d) between the lens (215) and the light-emitting member (225) can be adjusted, so that the focal length can be easily adjusted and installed when constructing or maintaining the aviation obstacle warning light.

[0105] Fig. 11 is a cross-sectional view illustrating a sliding groove inside the housing of an aviation obstacle warning light according to a second modified example of the present application.

[0106] Referring to Fig. 11, the housing (210) of the lighting unit (200) of the aviation obstacle warning light according to the second modified example of the present application may have a cylindrical shape with an interior that is hollow and open at both ends. The housing (210) may include a first protrusion (211) and a sliding groove (213).

[0107] The first protrusions (211) may be formed in pairs on the inner wall (210a) of the housing (210). A pair of the first protrusions (211) may be symmetrical with respect to an imaginary line that passes through the center of the housing (210) in the longitudinal direction. The first protrusions (211) may be formed in plurality and spaced apart from each other in the longitudinal direction (z-axis direction) of the housing (210).

[0108] The above sliding groove (213) does not overlap with the first protrusion (211) and may be formed recessed in the longitudinal direction (z-axis direction) of the housing (210) on the inner wall (210a) of the housing (210). The sliding groove (213) may be formed singly or in a pair symmetrically to each other. The sliding groove (213) may include an inclined surface (213a).

[0109] In other words, the thickness of the inner wall (210a) in which the sliding groove (213) is formed may include a thickness that becomes thinner from the outside to the inside of the sliding groove (213). That is, when the inner member (220) rotates inside the housing (210), the second protrusion (221) of the inner member (220) can be smoothly introduced into the sliding groove (213) by the inclined surface (213a). Accordingly, when adjusting the focal length, it can be easily and conveniently operated, thereby improving the convenience of the user.

[0110] FIG. 12 and FIG. 13 are cross-sectional views illustrating rotation of an internal member inside a housing of an aviation obstacle warning light according to a third modified example of the present application, and FIG. 14 is a cross-sectional view taken along line C-C' of FIG. 13.

[0111] Referring to FIGS. 12 and 13, the lighting unit (200) of the aviation obstacle warning light according to the third modified example of the present application may include a housing (210), a lens (215), an internal member (220), and a light-emitting member (225).

[0112] The housing (210) may have a cylindrical shape with an interior that is hollow and open at both ends. The housing (210) may include a first protrusion (211) and a sliding groove (213).

[0113] The first protrusions (211) may be formed in pairs on the inner wall (210a) of the housing (210). The pair of first protrusions (211) may be symmetrical with respect to an imaginary line passing through the center of the housing (210) in the longitudinal direction. The pair of first protrusions (211) may be formed in plurality and spaced apart from each other in the longitudinal direction (z-axis direction) of the housing (210). As illustrated in FIG. 12, the first protrusions (211) may include a first-first protrusion (211a), a first-second protrusion (211b), a first-third protrusion (211c), and a first-fourth protrusion (211d).

[0114] The sliding groove (213) may be formed on both sides of the inner wall (210a) so as not to overlap with the first protrusion (211). Some of the sliding grooves (213) on both sides may be symmetrical with respect to an imaginary line passing through the center of the housing (210) in the longitudinal direction, and the remaining parts may be asymmetrical. The sliding groove (213) may be formed by recessing in the longitudinal direction (z-axis direction) of the housing (210) on the inner wall (210a) of the housing (210). The sliding grooves (213) may be formed in plurality and spaced apart from each other in the longitudinal direction (z-axis direction) of the housing (210). As illustrated in FIG. 14, the sliding groove (213) may include a first sliding groove (213a), a second sliding groove (213b), a third sliding groove (213c), and a fourth sliding groove (213d).

[0115] The lens (215) can be coupled with the open end of the housing (210). For example, the lens (215) may be a plano-convex lens in which one side coupled with the open end of the housing (210) is flat and the other side is convex, but is not limited thereto.

[0116] The inner member (220) may be inserted into the interior of the housing (210). The inner member (220) may have a cylindrical shape with an outer diameter smaller than the inner diameter of the housing (210). The inner member (220) may include a second protrusion (221).

[0117] The second protrusions (221) may be formed as a pair on the cylindrical outer surface of the inner member (220). The pair of second protrusions (221) may be symmetrical with respect to an imaginary line passing through the center of the inner member (220) in the longitudinal direction. The second protrusions (221) may be seated on the first protrusions (211) or may move in the longitudinal direction (z-axis direction) of the housing (210) within the sliding groove (213).

[0118] For example, when the inner member (220) rotates in one direction inside the housing (210), the second protrusion (221) can be guided and seated on the 1-1 protrusion (211a) by the first sliding groove (213a). Then, when the inner member (220) rotates in one direction at a certain angle inside the housing (210), the second protrusion (221) can be guided and seated on the 1-2 protrusion (211b) by the second sliding groove (213b). In addition, when the inner member (220) rotates in one direction at a certain angle inside the housing (210), the second protrusion (221) can be guided and seated on the 1-3 protrusion (211c) by the third sliding groove (213c). Likewise, when the inner member (220) rotates in one direction at a certain angle inside the housing (210), the second protrusion (221) can be guided and seated on the first to fourth protrusion (213d) by the fourth sliding groove (213d).

[0119] As a result, the inner member (220) can be selectively rotated inside the housing (210) and can be selectively moved in the longitudinal direction (z-axis direction) of the housing (210). That is, when the inner member (220) is rotated in one direction by a certain angle inside the housing (210), the distance between the lens (215) and the inner member (220) can be adjusted stepwise. Accordingly, when constructing or maintaining an aviation obstacle warning light, the focal length can be easily adjusted for installation, and the light can be easily and simply operated.

[0120] The above light-emitting member (225) can be fixed on the inner member (220). The light-emitting member (225) can emit light toward the lens (215) from inside the housing (210). The light-emitting member (225) can be formed singly or in plurality, but is not limited thereto.

[0121] According to one embodiment, the light-emitting member (225) may selectively include one or more of a low-intensity LED, a medium-intensity LED, and a high-intensity LED. For example, the light-emitting member (225) may include at least one low-intensity LED and at least one medium-intensity LED. Alternatively, the light-emitting member (225) may include at least one low-intensity LED and at least one high-intensity LED. Alternatively, the light-emitting member (225) may include, but is not limited to, at least one medium-intensity LED and at least one high-intensity LED.

[0122] For example, the low-brightness LED may include a low-brightness A-type LED having a luminous intensity of 10 cd or more, and a low-brightness B-type LED having a luminous intensity of 32 cd or more. The medium-brightness LED may include a medium-brightness A-type LED having a luminous intensity of about 20,000 cd, a medium-brightness B-type LED that blinks with a luminous intensity of about 2,000 cd, and a medium-brightness C-type LED that is constantly on with a luminous intensity of about 2,000 cd. The high-brightness LED may include a high-brightness A-type LED having a luminous intensity of about 200,000 cd, and a high-brightness B-type LED having a luminous intensity of 100,000 cd.

[0123] Fig. 15 is a drawing for explaining an aviation obstacle indicator light according to a fourth modified example of the present application.

[0124] Referring to FIG. 15, an aviation obstacle warning light according to a fourth modified example of the present application may include a body part (100), a lighting part (200), a lighting control part (300), a control part (400), a solar cell panel (510), and a solar cell control part (520).

[0125] The body part (100), the lighting part (200), the lighting control part (300), and the control part (400) according to the fourth modified example of the present application are substantially the same as the body part (100), the lighting part (200), the lighting control part (300), and the control part (400) according to the embodiment of the present application, and therefore, a detailed description thereof is omitted.

[0126] The solar cell panel (510) may be installed on the upper surface of the body portion (100). Electric energy generated from sunlight may be stored through the solar cell panel (510). The electric energy generated through the solar cell panel (510) may be used for the light emission of the lighting portion (200) and the operation of the control portion (400), but is not limited thereto.

[0127] The above solar cell control unit (520) can adjust the angle of the solar cell panel (510) from the body unit (100). Accordingly, the efficiency of electric energy generated from sunlight can be increased.

[0128] Fig. 16 is a drawing for explaining an aviation obstacle indicator light according to a fifth modified example of the present application.

[0129] Referring to FIG. 16, an aviation obstacle warning light according to a fifth modified example of the present application may include a body part (100), a plurality of lighting parts (200), a lighting control part (300), and a control part (400).

[0130] The body part (100), the lighting control part (300), and the control part (400) according to the fifth modified example of the present application are substantially the same as the body part (100), the lighting control part (300), and the control part (400) according to the embodiment of the present application, and therefore, a detailed description thereof is omitted.

[0131] A plurality of the lighting units (200) may be fixed on the outer surface of the body portion (100). The plurality of the lighting units (200) may be spaced apart from each other at a predetermined interval and arranged radially on the outer surface of the body portion (100). In addition, the lighting units (200) may be fixed at different heights on the outer surface of the body portion (100). For example, a first lighting unit (201), which is defined as at least a portion of the lighting unit (200), may be fixed at a first height on the outer surface of the body portion (100). A second lighting unit (202), which is defined as the remaining portion of the lighting units (200), may be fixed at a second height on the outer surface of the body portion (100). That is, the plurality of the lighting units (201, 202) may include at least two or more radial arrangements. The direction of the first lighting unit (201) fixed to the first height may be arranged so as to be different from the light-emitting direction of the second lighting unit (202) fixed to the second height. That is, the first lighting unit (201) fixed to the first height and the plurality of second lighting units (202) fixed to the second height may be arranged so as to be staggered from each other. In other words, the light-emitting directions of the plurality of first lighting units (201) and second lighting units (202) may be different from each other. Accordingly, the light-emitting efficiency of the lighting units (201, 202) is improved, and visibility can be greatly improved even at night.

[0132] Although not shown, a light source, LED, lighting unit (201, 202), solar panel, etc. may be additionally placed on the upper surface of the body portion (100), but this is not limited thereto.

[0133] Figures 17 to 19 are drawings for explaining an aviation obstacle indicator light according to a sixth modified example of the present application.

[0134] Referring to FIGS. 17 to 19, an aviation obstacle warning light according to a sixth modified example of the present application may include a body portion (100), a plurality of lighting portions (200), a lighting control portion (300), a control portion (400), a solar cell panel (510), a solar cell control portion (520), and an energy conversion member (530).

[0135] The body part (100), the lighting control part (300), and the control part (400) according to the sixth modified example of the present application are substantially the same as the body part (100), the lighting control part (300), and the control part (400) according to the embodiment of the present application, and therefore, a detailed description thereof is omitted.

[0136] A plurality of the lighting units (200) may be fixed on the outer surface of the body portion (100). The plurality of the lighting units (200) may be spaced apart from each other at a predetermined interval and arranged radially on the outer surface of the body portion (100). In addition, the lighting units (200) may be fixed at different heights on the outer surface of the body portion (100). For example, a first lighting unit (201), which is defined as at least a portion of the lighting unit (200), may be fixed at a first height on the outer surface of the body portion (100). A second lighting unit (202), which is defined as the remaining portion of the lighting units (200), may be fixed at a second height on the outer surface of the body portion (100). That is, the plurality of the lighting units (201, 202) may include at least two or more radial arrangements. The direction of the first lighting unit (201) fixed to the first height may be arranged so as to be different from the light-emitting direction of the second lighting unit (202) fixed to the second height. That is, the first lighting unit (201) fixed to the first height and the plurality of second lighting units (202) fixed to the second height may be arranged so as to be staggered from each other. In other words, the light-emitting directions of the plurality of first lighting units (201) and second lighting units (202) may be different from each other. Accordingly, the light-emitting efficiency of the lighting units (201, 202) is improved, and visibility can be greatly improved even at night.

[0137] The solar cell panel (510) may be installed on the upper surface of the body portion (100). Electric energy generated from sunlight may be stored through the solar cell panel (510). The electric energy generated through the solar cell panel (510) may be used for the light emission of the lighting portion (200) and the operation of the control portion (400), but is not limited thereto.

[0138] The above solar cell control unit (520) can adjust the angle of the solar cell panel (510) from the body unit (100). Accordingly, the efficiency of electric energy generated from sunlight can be increased.

[0139] The energy conversion member (530) is disposed on the lower surface of the body portion (100) and may be disposed adjacent to a transmission line. The energy conversion member (530) may convert electromagnetic waves generated from the transmission line into electrical energy. The energy conversion member (530) may include an antenna (531), a rectifier (532 to 535), an energy storage unit (536), and a ground unit (537).

[0140] The antenna (531) can convert electromagnetic waves generated from the transmission line or transmission tower into alternating current. The antenna (531) may be formed of a conductive material in the form of a fiber, mesh, or sheet. The conductive material may include at least one of a metal (e.g., aluminum, iron, etc.) or a conductive polymer. An input node into which the alternating current is input is provided through the antenna (531).

[0141] The above-mentioned alternating current may be a surface current generated when an electromagnetic wave generated from the transmission tower or the transmission line contacts a conductive object (the antenna (531)). The surface current may flow along the surface of the conductive object (the antenna (531)).

[0142] The rectifiers (532 to 535) above can rectify the AC current converted by the electromagnetic wave-current converter. The rectifiers (532 to 535) can transmit the rectified AC current to the energy storage unit (536). The rectifiers (532 to 535) may include a first diode (532) to a fourth diode (535).

[0143] The cathode of the first diode (532) may be connected to the input node. The anode of the first diode (532) may be connected to the anode of the third diode (534).

[0144] The anode of the third diode (534) may be connected to the anode of the first diode (532). The cathode of the third diode (534) may be connected to the anode of the fourth diode (535) and may be connected to the grounding portion (537) to provide grounding.

[0145] The cathode of the fourth diode (535) may be connected to the cathode of the second diode (533). The anode of the fourth diode (535) may be connected to the cathode of the third diode (534) and may be connected to the grounding portion (537) to provide grounding.

[0146] The energy storage unit (536) may include an energy storage element (e.g., a capacitor). One end of the energy storage unit (536) may be connected to the anode of the first diode (532) and the anode of the third diode (534). The other end of the energy storage unit (536) may be connected to the cathode of the second diode (533) and the cathode of the fourth diode (535).

[0147] Among the AC currents provided to the input node (AC current converted by the antenna (531), an AC current having a (-) polarity can be provided to the first node by passing through the first diode (532). Conversely, among the AC currents provided to the input node, an AC current having a (+) polarity can be provided to the second node by passing through the second diode (533). Accordingly, electric energy can be stored in the energy storage unit (536) connected to the first node and the second node.

[0148] In other words, by installing the circuit of the energy conversion member (530), electromagnetic waves naturally occurring in the transmission line can be converted into electrical energy. The converted electrical energy can be stored through the energy storage unit (536) of the energy conversion member (530). Accordingly, the lighting unit (513) can emit light on its own without the need for external power supply, thereby improving energy efficiency.

[0149] FIG. 20 is a drawing for explaining a processing line on which an aviation obstacle warning light is installed according to the seventh modified example of the present application, and FIGS. 21 to 23 are drawings for explaining an aviation obstacle warning light according to the seventh modified example of the present application.

[0150] Referring to FIGS. 20 to 23, an aviation obstacle warning light according to a seventh modified example of the present application can be connected to an overhead line (20) providing a ground (G). The aviation obstacle warning light can be installed on a transmission line (10), an overhead line (20), etc. between buildings, structures, transmission towers (2). The aviation obstacle warning light can include a body (100), a lighting unit (200), a lighting control unit (300), a control unit (400), a solar panel (510), an energy conversion member (530), a connector (610), an extension unit (700), and a plate (800).

[0151] The above-mentioned transmission line (10) can transmit electric energy produced at a power plant to a substation or from a substation to another substation. The above-mentioned transmission line (10) can generally supply electric power underground using a support structure such as the above-mentioned transmission tower (2).

[0152] The above-mentioned overhead line (20), like the above-mentioned transmission line (10), can be installed by connecting between supports such as the above-mentioned transmission tower (2). The above-mentioned overhead line (20) provides grounding (G) from the ground (1) and can be installed at a higher position than the above-mentioned transmission line (10). The above-mentioned overhead line (20) can shield an induced lightning, which is an abnormal voltage that causes a problem in the above-mentioned transmission line (10).

[0153] The body part (100), the lighting part (200), the lighting control part (300), and the control part (400) according to the seventh modified example of the present application are substantially the same as the body part (100), the lighting part (200), the lighting control part (300), and the control part (400) according to the embodiment of the present application, and the solar cell panel (510) and the energy conversion member (530) according to the seventh modified example of the present application are substantially the same as the solar cell panel (510) and the energy conversion member (530) according to the sixth modified example of the present application, and therefore, a detailed description thereof will be omitted.

[0154] The connector (610) may include at least a portion of the processed ground line (20). The connector (610) may include a fixed connector (611, 612) and a ground connector (613).

[0155] The above fixed connectors (611) can be arranged in pairs spaced apart from each other on the processing line (20). The above fixed connectors (611, 612) can include an upper connector (611a, 612a), a lower connector (611b, 612b), and a connecting member.

[0156] The upper connector (611a, 612a) may surround the upper end of the processing line (20). For example, the upper connector (611a, 612a) may have a hollow semi-cylindrical shape. As illustrated in Fig. 22, the upper connector (611a, 612a) may include flanges at both ends.

[0157] The lower connector (611b, 612b) may wrap around the lower end of the processing line (20). The lower connector (611b, 612b) may have a hollow semi-cylindrical shape like the upper connector (611a, 612a). Similarly, as illustrated in FIG. 22, the lower connector (611b, 612b) may include flanges at both ends.

[0158] The above-described joining member can join the upper connector (611a, 612a) and the lower connector (611b, 612b). The upper connector (611a, 612a) and the lower connector (611b, 612b) can be fixed on the processing line (20) through the joining member. For example, the joining member can include, but is not limited to, a bolt and a nut.

[0159] The above ground connector (613) may be located between a pair of the fixed connectors (611, 612). The above ground connector (613) may include an upper connector (613a), a lower connector (613b), and a through hole (613c).

[0160] The upper connector (613a) may surround the upper end of the processing line (20). For example, the upper connector (613a) may have a hollow semi-cylindrical shape. As illustrated in Fig. 23, the upper connectors (611a, 612a) may include flanges at both ends.

[0161] The lower connector (613b) may surround the lower end of the processing line (20). For example, the lower connector (613b) may have a hollow semi-cylindrical shape. As illustrated in Fig. 23, the lower connector (613b) may include flanges at both ends. The lower connector (613b) may include a through hole (613c) formed penetrating toward the transmission line (10).

[0162] The ground wire (713) described later can be inserted into the above through hole (613c). The processed ground wire (20) and the ground wire (713) can be electrically connected through the above through hole (613c).

[0163] The above extension portions may be formed to extend downward from the connector (610). The above extension portions may include support rods (711, 712) and ground wires (713).

[0164] The above support rods (711, 712) may be formed to extend downward from a pair of the above fixed connectors (611, 612), respectively. Accordingly, the support rods (711, 712) may be formed to extend downward from the lower end of the above-mentioned processing wire (20).

[0165] The ground wire (713) may be formed to extend downward from the ground connector (613). As described above, the upper end of the ground wire (713) may be inserted into the through hole (613c) formed in the lower connector (613b) of the ground connector (613). Accordingly, the ground wire (713) may be electrically connected to the overhead wire (20). The lower end of the ground wire (713) may be electrically connected to the lighting unit (200). Through the ground wire (713), a ground (G) may be provided to the light-emitting member (225) of the lighting unit (200), the solar cell panel (510), and the energy conversion member (530).

[0166] The above plate (800) can connect a pair of the above support rods (711, 712). The plate (800) can have a flat plate shape. The body part (100), the lighting part (200), the control part (400), and the solar cell panel (510) can be arranged on the plate (800).

[0167] Fig. 24 is a drawing for explaining an aviation obstacle indicator light according to the eighth modified example of the present application.

[0168] Referring to FIG. 24, an aviation obstacle warning light according to the eighth modified example of the present application may include a body part (100), a lighting part (200), a lighting control part (300), a control part (400), a power part (500), and a connector (610).

[0169] The lighting unit (200), the lighting control unit (300), and the control unit (400) according to the eighth modified example of the present application are substantially the same as the lighting unit (200), the lighting control unit (300), and the control unit (400) according to the embodiment of the present application, and therefore, a detailed description thereof is omitted.

[0170] The above body part (100) can be placed in the upper central area of ​​the connector (610).

[0171] The above power supply unit (500) may include a solar cell panel (510) and an energy conversion member (530).

[0172] The solar cell panel (510) may be positioned on the upper side of the connector (610). The solar cell panel (510) may be positioned at a location that does not overlap with the body portion (100). Electric energy generated from sunlight through the solar cell panel (510) may be stored through the control unit. Accordingly, the light-emitting member (225) of the lighting unit (200) may emit light on its own without the need for external power supply, thereby improving energy efficiency.

[0173] The energy conversion member (530) is arranged on the lower connector that surrounds the lower end of the processing line (20), and may be arranged close to the transmission line (10). Through the energy conversion member (530), electromagnetic waves generated from the transmission line (10) can be converted into electrical energy and stored.

[0174] The connector (610) may include at least a portion of the processed branch line (20). The inner surface of the connector (610) may include a curved surface to increase the contact area with the processed branch line (20). For example, the outer surface of the connector (610) may include a shape of a square pillar extending in the longitudinal direction of the processed branch line (20) to ensure the stability of the component. The connector (610) may include an upper connector that wraps around the upper end of the processed branch line (20), and a lower connector that wraps around the lower end of the processed branch line (20).

[0175] Fig. 25 is a drawing for explaining an aviation obstacle indicator light according to the ninth modified example of the present application.

[0176] Referring to Fig. 25, an aviation obstacle warning light according to a ninth modified example of the present application is connected to an overhead line (20) providing a ground (G) and can be installed at a higher position than a transmission line (10). The aviation obstacle warning light can include a body (100), a lighting unit (200), a lighting control unit (300), a control unit (400), a battery (450), a connecting line (501), a solar panel (510), an energy conversion member (530), a first connector (620), and a second connector (630).

[0177] The lighting unit (200) and the lighting control unit (300) according to the ninth modified example of the present application are substantially the same as the lighting unit (200) and the lighting control unit (300) according to the embodiment of the present application, and the solar cell panel (510) and the energy conversion member (530) according to the ninth modified example of the present application are substantially the same as the solar cell panel (510) and the energy conversion member (530) according to the sixth modified example of the present application, so a detailed description thereof is omitted.

[0178] The above body part (100) is coupled to the upper end of the first connector (620) and can be installed on a building, structure, power transmission line (10) or overhead line (20). The body part (100) can be installed adjacent to the solar cell panel (510) and energy conversion member (530).

[0179] The above control unit (400) may be fixed to the lower end of the first connector (620). The above control unit (400) may include a light sensor (CdS), a global positioning system (GPS), and a maximum power point tracking (MPPT) controller.

[0180] The above battery (450) can be fixed to the lower end of the first connector (620). The battery (450) can supply power to the light-emitting member (225) of the lighting unit (200).

[0181] The above connecting line (501) can electrically connect the lighting unit (200) and the battery (450) and / or the solar panel (510) and / or the energy conversion member (530).

[0182] The solar cell panel (510) can be fixed to the upper end of the second connector (630), and the energy conversion member (530) can be fixed to the lower end of the second connector (630).

[0183] The first connector (620) and the second connector (630) may include at least a portion of the processed ground wire (20).

[0184] In other words, depending on the state of the transmission line (10) or the overhead line (20), the positions of the body part (100) and the lighting part (200) can be selected and installed. That is, the lighting part (200) can be placed at the top or bottom of the overhead line (20) depending on the situation. Depending on the placement of the lighting part (200), the placement of the control part (400) and the battery (450) can vary. Accordingly, the convenience of the worker installing the aviation obstacle warning light can be improved, and the visibility of the aviation obstacle warning light can be further improved.

[0185] Fig. 26 is a drawing for explaining an aviation obstacle indicator light according to the 10th modified example of the present application.

[0186] Referring to FIG. 26, an aviation obstacle warning light according to the 10th modified example of the present application may include a body part (100), a lighting part (200), a lighting control part (300), a control part (400), a battery (450), a connecting line (501), a solar panel (510), an energy conversion member (530), a first connector (620), and a second connector (630).

[0187] The lighting unit (200) and the lighting control unit (300) according to the 10th modified example of the present application are substantially the same as the lighting unit (200) and the lighting control unit (300) according to the embodiment of the present application, and the solar cell panel (510) and the energy conversion member (530) according to the 10th modified example of the present application are substantially the same as the solar cell panel (510) and the energy conversion member (530) according to the 6th modified example of the present application, so a detailed description thereof is omitted.

[0188] The above body part (100) is coupled to the lower end of the first connector (620) and can be installed on a building, structure, power transmission line (10) or overhead line (20). The body part (100) can be installed adjacent to the solar cell panel (510) and energy conversion member (530).

[0189] The above control unit (400) may be fixed to the upper end of the first connector (620). The control unit (400) may include a light sensor (CdS), a global positioning system (GPS), and a maximum power point tracking (MPPT) controller.

[0190] The above battery (450) can be fixed to the upper end of the first connector (620). The battery (450) can supply power to the light-emitting member (225) of the lighting unit (200).

[0191] The above connecting line (501) can electrically connect the lighting unit (200) and the battery (450) and / or the solar panel (510) and / or the energy conversion member (530).

[0192] The solar cell panel (510) can be fixed to the upper end of the second connector (630), and the energy conversion member (530) can be fixed to the lower end of the second connector (630).

[0193] The first connector (620) and the second connector (630) may include at least a portion of the processed ground wire (20).

[0194] In other words, depending on the state of the transmission line (10) or the overhead line (20), the positions of the body part (100) and the lighting part (200) can be selected and installed. That is, the lighting part (200) can be placed at the top or bottom of the overhead line (20) depending on the situation. Depending on the placement of the lighting part (200), the placement of the control part (400) and the battery (450) can vary. Accordingly, the convenience of the worker installing the aviation obstacle warning light can be improved, and the visibility of the aviation obstacle warning light can be further improved.

[0195] Figure 27 is a drawing for explaining an aviation obstacle indicator light according to the 11th modified example of the present application.

[0196] Referring to FIG. 27, an aviation obstacle warning light according to the 11th modified example of the present application may include a plurality of body parts (100), a lighting part (200), a lighting control part (300), a control part (400), a battery (450), a connecting line (501), a solar panel (510), an energy conversion member (530), a first connector (620), and a second connector (630).

[0197] The lighting unit (200) and the lighting control unit (300) according to the 11th modified example of the present application are substantially the same as the lighting unit (200) and the lighting control unit (300) according to the embodiment of the present application, and the solar cell panel (510) and the energy conversion member (530) according to the 11th modified example of the present application are substantially the same as the solar cell panel (510) and the energy conversion member (530) according to the 6th modified example of the present application, so a detailed description thereof is omitted.

[0198] The above body part (100) is coupled to the upper or lower end of the first connector (620) and can be installed in multiple numbers on a building, structure, power transmission line (10) or overhead line (20). A plurality of the above body parts (100) can be installed adjacent to the solar cell panel (510) and energy conversion member (530).

[0199] The above control unit (400) may be fixed to the upper or lower portion of the first connector (620). The above control unit (400) may include a light sensor (CdS), a global positioning system (GPS), and a maximum power point tracking (MPPT) controller.

[0200] The above battery (450) can be fixed to the top or bottom of the first connector (620). The battery (450) can supply power to the light-emitting member (225) of the lighting unit (200).

[0201] The above connecting line (501) can electrically connect the lighting unit (200) and the battery (450) and / or the solar panel (510) and / or the energy conversion member (530).

[0202] The solar cell panel (510) can be fixed to the upper end of the second connector (630), and the energy conversion member (530) can be fixed to the lower end of the second connector (630).

[0203] The first connector (620) and the second connector (630) may include at least a portion of the processed ground wire (20).

[0204] In other words, depending on the condition of the transmission line (10) or the overhead line (20), the location and number of the body part (100) and the lighting part (200) can be selected and installed. That is, the lighting parts (200) can be arranged in multiple positions at the upper end of the overhead line (20) or in multiple positions at the lower end, depending on the situation. Accordingly, the visibility of the aviation obstacle warning light can be further improved.

[0205] FIG. 28 is a drawing for explaining an existing aviation obstacle indicator in which an aviation obstacle indicator is installed according to the 12th modified example of the present application, and FIG. 29 is a drawing for explaining an aviation obstacle indicator according to the 12th modified example of the present application.

[0206] Referring to FIGS. 28 and 29, an aviation obstacle warning light according to the 12th modified example of the present application can be attached to an existing aviation obstacle sign (30) installed on a transmission line (10) or overhead line (20) between a building, structure, or transmission tower (2). The aviation obstacle light can include a base (50), a body (100), a lighting unit (200), a lighting control unit (300), and a solar panel (510).

[0207] The existing aviation obstacle sign (30) may generally include a hemispherical upper structure and a hemispherical lower structure. The existing aviation obstacle sign (30) may be installed on the overhead wire (20) or the top of a high-rise building by combining the upper structure and the lower structure.

[0208] The base (50) may have a hollow hemisphere shape to be attached to the existing aviation obstacle sign (30). The base (50) may be attached to the existing aviation obstacle sign (30) using bolts and nuts, and / or an adhesive. The base (50) may be manufactured according to the curvature of the existing aviation obstacle sign (30). The base (50) may be manufactured from a material that is easy to process, has insulating properties, and is flame retardant. For example, the base (50) may be manufactured from a plastic having a hardness such as PVC (Poly Vinyl Chloride), but is not limited thereto.

[0209] The above bolt can be installed by penetrating the existing aviation obstacle indicator (30) and the base (50). The nut can be fastened to the bolt to securely connect the existing aviation obstacle indicator (30) and the base (50).

[0210] The above adhesive can be laminated on the existing aviation obstacle sign (30). The base (50) can be fixed on the existing aviation obstacle sign (30) through the adhesive.

[0211] One or more of the above solar cell panels (510) can be placed on the base (50).

[0212] The body part (100), the lighting part (200), and the lighting control part (300) according to the 12th modified example of the present application are substantially the same as the body part (100), the lighting part (200), and the lighting control part (300) according to the embodiment of the present application, and the solar cell panel (510) according to the 12th modified example of the present application is substantially the same as the solar cell panel (510) according to the 6th modified example of the present application, so a detailed description thereof is omitted.

[0213] Fig. 30 is a drawing for explaining an aviation obstacle indicator light according to the 13th modified example of the present application.

[0214] Referring to Fig. 30, an aviation obstacle warning light according to the 13th modified example of the present application can be attached to an existing aviation obstacle warning light (30). The aviation obstacle warning light can include a base (50), a body (100), a lighting unit (200), a lighting control unit (300), a solar panel (510), an energy conversion member (530), and a connector (610).

[0215] The base (50) may have a hollow hemisphere shape to be attached to the existing aviation obstacle sign (30). The base (50) may be attached to the existing aviation obstacle sign (30) using bolts and nuts, and / or an adhesive. The base (50) may be manufactured according to the curvature of the existing aviation obstacle sign (30). The base (50) may be manufactured from a material that is easy to process, has insulating properties, and is flame retardant. For example, the base (50) may be manufactured from a plastic having a hardness such as PVC (Poly Vinyl Chloride), but is not limited thereto.

[0216] The above body part (100) is coupled to the upper end of the base (50) and can be installed on a building, structure, power transmission line (10) or overhead line (20). The body part (100) can be installed adjacent to the solar cell panel (510) and energy conversion member (530).

[0217] The lighting unit (200) and the lighting control unit (300) according to the 13th modified example of the present application are substantially the same as the lighting unit (200) and the lighting control unit (300) according to the embodiment of the present application, and the solar cell panel (510) and the energy conversion member (530) according to the 13th modified example of the present application are substantially the same as the solar cell panel (510) and the energy conversion member (530) according to the 6th modified example of the present application, so a detailed description thereof is omitted.

[0218] The solar cell panel (510) can be fixed to the upper part of the connector (610), and the energy conversion member (530) can be fixed to the lower part of the connector (610).

[0219] The connector (610) may include a component that surrounds at least a portion of the processed ground line (20). The connector (610) may be installed adjacent to the existing aviation obstacle indicator (30).

[0220] Figure 31 is a drawing for explaining an aviation obstacle indicator light according to the 14th modified example of the present application.

[0221] Referring to Fig. 31, an aviation obstacle indicator according to the 14th modified example of the present application can be attached to an existing aviation obstacle indicator (30). The aviation obstacle indicator can include a base (50), a body (100), a lighting unit (200), a lighting control unit (300), a solar panel (510), an energy conversion member (530), and a connector (610).

[0222] The base (50) may have a hollow hemisphere shape to be attached to the existing aviation obstacle sign (30). The base (50) may be attached to the existing aviation obstacle sign (30) using bolts and nuts, and / or an adhesive. The base (50) may be manufactured according to the curvature of the existing aviation obstacle sign (30). The base (50) may be manufactured from a material that is easy to process, has insulating properties, and is flame retardant. For example, the base (50) may be manufactured from a plastic having a hardness such as PVC (Poly Vinyl Chloride), but is not limited thereto.

[0223] The above body part (100) is coupled to the lower end of the base (50) and can be installed on a building, structure, power transmission line (10) or overhead line (20). The body part (100) can be installed adjacent to the solar cell panel (510) and energy conversion member (530).

[0224] The lighting unit (200) and the lighting control unit (300) according to the 14th modified example of the present application are substantially the same as the lighting unit (200) and the lighting control unit (300) according to the embodiment of the present application, and the solar cell panel (510) and the energy conversion member (530) according to the 14th modified example of the present application are substantially the same as the solar cell panel (510) and the energy conversion member (530) according to the 6th modified example of the present application, so a detailed description thereof is omitted.

[0225] The solar cell panel (510) can be fixed to the upper part of the connector (610), and the energy conversion member (530) can be fixed to the lower part of the connector (610).

[0226] The connector (610) may include a component that surrounds at least a portion of the processed ground line (20). The connector (610) may be installed adjacent to the existing aviation obstacle indicator (30).

[0227] In other words, depending on the condition of the transmission line (10) or the overhead line (20), the positions of the body part (100) and the lighting part (200) can be selected and installed. That is, the lighting part (200) can be placed at the top or bottom of the overhead line (20) depending on the situation. Accordingly, the visibility of the aviation obstacle warning light can be further improved.

[0228] FIG. 32 and FIG. 33 are drawings for explaining an aviation obstacle indicator light according to the 15th modified example of the present application.

[0229] Referring to FIGS. 32 and 33, the aviation obstacle warning light according to the 15th modified example of the present application may include a body part (100), a lighting part (200), and a lighting control part (300).

[0230] The body portion (100) may have a hollow cylindrical shape or a hollow polygonal column shape. As illustrated in FIG. 33, the body portion (100) may have a shape such as a cylinder, a triangular column, or a square column. Wires, circuits, batteries, and the like may be embedded inside the body portion (100).

[0231] The above lighting unit (200) may be formed in multiple pieces and fixed on the outer surface of the body unit (100). The lighting unit (200) unit may be defined as a single unit including a plate (200a), a first lighting unit (201), a second lighting unit (202), and a third lighting unit (203). The lighting unit (200) unit may include the first lighting unit (201), the second lighting unit (202), and the third lighting unit (203) being formed integrally through the plate (200a).

[0232] The above plate (200a) can fix the first lighting unit (201), the second lighting unit (202), and the third lighting unit (203) on the outer surface of the body part (100). The plate (200a) to which the first lighting unit (201), the second lighting unit (202), and the third lighting unit (203) are fixed can be attached on the outer surface of the body part (100). For example, the plate (200a) can include a curved surface.

[0233] For example, if the body part (100) is cylindrical, the plate (200a) may include a portion that surrounds 1 / 4 of the outer surface of the body part (100). That is, one end and the other end of the plate (200a) may include a portion that surrounds the outer surface of the body part (100) within a 90-degree range based on the imaginary central axis of the body part (100).

[0234] For another example, when the body part (100) is a triangular prism, the plate (200a) may include a portion that surrounds 1 / 3 of the side surface of the body part (100). That is, one end and the other end of the plate (200a) may include a portion that surrounds the entirety of one of the three side surfaces of the body part (100) that is a triangular prism. In this case, in order to fix the body part (100) having a flat surface and the plate (200a) having a curved surface, the lighting part (200) may further include upper and lower plates (200b).

[0235] For another example, if the body part (100) is a square column, the plate (200a) may include a portion that surrounds 1 / 4 of the side surface of the body part (100). That is, one end and the other end of the plate (200a) may include a portion that surrounds the entirety of one of the four side surfaces of the body part (100) that is a square column. In this case, in order to fix the body part (100) having a flat surface and the plate (200a) having a curved surface, the lighting part (200) may further include upper and lower plates (200b).

[0236] As described above, the upper and lower plates (200b) can be fixed between the body portion (100) having a flat surface and the plate (200a) having a curved surface. The upper and lower plates (200b) can fix the upper and lower portions of the plate (200a) from the upper and lower portions of the body portion (100) while simultaneously blocking the gap therebetween.

[0237] The first lighting unit (201), the second lighting unit (202), and the third lighting unit (203) of the lighting unit may be fixed at different heights on the outer surface of the body part (100). In addition, the first lighting unit (201), the second lighting unit (202), and the third lighting unit (203) of the lighting unit may emit light in different directions on the outer surface of the body part (100). That is, the first lighting unit (201), the second lighting unit (202), and the third lighting unit (203) fixed at different heights may include at least three or more radial arrangements.

[0238] The first lighting unit (201) may be defined as at least a portion of the lighting unit. The first lighting unit (201) may be fixed at a first height on the outer circumferential surface of the body unit (100). The first lighting unit (201) may include a plurality of independent light-emitting members, and the plurality of light-emitting members of the first lighting unit (201) may each emit light in different directions.

[0239] The second lighting unit (202) may be defined as another part of the lighting unit. The second lighting unit (202) may be fixed at a second height on the outer circumferential surface of the body unit (100). The second lighting unit (202) may include a plurality of independent light-emitting members, and the plurality of light-emitting members of the second lighting unit (202) may each emit light in different directions.

[0240] The third lighting unit (203) may be defined as the remaining part of the lighting unit. The third lighting unit (203) may be fixed at a third height on the outer circumference of the body unit (100). The third lighting unit (203) may include a plurality of independent light-emitting members, and the plurality of light-emitting members of the third lighting unit (203) may each emit light in different directions.

[0241] When the first height is higher than the second height and the second height is higher than the third height, the first lighting unit (201) may include two independent light-emitting members, the second lighting unit (202) may include three independent light-emitting members, and the third lighting unit (203) may include four independent light-emitting members, respectively. The nine independent light-emitting members may each emit light in different directions. The first lighting unit (201) fixed to the first height, the second lighting unit (202) fixed to the second height, and the third lighting unit (203) fixed to the third height may be arranged to be staggered from each other. For example, the nine independent light-emitting members may be installed at 10-degree intervals, and may emit light in different directions on the outer surface of the body portion (100) within a 90-degree range with respect to an imaginary central axis of the body portion (100).

[0242] As a result, a plurality of the above lighting units can be combined according to the shape of the body portion (100), and accordingly, a plurality of the above light-emitting members can be efficiently arranged. In addition, as a plurality of the above light-emitting members are installed at various heights to have various light-emitting angles, the light-emitting efficiency of the above lighting units is improved, and visibility can be greatly improved even at night.

[0243] Since the above lighting control unit (300) is substantially the same as the lighting control unit (300) according to the embodiment of the present application, a detailed description is omitted.

[0244] FIGS. 34 and 35 are drawings for explaining an aviation obstacle indicator light according to the 16th modified example of the present application.

[0245] Referring to FIGS. 34 and 35, the aviation obstacle warning lights according to the 16th modified example of the present application can be installed at the upper, middle, and lower portions of the transmission tower (2), respectively. The aviation obstacle warning lights can include a body portion (100), a lighting portion (200), and a lighting control portion.

[0246] The body portion (100) may have a hollow cylindrical shape or a hollow polygonal column shape. As illustrated in FIG. 35, the body portion (100) may have a shape such as a cylinder, a triangular column, or a square column. Wires, circuits, batteries, and the like may be embedded within the body portion (100).

[0247] The above lighting unit (200) may be formed as a single unit and fixed on the outer surface of the body part (100). The lighting unit (200) may be defined as a single unit including a first lighting unit (201), a second lighting unit (202), and a third lighting unit (203). For example, when the body part (100) is a cylinder, the first lighting unit (201), the second lighting unit (202), and the third lighting unit (203) may include a unit that surrounds the entire outer surface of the body part (100). That is, one end and the other end of the plate (200a) may include a unit that surrounds the outer surface of the body part (100) within a range of 360 degrees based on an imaginary central axis of the body part (100).

[0248] The first lighting unit (201), the second lighting unit (202), and the third lighting unit (203) of the lighting unit may be fixed at different heights on the outer surface of the body part (100). In addition, the first lighting unit (201), the second lighting unit (202), and the third lighting unit (203) of the lighting unit may emit light in different directions on the outer surface of the body part (100). That is, the first lighting unit (201), the second lighting unit (202), and the third lighting unit (203) fixed at different heights may include at least three or more radial arrangements.

[0249] The first lighting unit (201) may be defined as at least a portion of the lighting unit. The first lighting unit (201) may be fixed at a first height on the outer circumferential surface of the body unit (100). The first lighting unit (201) may include a plurality of independent light-emitting members, and the plurality of light-emitting members of the first lighting unit (201) may each emit light in different directions.

[0250] The second lighting unit (202) may be defined as another part of the lighting unit. The second lighting unit (202) may be fixed at a second height on the outer circumferential surface of the body unit (100). The second lighting unit (202) may include a plurality of independent light-emitting members, and the plurality of light-emitting members of the second lighting unit (202) may each emit light in different directions.

[0251] The third lighting unit (203) may be defined as the remaining part of the lighting unit. The third lighting unit (203) may be fixed at a third height on the outer circumference of the body unit (100). The third lighting unit (203) may include a plurality of independent light-emitting members, and the plurality of light-emitting members of the third lighting unit (203) may each emit light in different directions.

[0252] When the first height is higher than the second height and the second height is higher than the third height, the first lighting unit (201) may include eight independent light-emitting members, the second lighting unit (202) may include twelve independent light-emitting members, and the third lighting unit (203) may include sixteen independent light-emitting members, respectively. The 36 independent light-emitting members may each emit light in different directions. The first lighting unit (201) fixed to the first height, the second lighting unit (202) fixed to the second height, and the third lighting unit (203) fixed to the third height may be arranged to be staggered from each other. For example, 36 independent light-emitting elements are installed at 10-degree intervals, and can emit light in different directions on the outer surface of the body (100) within a 360-degree range based on the imaginary central axis of the body (100).

[0253] As a result, the lighting unit can be simply installed at each of the upper, middle, and lower portions of the transmission tower (2), and thus, a plurality of the light-emitting members can be efficiently arranged. In addition, since a plurality of the light-emitting members are installed at various heights to have various light-emitting angles, the light-emitting efficiency of the lighting unit is improved, and visibility can be significantly improved even at night.

[0254] Since the above lighting control unit is substantially the same as the lighting control unit (300) according to the embodiment of the present application, a detailed description is omitted.

[0255] Although not shown, the aviation obstacle warning light according to the 17th modified example of the present application may include a lighting unit including a light-emitting member, a battery, a solar panel, a connecting line, and a controller.

[0256] The above lighting unit can be installed on an overhead wire. Since the lighting unit is substantially the same as the lighting unit according to the embodiment of the present application, a detailed description thereof will be omitted.

[0257] The above battery may be installed on a transmission tower. The battery may selectively supply power to the light-emitting element of the lighting unit, or may not supply power to the light-emitting element.

[0258] The above solar cell panel may be installed on a transmission tower. The above solar cell panel may selectively supply or not supply power to the light-emitting member of the lighting unit.

[0259] The above connecting line can electrically connect the battery and the lighting unit, and electrically connect the solar panel and the lighting unit. The connecting line can be attached along the overhead wire.

[0260] The controller can selectively supply power from the battery or the solar panel to the light-emitting member of the lighting unit.

[0261] In other words, the battery and the solar panel may be installed on a transmission tower, and the lighting unit may be installed on an overhead line. That is, the battery and the solar panel may supply power to the light-emitting member through a connecting line attached along the overhead line. Accordingly, the convenience of the worker installing the aircraft obstacle warning light may be improved, and the visibility of the aircraft obstacle warning light may be further improved.

[0262] FIG. 36 is a drawing for explaining a lighting unit of an aviation obstacle indicator according to the 17th modified example of the present application, FIG. 37 is a drawing for explaining a support part according to the 17th modified example of the present application, FIG. 38 is a perspective view for explaining a support plate according to the 17th modified example of the present application, FIG. 39 is a drawing for explaining that a plurality of support parts are combined according to the 17th modified example of the present application, FIG. 40 is a perspective view for explaining a support part according to the 17th modified example of the present application, and FIGS. 41 and 42 are perspective views for explaining that an angle of a lighting part is adjusted according to the 17th modified example of the present application.

[0263] Referring to FIGS. 36 to 42, an aviation obstacle warning light according to the 17th modified example of the present application can be installed on transmission lines, overhead lines, etc. between buildings, structures, transmission towers, etc. The aviation obstacle warning light can include a body (50) and a lighting unit (1).

[0264] The body portion (50) may have a hollow cylindrical shape or a hollow polygonal column shape. For example, the body portion (50) may have a shape such as a cylinder, a triangular column, a square column, or a hexagonal column, but is not limited thereto. Wires, circuits, batteries, etc. may be embedded inside the body portion (50).

[0265] The above lighting unit (1) can be coupled to the outer circumference of the body portion (50). The lighting unit (1) can surround at least a portion of the outer circumference of the body portion (50). One lighting unit (1) can be formed in a fan shape to surround 1 / 4 of the outer circumference of the body portion (50). As illustrated in FIG. 39, a plurality of lighting units (1) can surround the entire outer circumference of the body portion (50). The lighting unit (1) can include a support portion (100) and a lighting unit (200) that are coupled to be formed as one piece.

[0266] The above support member (100) can be attached to the outer circumferential surface of the body member (50) and support the lighting member (200). The support member (100) can be formed to extend in the longitudinal direction of the body member (50). The support member (100) can include a plurality of support plates (110, 120, 130, 140, 150) spaced apart from each other, and upper and lower plates (101) connecting the plurality of support plates (110, 120, 130, 140, 150).

[0267] The upper and lower plates (101) can be fixed between the body portion (50) having a curved surface and the support plate (100) having a flat surface. The upper and lower plates (101) can fix the upper and lower portions of the support plate (100) from the upper and lower portions of the body portion (50) while blocking the gap therebetween.

[0268] The plurality of support plates (110, 120, 130, 140, 150) extend in the longitudinal direction of the body portion (50) as described above, and may be spaced apart from each other along the outer circumferential surface of the body portion (50). The support plates (110, 120, 130, 140, 150) may be combined with a single or a plurality of lighting units (200). The plurality of support plates (110, 120, 130, 140, 150) may include a first plate (110), a second plate (120), a third plate (130), a fourth plate (140), and a fifth plate (150).

[0269] The above first plate (110) is coupled to the outer surface of the body portion (50), but can be placed in the central portion of the support portion (100).

[0270] The second plate (120) is coupled to the outer surface of the body portion (50), but may be spaced apart from the first plate (110) in one direction.

[0271] The third plate (130) is coupled to the outer surface of the body portion (50), but can be spaced apart from the first plate (110) in the other direction.

[0272] The second plate (120) and the third plate (130) may be spaced apart from each other on both sides of the first plate (110) along the outer circumference of the body portion (50). The second plate (120) and the third plate (130) may be arranged symmetrically with respect to the first plate (110).

[0273] The fourth plate (140) is coupled to the outer surface of the body portion (50), but may be spaced apart from the second plate (120) in one direction.

[0274] The fifth plate (150) is coupled to the outer surface of the body portion (50), but can be spaced apart from the third plate (130) in the other direction.

[0275] The fourth plate (140) and the fifth plate (150) may be spaced apart from each other on both sides of the second plate (120) and the third plate (130) along the outer circumference of the body portion (50). The fourth plate (140) and the fifth plate (150) may be arranged symmetrically with respect to the first plate (110).

[0276] According to one embodiment, the first plate (110), the second plate (110), the third plate (130), the fourth plate (140), and the fifth plate (150) may include a heat dissipation structure. The support plates (110, 110, 130, 140, 150) may be described through the first plate (110).

[0277] The above support plate (110) may include a first guide groove (111) and a second guide groove (112) that extend in the longitudinal direction of the support plate (110) and are spaced apart from each other, and a joining line (113) that is arranged between the first guide groove (111) and the second guide groove (112).

[0278] The above-mentioned joining line (113) can be inserted into the joining groove of the lighting unit (200). Accordingly, the lighting unit (200) and the supporting plate (110) can be joined. A plurality of holes can be formed in the joining line (113). For example, as illustrated in FIG. 38, a first through hole (110a) and a second through hole (110b) can be formed in the joining line (113). The first through hole (110a) can be used to pull out a wire connected to the lighting unit (200) when the lighting unit (200) and the supporting plate (110) are joined. Alternatively, the second through hole (110b) can be used to insert a screw to more strongly join the lighting unit (200) to the supporting plate (110).

[0279] The above support plate (110) may include a first side wall (114) and a second side wall (115) extending in the longitudinal direction of the support plate (110) and in the vertical direction of the lower surface of the support plate (110) on both sides of the support plate (110). Between the first side wall (114) and the second side wall (115), the first guide groove (111), the joining line (113), and the second guide groove (112) may be sequentially arranged.

[0280] The first side wall (114) and the second side wall (115) may be divided into an inner side and an outer side, respectively. The inner side of the first side wall (114) and the second side wall (115) may be a portion exposed in the direction of the first guide groove (111), the joining line (113), and the second guide groove (112). Alternatively, the outer side of the first side wall (114) and the second side wall (115) may be a portion facing the inner side and exposed to the outside of the support plate (110).

[0281] According to one embodiment, the inner sides of the first side wall (114) and the second side wall (115) may have an inclined shape. Accordingly, when the lighting unit (200) and the support plate (110) are combined, the outer side of the lighting unit (200) may be supported by the first side wall (114) and the second side wall (115) of the support plate (110).

[0282] The support plate (110) may further include first and second fasteners (116a, 116b) and first and second heat dissipation members (117a, 117b). Specifically, the first fastener (116a) may protrude from the lower surface of the support plate (110) in a direction opposite to the first side wall (114). In contrast, the second fastener (116b) may protrude from the lower surface of the support plate (110) in a direction opposite to the second side wall (115).

[0283] The first and second heat dissipation members (117a, 117b) may be arranged between the first and second fasteners (116a, 116b). Specifically, for example, the first heat dissipation member (117a) may protrude in an opposite direction of the first guide groove (111) from the lower surface of the support plate (110). In contrast, the second heat dissipation member (117b) may protrude in an opposite direction of the second guide groove (112) from the lower surface of the support plate (110). As the surface area of ​​the support plate (110) is increased by the first and second heat dissipation members (117a, 117b), the heat dissipation efficiency of the lighting unit (200) may be improved.

[0284] The above lighting unit (200) can be coupled with the support unit (100). As illustrated in FIG. 41, the lighting unit (200) can be rotated relative to the support unit (100), so that the coupling angle of the lighting unit (200) can be adjusted. The lighting unit (200) can be coupled to the body unit (50) via a plurality of the support plates (110, 120, 130, 140, 150). The lighting unit (200) can include a light-emitting member and emit light radially from the body unit (50). The lighting unit (200) can include a first light (201), a second light (202), a third light (203), a fourth light (204), and a fifth light (205).

[0285] The above light-emitting member may include irradiating light through an LED (Light Emitting Diode).

[0286] The first light (201) may be fixed to the first plate (110). The first light (201) may irradiate the first light (L1) through the light-emitting member. The first light (201) may irradiate the first light (L1) toward the normal direction of the body portion (50).

[0287] For example, the first light (201) may be coupled to the middle height of the first plate (110).

[0288] The second light (202) may be fixed to the second plate (120). The second light (202) may include a second upper light (202a) fixed to the upper portion of the second plate (120) and a second lower light (202b) fixed to the lower portion of the second plate (120). The second light (202) may irradiate the second light (L2) in a direction inclined at a certain angle in the positive direction with the first light (L1) as an imaginary axis.

[0289] The second upper light (202a) can irradiate the second upper light (L2a) through the light-emitting member, and the second lower light (202b) can irradiate the second lower light (L2b) through the light-emitting member. The second upper light (202a) and the second lower light (202b) can irradiate the second upper light (L2a) and the second lower light (L2b) in different directions, respectively.

[0290] For example, the second upper light (202a) may be positioned at a higher position than the height at which the first light (201) is combined, and the second lower light (202b) may be positioned at a lower position than the height at which the first light (201) is combined.

[0291] The third light (203) may be fixed to the third plate (130). The third light (203) may include a third upper light (203a) fixed to the upper portion of the third plate (130) and a third lower light (203b) fixed to the lower portion of the third plate (130). The third light (203) may irradiate the third light (L3) in a direction tilted at a certain angle in the negative direction with the first light (L1) as an imaginary axis.

[0292] The third upper light (203a) can irradiate the third upper light (L3a) through the light-emitting member, and the third lower light (203b) can irradiate the third lower light (L3b) through the light-emitting member. The third upper light (203a) and the third lower light (203b) can irradiate the third upper light (L3a) and the third lower light (L3b) in different directions, respectively.

[0293] For example, the third upper light (203a) may be positioned at a higher position than the height at which the first light (201) is combined, and the third lower light (203b) may be positioned at a lower position than the height at which the first light (201) is combined.

[0294] The fourth light (204) may be fixed to the fourth plate (140). The fourth light (204) may include a fourth upper light (204a) fixed to the upper portion of the fourth plate (140) and a fourth lower light (204b) fixed to the lower portion of the fourth plate (140). The fourth light (204) may irradiate the fourth light (L4) in a direction inclined at a certain angle in the positive direction with the first light (L1) as an imaginary axis.

[0295] The fourth upper light (204a) can irradiate the fourth upper light (L4a) through the light-emitting member, and the fourth lower light (204b) can irradiate the fourth lower light (L4b) through the light-emitting member. The fourth upper light (204a) and the fourth lower light (204b) can irradiate the fourth upper light (L4a) and the fourth lower light (L4b) in different directions, respectively.

[0296] For example, the fourth upper light (204a) may be positioned at a higher position than the height at which the first light (201) is combined, and the fourth lower light (204b) may be positioned at a lower position than the height at which the first light (201) is combined.

[0297] The fifth light (205) may be fixed to the fifth plate (150). The fourth light (205) may include a fifth upper light (205a) fixed to the upper portion of the fifth plate (150) and a fifth lower light (205b) fixed to the lower portion of the fifth plate (150). The fifth light (205) may irradiate the fifth light (L5) in a direction tilted at a certain angle in the negative direction with the first light (L1) as an imaginary axis.

[0298] The fifth upper light (205a) can irradiate the fifth upper light (L5a) through the light-emitting member, and the fifth lower light (205b) can irradiate the fifth lower light (L5b) through the light-emitting member. The fifth upper light (205a) and the fifth lower light (205b) can irradiate the fifth upper light (L5a) and the fifth lower light (L5b) in different directions, respectively.

[0299] For example, the fifth upper light (205a) may be positioned at a higher position than the height at which the first light (201) is combined, and the fifth lower light (205b) may be positioned at a lower position than the height at which the first light (201) is combined.

[0300] According to one embodiment, the first to fifth lights (201, 202, 203, 204, 205) can irradiate the first light (L1), the second light (L2), the third light (L3), the fourth light (L4), and the fifth light (L5) in directions inclined at 0°, ±10°, ±20°, ±30°, and ±40° with the first light (L1) irradiated in the normal direction as an imaginary axis.

[0301] More specifically, the first light (201) can irradiate the first light (L1) toward the normal direction of the body part (50). That is, the first light (201) can irradiate the first light (L1) in the 0° direction with the irradiation path of the first light (L1) as an imaginary axis.

[0302] The second light (202) can irradiate the second light (L2) in a direction inclined at 10° and 20° in the positive direction with the first light (L1) as an imaginary axis. Accordingly, one of the second upper light (202a) and the second lower light (202b) can irradiate the light in a direction inclined at 10°, and the other of the second upper light (202a) and the second lower light (202b) can irradiate the light in a direction inclined at 20°.

[0303] The third light (203) can irradiate the third light (L3) in a direction inclined at 10° and 20° in the negative direction with the first light (L1) as an imaginary axis. Accordingly, one of the third upper light (203a) and the third lower light (203b) can irradiate light in a direction inclined at -10°, and the other of the third upper light (203a) and the third lower light (203b) can irradiate light in a direction inclined at -20°.

[0304] The fourth light (204) can irradiate the fourth light (L4) in a direction inclined at 30° and 40° in the positive direction with the first light (L1) as an imaginary axis. Accordingly, one of the fourth upper light (204a) and the fourth lower light (204b) can irradiate light in a direction inclined at 30°, and the other of the fourth upper light (204a) and the fourth lower light (204b) can irradiate light in a direction inclined at 40°.

[0305] The fifth light (205) can irradiate the fifth light (L5) in a direction inclined at 30° and 40° in the negative direction with the first light (L1) as an imaginary axis. Accordingly, one of the fifth upper light (205a) and the fifth lower light (205b) can irradiate light in a direction inclined at -30°, and the other of the fifth upper light (205a) and the fifth lower light (205b) can irradiate light in a direction inclined at -40°.

[0306] In other words, the second light (202) and the third light (203) can each emit light in directions symmetrical to each other with respect to the first light (L1). In addition, the fourth light (204) and the fifth light (205) can each emit light in directions symmetrical to each other with respect to the first light (L1).

[0307] As a result, the lighting unit (200) can include nine independent lights, and the first light (201), the second upper light (202a), the second lower light (202b), the third upper light (203a), the third lower light (203b), the fourth upper light (204a), the fourth lower light (204b), the fifth upper light (205a), and the fifth lower light (205b) are arranged to emit light in different directions, so that the light emission efficiency of the lighting unit (1) is improved, and visibility can be greatly improved even at night.

[0308] As described above, the plurality of lighting units (1) can surround the entire outer surface of the body portion (50). As illustrated in FIG. 39, when four lighting units (1) are connected to each other, the entire outer surface of the body portion (50) can be surrounded. The four lighting units (1) include lights of 36 independent lighting units (200), and the 36 lights are installed at 10-degree intervals so as to emit light in different directions on the outer surface of the body portion (50) within a 360-degree range based on the imaginary central axis of the body portion (50). Accordingly, the light emission efficiency of the lighting units (1) is improved, and visibility can be greatly improved even at night.

[0309] Fig. 43 is a plan view for explaining a support part of an aviation obstacle indicator light according to the 18th modified example of the present application.

[0310] Referring to FIG. 43, the aviation obstacle warning light according to the 18th modified example of the present application may include a body part (50) and a lighting unit (1).

[0311] Since the above body part (50) is substantially the same as the body part (50) according to the 17th modified example of the present application, a detailed description is omitted.

[0312] The above lighting unit (1) can be coupled to the outer surface of the body portion (50). The lighting unit (1) can include a support portion (100) and a lighting portion (200) that are coupled to form an integral body.

[0313] The above support member (100) can be attached to the outer surface of the body member (50) and support the lighting member (200). The support member (100) can be formed in a cylindrical shape to surround the entire outer surface of the body member (50).

[0314] The above lighting unit (200) can be coupled to the body unit (50) via the support unit (100). The lighting unit (200) includes 36 independent light-emitting members and can emit light radially from the body unit (50).

[0315] As a result, the 36 light-emitting elements are installed at 10-degree intervals, and can emit light in different directions on the outer surface of the body portion (50) within a 360-degree range based on the imaginary central axis of the body portion (50). Accordingly, the light-emitting efficiency of the lighting unit (1) is improved, and visibility can be greatly improved even at night.

[0316] FIG. 44 and FIG. 45 are drawings for explaining how the angle of the lighting unit is adjusted according to the 19th modified example of the present application.

[0317] Referring to FIGS. 44 and 45, the aviation obstacle warning light according to the 19th modified example of the present application may include a body part (50) and a lighting unit (1).

[0318] Since the above body part (50) is substantially the same as the body part (50) according to the 17th modified example of the present application, a detailed description is omitted.

[0319] The above lighting unit (1) may be coupled to the outer circumference of the body portion (50). The lighting unit (1) may surround at least a portion of the outer circumference of the body portion (50). One lighting unit (1) may be formed in a fan shape to surround 1 / 4 of the outer circumference of the body portion (50). A plurality of lighting units (1) may surround the entire outer circumference of the body portion (50). The lighting unit (1) may include a support portion (100) and a lighting unit (200) that are coupled to be formed as one piece.

[0320] The above support member (100) is attached to the outer circumferential surface of the body member (50) and can support the lighting member (200). The above support member (100) can include a plurality of support plates (110) that are spaced apart from each other.

[0321] Each of the above support plates (110) may or may not be coupled to the lighting unit (200).

[0322] The above lighting unit (200) can be coupled to the body unit (50) via a plurality of the above support plates (110). The lighting unit (200) can emit light radially from the body unit (50) by including nine independent light-emitting members.

[0323] As a result, the nine light-emitting members are installed at 10-degree intervals, and can emit light in different directions on the outer surface of the body part (50) within a 90-degree range based on the imaginary central axis of the body part (50).

[0324] That is, when four of the above lighting units (1) are connected to each other, they can cover the entire outer surface of the body part (50). The four of the above lighting units (1) include the lights of 36 independent lighting units (200), and the 36 lights are installed at 10-degree intervals, so that they can emit light in different directions on the outer surface of the body part (50) within a 360-degree range based on the imaginary central axis of the body part (50).

[0325] Accordingly, the luminous efficiency of the lighting unit (1) is improved, and visibility can be greatly improved even at night.

[0326] Figure 46 is a drawing for explaining an aviation obstacle indicator light according to the 20th modified example of the present application.

[0327] Referring to Fig. 46, an aviation obstacle warning light according to the 20th modified example of the present application can be installed on an overhead line (20) between transmission towers (2). The aviation obstacle warning light can include a lighting unit (1), a solar panel (510), a battery, and a control unit.

[0328] Since the above lighting unit (1) is substantially the same as the lighting unit (1) according to the 17th modified example of the present application, a detailed description is omitted.

[0329] The solar cell panel (510) may be installed on the upper surface of the lighting unit (1). Electric energy generated from sunlight may be stored through the solar cell panel (510). The electric energy generated through the solar cell panel (510) may be used for light emission of the lighting unit (1) and operation of the control unit, but is not limited thereto.

[0330] That is, the lighting unit (1) and the solar panel (510) are installed on the processing line (20) as described above, so that the visibility of the aviation obstacle warning light can be further improved.

[0331] Although not shown, the battery and control unit may be located inside the lighting unit (1), but are not limited thereto.

[0332] Figure 47 is a drawing for explaining an aviation obstacle indicator light according to the 21st modified example of the present application.

[0333] Referring to Fig. 47, an aviation obstacle warning light according to the 21st modified example of the present application may be installed on an overhead line (20) between transmission towers (2). The aviation obstacle warning light may include a lighting unit (1), a solar panel (510), a control unit (400), a battery, and a connecting line.

[0334] Since the above lighting unit (1) is substantially the same as the lighting unit (1) according to the 17th modified example of the present application, a detailed description is omitted.

[0335] The above solar cell panel (510) may be installed inside the transmission tower (2). Electric energy generated from sunlight may be stored through the solar cell panel (510). The electric energy generated through the solar cell panel (510) may be used for the light emission of the lighting unit (1) and the operation of the control unit (400), but is not limited thereto.

[0336] The above control unit (400) may be installed inside the transmission tower (2). The above control unit (400) may include a light sensor (CdS), a global positioning system (GPS), and a maximum power point tracking (MPPT) controller.

[0337] Although not shown, the battery may be installed inside the transmission tower (2).

[0338] The above connecting line can electrically connect the lighting unit (1) and the battery (450) and / or the solar panel (510).

[0339] As a result, depending on the state of the processing line (20), the positions of the solar panel (510), the control unit (400), and the battery can be selected and installed. In other words, the arrangement of the aviation obstacle warning light can be changed according to the situation. Accordingly, the convenience of the worker installing the aviation obstacle warning light can be improved, and the visibility of the aviation obstacle warning light can be further improved.

[0340]

[0341] While the present invention has been described in detail using preferred embodiments, the scope of the present invention is not limited to the specific embodiments described above, and should be construed in accordance with the appended claims. Furthermore, those skilled in the art will appreciate that numerous modifications and variations are possible without departing from the scope of the present invention.

[0342]

[0343] The high-efficiency aviation obstacle warning light, which is easy to install and install stably, easy to maintain, has an adjustable focal length, and operates efficiently by irradiating 360 degrees in all directions according to the technical idea of ​​the present application, can be used in the aviation obstacle lighting industry, energy harvester field, etc.

Claims

1. A body part including a columnar shape with an empty interior; and Including a lighting unit arranged radially on the outer surface of the above body part, The above lighting unit, A cylindrical housing with an interior that is hollow and open at both ends; A lens coupled to one end of the above housing; an inner member inserted into the empty interior of the housing; and An aviation obstacle warning light fixed on the inner member and including a light-emitting member that lights up toward the lens.

2. In paragraph 1, Further comprising a power supply electrically connected to the light-emitting member of the lighting unit, The above power supply unit, An aviation obstacle warning light, which is disposed on the upper surface of the body and includes a solar panel that generates and stores electric energy from sunlight.

3. In paragraph 2, The above power supply unit, An aviation obstacle warning light further comprising an energy conversion unit disposed adjacent to a power transmission line and disposed on a lower surface of the body portion, the energy conversion unit converting electromagnetic waves generated from the power transmission line into electrical energy.

4. In paragraph 1, Further comprising a power supply electrically connected to the above lighting unit, The above power supply unit, An aviation obstacle warning light, which is arranged adjacent to a power transmission line and is arranged on the lower surface of the body, and includes an energy conversion unit that converts electromagnetic waves generated from the power transmission line into electrical energy.

5. In paragraph 1, Further comprising a lighting control unit connecting the above body unit and the above lighting unit, The above lighting control unit, A first fixture having one end fixed to the body and including a receiving space at the other end; and One end is fixed to the above lighting unit, and the other end includes a second fixture that rotates inside the receiving space of the first fixture. An aviation obstacle warning light including an angle of the lighting unit being adjusted from the body unit.

6. In paragraph 1, A pair of fixed connectors spaced apart from each other, wrapping at least a portion of the processing line; A pair of support rods each extending downward from a pair of the above fixed connectors; A plate connecting a pair of the above support rods; a ground connector positioned between a pair of said fixed connectors and surrounding at least a portion of said processed ground wire; and It further includes a ground wire that is connected to the above-mentioned ground line through the above-mentioned ground connector and extends downward from the above-mentioned ground connector, The above body part is placed on the plate, An aviation obstacle warning light, wherein the light-emitting member of the lighting unit is electrically connected to the ground wire.

7. A body part including a columnar shape with an empty interior; A support part attached to the outer surface of the above body part; and A lighting unit comprising a lighting unit coupled to the above support unit, The above support part, It includes a plurality of support plates extending in the longitudinal direction of the body portion and spaced apart from each other, The above lighting unit, An aviation obstacle warning light that is coupled to a plurality of the above support plates and includes a light source that radiates from the center of the body portion.

8. In paragraph 5, A plurality of the above lighting units are fixed, and further include a plate attached to the outer surface of the body unit, The above lighting units are: An aviation obstacle warning light including one formed integrally through the above plate.

9. In paragraph 8, The above lighting units are: A first lighting unit fixed at a first height on the outer surface of the above body portion; A second lighting unit fixed at a second height on the outer surface of the body portion; and Including a third lighting unit fixed at a third height on the outer surface of the above body portion, The direction of the first lighting unit fixed at the first height is arranged differently from the direction of the second lighting unit fixed at the second height, The direction of the second lighting unit fixed at the second height is arranged differently from the direction of the third lighting unit fixed at the third height, The direction of the third lighting unit fixed at the third height is arranged differently from the direction of the first lighting unit fixed at the first height. An aviation obstacle warning light including a plurality of said lighting units each emitting light in different directions from the center of said body portion.

10. In paragraph 9, The above plate, An aviation obstacle warning light that surrounds at least a portion of the outer surface of the body portion, or encompasses the entire outer surface of the body portion.

11. In paragraph 1, A battery and solar panel electrically connected to the light-emitting member of the lighting unit; Further comprising a controller that selectively supplies power from the battery or the solar panel to the light-emitting member of the lighting unit, The above lighting unit is installed on the processing line, The above battery, the solar panel, and the controller are installed on a transmission tower, The above battery and the above solar panel, An aviation obstacle warning light comprising power being supplied to the light-emitting member through a connecting line attached along the above-mentioned processing line.

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