Aviation obstruction beacon

Abstract

The utility model provides an aviation obstruction beacon, which relates to the field of lamps and comprises a lamp shell, a first reflecting cover, a second reflecting cover, a first lamp strip, a second lamp strip and the like. In conclusion, the size of the single aviation obstruction beacon is relatively small, and production, installation or transportation and the like are relatively convenient. When the aviation obstruction beacon is used, if light needs to be emitted to the periphery, a plurality of aviation obstruction beacons can be combined for use, and therefore application requirements are met.

Description

TECHNICAL FIELD

[0001] The utility model relates to the field of lamps and lanterns, specifically, an aviation obstruction light. BACKGROUND

[0002] The aviation obstruction light is used to show the outline of the structure, so that the operator of the aircraft can accurately determine the height and outline of the obstruction, and play a warning role. According to the height of light intensity, the aviation obstruction light is divided into three categories of high light intensity, medium light intensity and low light intensity, and the types, height and position of the corresponding building of different obstruction lights are different.

[0003] The existing aviation obstruction light needs to install multiple reflector hoods and corresponding lamp strips to realize the light emission around, and the multiple reflector hoods constitute 360-degree light emission light. Since multiple reflector hoods and corresponding lamp strips are installed around the aviation obstruction light, the volume of a single aviation obstruction light is too large. UTILITY MODEL CONTENT

[0004] The utility model aims at solving the problem in the background art, and further provides an aviation obstruction light.

[0005] The utility model solves the technical problems by adopting the technical scheme:

[0006] An aviation obstruction light comprises:

[0007] A lamp shell;

[0008] A first reflector hood;

[0009] A second reflector hood, the first reflector hood and the second reflector hood are arranged in the lamp shell;

[0010] A first lamp strip, the first lamp strip is arranged at the front end of the first reflector hood, the first reflector hood is used for reflecting the light emitted by the first lamp strip into a first reflected light beam, and the first reflected light beam is emitted out of the lamp shell;

[0011] A second lamp strip, the second lamp strip is arranged at the front end of the second reflector hood, the second reflector hood is used for reflecting the light emitted by the second lamp strip into a second reflected light beam, and the second reflected light beam is emitted out of the lamp shell.

[0012] Further, the first reflected light beam and the second reflected light beam are parallel light beams.

[0013] Further, the utility model further comprises:

[0014] A first heat dissipation block, the first lamp strip is arranged on the first heat dissipation block;

[0015] A second heat dissipation block, the second lamp strip is arranged on the second heat dissipation block.

[0016] Further, the first reflector, the second reflector, the first lamp strip, the second lamp strip, the first heat dissipation block and the second heat dissipation block are respectively provided with a plurality of, the plurality of first reflectors, the first lamp strips and the first heat dissipation blocks are sequentially arranged from top to bottom respectively; the plurality of second reflectors, the second lamp strips and the second heat dissipation blocks are sequentially arranged from top to bottom respectively.

[0017] Further, the first installation plate, the second installation plate and the mounting support are further provided with a plurality of.

[0018] The first installation plate, the second installation plate and the mounting support are further provided with a plurality of.

[0019] The second installation plate, the second reflector, the second lamp strip and the second heat dissipation block are sequentially arranged from top to bottom respectively.

[0020] Further, the first installation plate, the second installation plate and the mounting support are further provided with a plurality of.

[0021] The first installation plate, the second installation plate and the mounting support are further provided with a plurality of.

[0022] Further, the lamp shell comprises:

[0023] The lamp shell comprises:

[0024] The lamp shell comprises:

[0025] Further, the first installation plate, the second installation plate and the mounting support are further provided with a plurality of.

[0026] The first installation plate, the second installation plate and the mounting support are further provided with a plurality of.

[0027] Further, the first installation plate, the second installation plate and the mounting support are further provided with a plurality of.

[0028] The circuit board is arranged in the lamp shell, and the circuit board is electrically connected with the first lamp strip and the second lamp strip respectively.

[0029] Further, the first installation plate, the second installation plate and the mounting support are further provided with a plurality of.

[0030] The power supply board is arranged in the lamp shell, and the power supply board is electrically connected with the circuit board.

[0031] Compared with the prior art, the beneficial effects of the utility model are:

[0032] Compared with the prior art, the volume of the single aeronautical obstacle light in the application is relatively small, and production, installation or transportation is relatively convenient. In use, if it is necessary to emit light to the surrounding, a plurality of aeronautical obstacle lights can be combined for use, so as to meet the application requirements. Specifically, when the first reflected light beam and the second reflected light beam are 180 degrees apart, two aeronautical obstacle lights can be combined into a group; when the first reflected light beam and the second reflected light beam are 120 degrees apart, three aeronautical obstacle lights can be combined into a group; and when the first reflected light beam and the second reflected light beam are 90 degrees apart, four aeronautical obstacle lights can be combined into a group. In this way, the application requirements of 360-degree light emission can be met. BRIEF DESCRIPTION OF DRAWINGS

[0033] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0034] Figure 2 It is a schematic diagram of the lamp shell;

[0035] Figure 3 It is a schematic diagram of the exploded structure of the aeronautical obstacle light;

[0036] Figure 4 It is an exploded schematic diagram of the aeronautical obstacle light;

[0037] Reference signs:

[0038] 10, lampshade; 101, lamp shell; 102, cover body; 20, mounting base; 30, mounting bracket; 301, main mounting plate; 302, lower end mounting plate; 303, upper end mounting plate; 40, first reflector; 50, second reflector; 60, first light bar; 70, second light bar; 80, first heat dissipation block; 90, second heat dissipation block; 11, first mounting plate; 12, second mounting plate; 13, threaded connecting rod; 14, circuit board; 15, power board; 16, inner shell cover. DETAILED DESCRIPTION

[0039] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of protection of the utility model. The utility model will be further described in combination with the drawings and embodiments:

[0040] As Figures 1 to 4As shown in the figure, an aviation obstruction light, a lamp shell 101, a first reflector 40, a second reflector 50, a first light bar 60 and a second light bar 70, the first reflector 40 and the second reflector 50 are installed in the lamp shell 101 at a set angle; the first light bar 60 is installed at the front end of the first reflector 40, the first reflector 40 is used to reflect the light emitted by the first light bar 60 into a first reflected light beam, and the light is emitted outward through the lamp shell 101; the second light bar 70 is installed at the front end of the second reflector 50, the second reflector 50 is used to reflect the light emitted by the second light bar 70 into a second reflected light beam, and the light is emitted outward through the lamp shell 101.

[0041] Specifically, as shown in the figure, Figure 2 The first reflector 40 and the second reflector 50 can be arranged at a set angle. For example, the angle can be 180 degrees, 120 degrees or 90 degrees. The first light bar 60 is arranged directly in front of the first reflector 40; in this way, the light emitted by the first light bar 60 can be reflected by the first reflector 40 and then emitted outward through the lamp shell 101. Similarly, the second light bar 70 is arranged directly in front of the second reflector 50; in this way, the light emitted by the second light bar 70 can be reflected by the second reflector 50 and then emitted outward through the lamp shell 101. The first reflected light beam and the second reflected light beam are parallel light beams; in this way, the angle between the first reflected light beam and the second reflected light beam is the same as the set angle between the first reflector 40 and the second reflector 50 (i.e. the angle can be 180 degrees, 120 degrees or 90 degrees).

[0042] Since a single lamp does not need to be provided with reflectors and light bars around it, the volume of a single aviation obstruction light is relatively small, and production, installation or transportation is relatively convenient. In use, if light needs to be emitted in all directions, multiple aviation obstruction lights can be combined. For example, when the angle between the first reflected light beam and the second reflected light beam is 180 degrees, two aviation obstruction lights can be combined into a group; when the angle between the first reflected light beam and the second reflected light beam is 120 degrees, three aviation obstruction lights can be combined into a group; when the angle between the first reflected light beam and the second reflected light beam is 90 degrees, four aviation obstruction lights can be combined into a group. In this way, the application requirement of 360-degree light emission can be met.

[0043] As shown in the figure, Figure 4 The first light bar 60 and the second light bar 70 can be respectively provided with a plurality of lamp beads (the lamp beads are not labeled in the figure), and the plurality of lamp beads are arranged in a straight line. The first reflector 40 and the second reflector 50 are respectively provided with a reflecting inclined surface at the opposite side and the two sides of the first light bar 60 and the second light bar 70.

[0044] Therefore, when the light emitted by the lamp beads on the first light bar 60 and the second light bar 70 is reflected to the opposite inclined reflective surfaces, the light is then reflected to the two sides and then emitted outward. In this way, the light reflected from the opposite light bar is not blocked by the light bar, thereby improving the utilization rate of the light. Specifically, the lamp beads can be LED lamp beads.

[0045] Referring to Figures 2 to 4 , the aviation obstruction light further comprises a first heat dissipation block 80 and a second heat dissipation block 90. The first light bar 60 is mounted on the first heat dissipation block 80 to dissipate heat through the first heat dissipation block 80. The second light bar 70 is mounted on the first heat dissipation block 80 to dissipate heat through the second heat dissipation block 90. The back surface of the first heat dissipation block 80 and the second heat dissipation block 90 can be provided with a plurality of heat dissipation fins (not labeled in the figure). The plurality of heat dissipation fins can greatly increase the heat dissipation area. Specifically, the first heat dissipation block 80 and the second heat dissipation block 90 are made of metal. The first light bar 60 is mounted on the front surface of the first heat dissipation block 80. The second light bar 70 is mounted on the front surface of the second heat dissipation block 90. In this way, the heat generated by the first light bar 60 can be conducted out through the first heat dissipation block 80 and rapidly dissipated through the heat dissipation fins. The heat generated by the second light bar 70 can be conducted out through the second heat dissipation block 90 and rapidly dissipated through the heat dissipation fins.

[0046] Referring to Figures 2 to 4 , a plurality of first light covers 40, first light bars 60, and first heat dissipation blocks 80 are sequentially arranged from top to bottom. A plurality of second light covers 50, second light bars 70, and second heat dissipation blocks 90 are sequentially arranged from top to bottom. The plurality of first light bars 60 and the second light bars 70 can increase the light emitted, thereby meeting the light emission requirements of the obstruction light. In addition, the first light cover 40 and the second light cover 50 have a relatively small manufacturing volume. Therefore, the overall volume of the aviation obstruction light is reduced. Since the first light cover 40 and the second light cover 50 have a relatively small manufacturing volume, the volume of the individual light cover can be reduced, thereby reducing the cost of the light cover.

[0047] Referring to Figure 2 and Figure 4 , the aviation obstruction light further comprises a first mounting plate 11 and a second mounting plate 12. A plurality of first light covers 40 are mounted on the first mounting plate 11. A plurality of second light covers 50 are mounted on the second mounting plate 12.

[0048] As Figure 4As shown in the middle, the included angle between the first mounting plate 11 and the second mounting plate 12 is also set to an angle, as above. In this way, after the first reflector 40 and the second reflector 50 are installed, a set angle can be formed. Further, the sequential installation of multiple reflectors can be facilitated.

[0049] Referring to Figure 4 , the aviation obstruction light further comprises: a mounting bracket 30, the first mounting plate 11 and the second mounting plate 12 are fixedly connected with the mounting bracket 30, so as to be installed and arranged in the lamp shell 101 through the mounting bracket 30. The first mounting plate 11 and the second mounting plate 12 can be installed and fixed at a set angle through the mounting bracket 30.

[0050] Referring to Figure 3 and Figure 4 , the lamp shell 101 comprises: a lampshade 10 and a mounting base 20, the lampshade 10 is a cylindrical lampshade 10; the bottom of the lampshade 10 is connected with the mounting base 20;

[0051] Further optimization of the above embodiment scheme, the lamp shell 101 is threadedly connected with a cover 102 to facilitate opening the lamp shell 101 from above; in addition, the aviation obstruction light can further comprise an inner cover 16 for accommodating the remaining parts except the lamp shell 101 and the mounting base 20, the inner cover 16 can shield the internal structure of the lamp, making the whole lamp more beautiful, and avoiding directly peeping at the circuit board mounting structure inside the lamp through the lamp shell 101.

[0052] As Figure 4 shown in the middle, the aviation obstruction light further comprises a threaded connecting rod 13, the mounting bracket 30 comprises a main mounting plate 301, an upper end mounting plate 303 and a lower end mounting plate 302, the upper end mounting plate 303 and the lower end mounting plate 302 are respectively provided with through holes, one end of the threaded connecting rod 13 is threadedly fixedly connected with the lampshade 10 through the through hole of the upper end mounting plate 303, and the other end of the threaded connecting rod 13 is fixedly connected with the mounting base 20 through the lower end mounting plate 302. That is, the lampshade 10, the mounting base 20 and the mounting bracket 30 can be connected in series into a whole structure through the threaded connecting rod 13. At the same time, the installation of the lampshade 10 is more convenient.

[0053] Referring to Figure 4 , the aviation obstruction light further comprises: a circuit board 14, the circuit board 14 is installed and arranged in the lamp shell 101, and the circuit board 14 is electrically connected with the first lamp strip 60 and the second lamp strip 70 respectively, so as to drive and control the first lamp strip 60 and the second lamp strip 70 to emit light. The circuit board 14 can be fixedly connected with the mounting bracket 30, so as to be installed and arranged in the lamp shell 101. Through the circuit board 14, a driving signal can be output to the lamp beads, so that the lamp beads on the first lamp strip 60 and the second lamp strip 70 can be driven to emit light, and further, the lighting and extinguishing control process of the first lamp strip 60 and the second lamp strip 70 can be realized.

[0054] Referring to Figure 4 The aviation obstruction light further comprises a power board 15, which is arranged in the lamp shell 101 and is electrically connected with the circuit board 14, and is used for converting input power into power supply of the circuit board 14 to supply power for the circuit board 14. The power board 15 can be fixedly connected with the mounting bracket 30, so as to be arranged in the lamp shell 101, and the input power can be connected through the power board 15, and the input power is converted in voltage to supply low-voltage direct-current power for the circuit board 14. For example, the input commercial alternating current can be converted into low-voltage direct-current power to supply low-voltage direct-current power for the circuit board 14.

[0055] The basic principle, main features and advantages of the present application are shown and described above. It should be understood by those skilled in the art that the present application is not limited by the above embodiments, and the above embodiments and descriptions in the specification are only to illustrate the principle of the present application. Without departing from the spirit and scope of the present application, various changes and improvements can be made to the present application, and these changes and improvements all fall within the scope of the present application. The scope of protection of the present application is defined by the appended claims and their equivalents.

Claims

1. An aeronautical obstacle light, characterized in that, It comprises: a lamp shell (101); a first light cover (40); a second light cover (50), the first light cover (40) and the second light cover (50) are arranged in the lamp shell (101); a first light bar (60), the first light bar (60) is arranged at the front end of the first light cover (40), the first light cover (40) is used for reflecting the light emitted by the first light bar (60) into a first reflected light beam and emitting the first reflected light beam out of the lamp shell (101); a second light bar (70), the second light bar (70) is arranged at the front end of the second light cover (50), the second light cover (50) is used for reflecting the light emitted by the second light bar (70) into a second reflected light beam and emitting the second reflected light beam out of the lamp shell (101).

2. An aeronautical obstruction light according to claim 1, wherein The first reflected light beam and the second reflected light beam are parallel light beams respectively.

3. An aeronautical obstruction light according to claim 1, wherein It further comprises: a first heat sink (80), the first light bar (60) is arranged on the first heat sink (80); a second heat sink (90), the second light bar (70) is arranged on the second heat sink (90).

4. An aeronautical obstruction light according to claim 3, wherein The first light cover (40), the second light cover (50), the first light bar (60), the second light bar (70), the first heat sink (80) and the second heat sink (90) are respectively provided with a plurality of the first light cover (40), the first light bar (60) and the first heat sink (80) are sequentially arranged from top to bottom; a plurality of the second light cover (50), the second light bar (70) and the second heat sink (90) are sequentially arranged from top to bottom.

5. The aviation obstruction light of claim 1, wherein It further comprises: a first mounting plate (11), a plurality of the first light cover (40) is arranged on the first mounting plate (11) respectively; a second mounting plate (12), a plurality of the second light cover (50) is arranged on the second mounting plate (12) respectively.

6. An aeronautical obstruction light according to claim 5, wherein It further comprises: a mounting bracket (30), the first mounting plate (11) and the second mounting plate (12) are fixedly connected with the mounting bracket (30).

7. An aeronautical obstruction light according to claim 1, wherein The lamp shell (101) comprises: a lamp cover (10), the main body shape of the lamp cover (10) is cylindrical; a mounting base (20), the bottom of the lamp cover (10) is connected with the mounting base (20).

8. An aeronautical obstruction light according to claim 7, wherein, It further comprises: a threaded connecting rod (13), the mounting bracket (30) comprises a main mounting plate (301), an upper end mounting plate (303) and a lower end mounting plate (302), the upper end mounting plate (303) and the lower end mounting plate (302) are respectively provided with through holes, one end of the threaded connecting rod (13) passes through the through hole of the upper end mounting plate (303) and is fixedly connected with the lamp cover (10) in a threaded manner, the other end of the threaded connecting rod (13) passes through the lower end mounting plate (302) and is fixedly connected with the mounting base (20).

9. An aeronautical obstruction light according to claim 1, wherein, It further comprises: a circuit board (14), the circuit board (14) is arranged in the lamp shell (101), and the circuit board (14) is electrically connected with the first light bar (60) and the second light bar (70) respectively.

10. An aeronautical obstruction light according to claim 9, wherein It further comprises: a power board (15), the power board (15) is arranged in the lamp shell (101), and the power board (15) is electrically connected with the circuit board (14).

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