A hoop type aviation obstruction light

Abstract

This utility model relates to the field of aviation obstruction light technology and provides a clamp-type aviation obstruction light, comprising: a support plate, a base fixedly connected to the middle of the upper end of the support plate, and a transparent protective cover disposed on the base; an installation assembly disposed between the base and the transparent protective cover; and a cleaning assembly disposed on the support plate; the cleaning assembly includes a motor fixedly connected to one side of the upper end of the support plate, and a first gear plate fixedly connected to the output end of the motor. The cleaning assembly facilitates cleaning of the transparent protective cover. When the motor is started, it drives the first gear plate to rotate. The first gear plate meshes with a circular gear ring, and the rotation of the circular gear ring drives a cleaning sponge brush to clean the exterior of the transparent protective cover, preventing rainwater stains from affecting the use of the aviation obstruction light. Heat dissipation holes facilitate heat dissipation of the aviation obstruction light, and a filler is provided to absorb moisture, preventing moisture from entering the interior.

Description

Technical Field

[0001] This utility model belongs to the field of aviation obstruction light technology, and in particular relates to a clamp-type aviation obstruction light. Background Technology

[0002] Aviation obstruction lights, also known as navigational lighting equipment, are special lighting fixtures used to mark obstacles. They belong to the navigational lighting equipment industry. The function of aviation obstruction lights is to display the outline of structures, enabling aircraft operators to judge the height and outline of obstacles and serve as a warning. To distinguish them from general-purpose lighting, aviation obstruction lights are not always on, but flashing. Low-intensity aviation obstruction lights are always on, while medium-intensity and high-intensity aviation obstruction lights flash.

[0003] Application CN201822023235.9 discloses a clamp-type aviation obstruction light bracket, including a light body and a light holder located at the lower end of the light body. The light holder has pre-drilled bolt holes. The lower end of the light holder is fixed to a main shaft, and the other end of the main shaft is fixed to a clamp. The clamp is fixed to a column by bolts. This design allows the aviation light to be designed and arranged without being restricted by buildings, facilitating the initial installation and construction of the aviation light, and benefiting the subsequent maintenance and repair of the aviation light equipment. It also increases the visibility of the aviation light's illumination area, achieving environmental protection and energy saving goals. Simultaneously, it reduces the number of aviation lights required, saving on apron construction costs and accelerating the construction and installation progress.

[0004] The existing technology still has the following shortcomings:

[0005] Existing obstruction lights cannot automatically clean their surfaces, causing snowflakes to accumulate on their surfaces during heavy snowfall, affecting their performance. Additionally, aviation obstruction lights require ventilation and heat dissipation during use, and the moisture in the air can easily cause the interior of the light body to become damp, which can also negatively impact its effectiveness. Utility Model Content

[0006] This utility model provides a clamp-type aviation obstruction light, which aims to solve the problems of existing obstruction lights not being able to automatically clean their surfaces, causing snowflakes to accumulate on the surface of the obstruction light in heavy snow, affecting the obstruction light. At the same time, aviation obstruction lights need ventilation and heat dissipation during use, but the moisture in the air can easily make the inside of the aviation obstruction light body damp, which to some extent affects the performance of the light.

[0007] This utility model is implemented as follows: a clamp-type aviation obstruction light includes: a support plate, a base fixedly connected to the middle of the upper end of the support plate, a transparent protective cover provided on the base; an installation assembly provided between the base and the transparent protective cover; a cleaning assembly provided on the support plate; the cleaning assembly includes a motor fixedly connected to one side of the upper end of the support plate, and a first gear plate fixedly connected to the output end of the motor.

[0008] Preferably, the cleaning assembly further includes a toothed ring sleeved on the outside of the base; a sliding ring is fixedly connected to the toothed ring near the inner wall of the base, and an annular groove is formed on the side of the base near the outer wall of the sliding ring; the sliding ring and the annular groove are slidably connected, and the first toothed disc and the toothed ring are meshed.

[0009] Preferably, the cleaning assembly further includes an L-shaped fixing rod fixedly connected to the upper end of the toothed ring, a connecting seat rotatably connected to the top of the transparent protective cover, a connecting plate detachably fixedly connected to the upper end of the connecting seat, the other side of the L-shaped fixing rod being fixedly connected to the connecting plate, and a cleaning sponge brush detachably fixedly connected to the side of the L-shaped fixing rod near the transparent protective cover, the cleaning sponge brush being in contact with the surface of the transparent protective cover.

[0010] Preferably, the upper end of the base has an installation groove, the main body of the aviation obstruction light is installed inside the installation groove, the upper end of the main body of the aviation obstruction light is located inside the transparent protective cover, the base has heat dissipation holes on both sides, the two heat dissipation holes are respectively filled with filler, the two heat dissipation holes are connected to the inside of the installation groove, and the two heat dissipation holes can be detachably and fixedly connected with filters.

[0011] Preferably, the mounting assembly includes a sealing rubber ring fixedly connected to the lower end of the inner wall of the transparent protective cover, and the sealing rubber ring is in contact with the main body of the aviation obstruction light.

[0012] Preferably, the mounting assembly further includes a U-shaped groove formed at the top of the four sides of the base, a magnetic U-shaped block fixedly connected to the bottom of the four sides of the transparent protective cover, a sealing ring sleeved on the upper end of the magnetic U-shaped block, a magnetic plate fixedly connected inside the U-shaped groove, the magnetic U-shaped block and the U-shaped groove being inserted into each other, and the magnetic U-shaped block and the magnetic plate being attracted to each other.

[0013] Preferably, the mounting assembly further includes connecting slots formed on both sides of the base and the magnetic loop block. Each pair of connecting slots adjacent to one side are interconnected. Positioning slots are formed on both sides of the interior of the base. Two positioning slots are connected to both sides of the loop block. All four connecting slots are connected to the loop block. Pull rods are provided on both sides of the exterior of the base. Positioning rods are fixedly connected to the sides of two pull rods adjacent to each other. The two positioning rods are inserted through the four connecting slots and the two positioning slots. Springs are sleeved on both positioning rods. One side of each spring is fixedly connected to the base, and the other side of each spring is fixedly connected to the two pull rods.

[0014] Preferably, a support rod is fixedly connected to the bottom of the support plate, and a fixing component is provided at the extended end of the support rod. The fixing component includes a C-shaped frame fixedly connected to the support rod. A screw is provided at the middle of each side of the C-shaped frame. The two screws are threadedly connected to the C-shaped frame. The extended ends of the two screws pass through the two sides of the C-shaped frame and are connected to arc-shaped clamping seats through bearings. Guide rods are fixedly connected to the upper and lower ends of the two arc-shaped clamping seats on opposite sides. Limiting nuts are threadedly connected to the extended ends of the four guide rods through the two sides of the C-shaped frame.

[0015] Compared with the prior art, the embodiments of this application have the following main advantages:

[0016] The transparent protective cover is easy to clean by setting up a cleaning component. When the motor is started, it drives the first gear plate to rotate. The first gear plate and the circular gear ring are meshed and connected. The rotation of the circular gear ring drives the cleaning sponge brush to clean the outside of the transparent protective cover, preventing rainwater stains from affecting the use of the aviation obstruction light. The heat dissipation holes facilitate the heat dissipation of the aviation obstruction light. The filler is set to absorb moisture and prevent moisture from entering the interior. Attached Figure Description

[0017] Figure 1 This is a front view structural diagram of the present invention;

[0018] Figure 2 This is a front view cross-sectional structural diagram of the present invention;

[0019] Figure 3 This is a utility model Figure 2 Enlarged structural diagram at point A in the middle;

[0020] Figure 4 This is a utility model Figure 2 Enlarged structural diagram at point B;

[0021] Figure 5This is a utility model Figure 4 Enlarged structural diagram at point C;

[0022] In the diagram: 1. Support plate; 2. Bracket rod; 3. Fixing component; 4. Base; 5. Transparent protective cover; 6. Mounting component; 7. Cleaning component; 8. Mounting groove; 9. Aviation obstruction light body; 10. Sealing rubber ring; 11. U-shaped groove; 12. Magnetic U-shaped block; 13. Sealing ring; 14. Magnetic plate; 15. Positioning groove; 16. Connecting groove; 17. Positioning rod; 18. Pull rod; 19. Spring; 20. Heat dissipation hole; 21. Filter screen; 22. Filler; 24. Motor; 25. First gear plate; 26. Gear ring; 27. Slip ring; 28. Circular sliding groove; 29. ​​L-shaped fixing rod; 30. Connecting seat; 31. Connecting plate; 32. Cleaning sponge brush; 33. C-shaped frame; 34. Screw; 35. Arc-shaped clamping seat; 36. Guide rod; 37. Limiting nut. Detailed Implementation

[0023] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs; the terminology used herein in the specification of the application is for the purpose of describing particular embodiments only and is not intended to be limiting of the application; the terms "comprising" and "having," and any variations thereof, in the specification, claims, and foregoing drawings of this application are intended to cover non-exclusive inclusion. The terms "first," "second," etc., in the specification, claims, or foregoing drawings of this application are used to distinguish different objects, not to describe a particular order.

[0024] In this document, the term "embodiment" means that a particular feature, structure, or characteristic described in connection with an embodiment may be included in at least one embodiment of this application. The appearance of this phrase in various places throughout the specification does not necessarily refer to the same embodiment, nor is it a separate or alternative embodiment mutually exclusive with other embodiments. It will be explicitly and implicitly understood by those skilled in the art that the embodiments described herein can be combined with other embodiments.

[0025] This utility model embodiment provides a clamp-type aviation obstruction light, such as Figure 1-5 As shown, it includes: a support plate 1, a base 4 fixedly connected to the middle of the upper end of the support plate 1, a transparent protective cover 5 provided on the base 4; an installation component 6 provided between the base 4 and the transparent protective cover 5, and a cleaning component 7 provided on the support plate 1; the cleaning component 7 includes a motor 24 fixedly connected to one side of the upper end of the support plate 1, and a first gear plate 25 fixedly connected to the output end of the motor 24.

[0026] It should be noted that, due to the lack of automatic surface cleaning for existing obstruction lights, snowflakes accumulate on their surface during heavy snowfall, affecting their performance. Furthermore, aviation obstruction lights require ventilation and heat dissipation during use; however, the moisture in the air during ventilation can easily cause the interior of the main body 9 of the aviation obstruction light to become damp, impacting its effectiveness. This solution addresses this by incorporating a cleaning component 7 to facilitate cleaning of the transparent protective cover 5. By starting the motor 24, the motor drives the first gear disc 25 to rotate. The first gear disc 25 and the circular gear ring 26 mesh, and the rotation of the circular gear ring 26 drives the cleaning sponge brush 32 to clean the exterior of the transparent protective cover 5, preventing rainwater stains from affecting the use of the aviation obstruction light. The presence of heat dissipation holes 20 facilitates heat dissipation, and the inclusion of a filler 22 helps absorb moisture, preventing it from entering the interior.

[0027] In a further preferred embodiment of this utility model, such as Figure 1-4 As shown, the cleaning component 7 also includes a toothed ring 26 sleeved on the outside of the base 4; a slip ring 27 is fixedly connected to the inner wall of the toothed ring 26 near the base 4, and an annular groove 28 is provided on the side of the base 4 near the outer wall of the slip ring 27; the slip ring 27 and the annular groove 28 are slidably connected, and the first toothed disc 25 and the toothed ring 26 are meshed.

[0028] In this embodiment, the first toothed disc 25 and the circular toothed ring 26 are meshed together. When the first toothed disc 25 rotates, it drives the circular toothed ring 26 to rotate. At the same time, the slip ring 27 slides inside the annular groove 28 to guide the rotation of the circular toothed ring 26. Preferably, the base 4 is cylindrical.

[0029] In a further preferred embodiment of this utility model, such as Figure 1-4 As shown, the cleaning assembly 7 also includes an L-shaped fixing rod 29 fixedly connected to the upper end of the toothed ring 26, a connecting seat 30 rotatably connected to the top of the transparent protective cover 5, a connecting plate 31 detachably fixedly connected to the upper end of the connecting seat 30, the other side of the L-shaped fixing rod 29 being fixedly connected to the connecting plate 31, and a cleaning sponge brush 32 detachably fixedly connected to the side of the L-shaped fixing rod 29 near the transparent protective cover 5, with the cleaning sponge brush 32 in contact with the surface of the transparent protective cover 5.

[0030] In this embodiment, cleaning is facilitated.

[0031] In a further preferred embodiment of this utility model, such as Figure 1-4As shown, the upper end of the base 4 is provided with a mounting groove 8, and the main body 9 of the aviation obstruction light is installed inside the mounting groove 8. The upper end of the main body 9 of the aviation obstruction light is located inside the transparent protective cover 5. The base 4 is provided with heat dissipation holes 20 on both sides. The two heat dissipation holes 20 are respectively filled with filler 22. Both heat dissipation holes 20 are connected to the inside of the mounting groove 8. Filters 21 can be detachably and fixedly connected inside both heat dissipation holes 20.

[0032] In this embodiment, for the purpose of facilitating heat dissipation, preferably, the filler 22 is a filler 22 that can absorb water vapor.

[0033] In a further preferred embodiment of this utility model, such as Figure 1-4 As shown, the mounting component 6 includes a sealing rubber ring 10 fixedly connected to the lower end of the inner wall of the transparent protective cover 5, and the sealing rubber ring 10 is in contact with the aviation obstruction light body 9.

[0034] In this embodiment, it is convenient to improve the sealing effect.

[0035] In a further preferred embodiment of this utility model, such as Figure 1-5 As shown, the mounting assembly 6 also includes a U-shaped groove 11 formed at the top of the side walls of the base 4. A magnetic U-shaped block 12 is fixedly connected to the bottom of the side walls of the transparent protective cover 5. A sealing ring 13 is fitted on the upper end of the magnetic U-shaped block 12. A magnetic plate 14 is fixedly connected inside the U-shaped groove 11. The magnetic U-shaped block 12 and the U-shaped groove 11 are inserted into each other, and the magnetic U-shaped block 12 and the magnetic plate 14 are attracted to each other.

[0036] In this embodiment, the transparent protective cover 5 is easy to install and position.

[0037] In a further preferred embodiment of this utility model, such as Figure 1-5 As shown, the mounting assembly 6 also includes connecting slots 16 on both sides of the base 4 and the magnetic loop block 12. The four connecting slots 16 are connected to each other by two slots that are close to one side. The base 4 has positioning slots 15 on both sides inside. The two positioning slots 15 are connected to the two sides of the loop block 11. All four connecting slots 16 are connected to the loop block 11. Pull rods 18 are provided on both sides of the base 4 outside. The two pull rods 18 are fixedly connected to positioning rods 17 on the side that is close to each other. The two positioning rods 17 are inserted through the four connecting slots 16 and the two positioning slots 15. Springs 19 are sleeved on the two positioning rods 17. One side of the two springs 19 is fixedly connected to the base 4, and the other side of the two springs 19 is fixedly connected to the two pull rods 18.

[0038] In this embodiment, it is easier to fix the transparent protective cover 5 more stably.

[0039] In a further preferred embodiment of this utility model, such as Figure 1-5As shown, a support rod 2 is fixedly connected to the bottom of the support plate 1. A fixing component 3 is provided at the extended end of the support rod 2. The fixing component 3 includes a C-shaped frame 33 fixedly connected to the support rod 2. A screw 34 is provided at the middle of each side of the C-shaped frame 33. The two screws 34 are threadedly connected to the C-shaped frame 33. The extended ends of the two screws 34 pass through the two sides of the C-shaped frame 33 and are connected to the arc-shaped clamping seats 35 through bearings. Guide rods 36 are fixedly connected to the upper and lower ends of the two arc-shaped clamping seats 35 on the opposite sides. The extended ends of the four guide rods 36 pass through the two sides of the two C-shaped frames 33 and are threadedly connected to the limit nuts 37.

[0040] In this embodiment, it is convenient to install and fix the device.

[0041] All electrical components mentioned in this article are electrically connected to the controller and power supply. The control method of this utility model is controlled by the controller. The control circuit of the controller can be implemented by simple programming by those skilled in the art. The power supply is also common knowledge in the art. Furthermore, this utility model is mainly used to protect mechanical devices, so the control method and circuit connection will not be explained in detail.

[0042] It should be noted that, for the sake of simplicity, the foregoing embodiments are all described as a series of actions. However, those skilled in the art should understand that the present invention is not limited to the described order of actions, as some steps may be performed in other orders or simultaneously according to the present invention. Furthermore, those skilled in the art should also understand that the embodiments described in the specification are preferred embodiments, and the actions and modules involved are not necessarily essential to the present invention.

[0043] It should be understood that the disclosed apparatus can be implemented in other ways, given the several embodiments provided in this application. For example, the apparatus embodiments described above are merely illustrative. For instance, the division of units described above may be implemented in other ways in practice. For example, multiple units or components may be combined or integrated into another system, or some features may be ignored or not executed. Furthermore, the coupling or communication connections shown or discussed may be through some interfaces; indirect coupling or communication connections between devices or units may be telecommunications or other forms.

[0044] The units described above as separate components may or may not be physically separate. The components shown as units may or may not be physical units; that is, they may be located in one place or distributed across multiple network units. Some or all of the units can be selected to achieve the purpose of this embodiment according to actual needs.

[0045] The above embodiments are only used to illustrate the technical solutions of this utility model, and are not intended to limit the scope of protection of this utility model. Obviously, the described embodiments are only some embodiments of this utility model, not all embodiments. Based on these embodiments, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this utility model. Although this utility model has been described in detail with reference to the above embodiments, those skilled in the art can still combine, add, delete, or otherwise adjust the features of the various embodiments of this utility model according to the circumstances without conflict or creative effort, thereby obtaining different technical solutions that do not fundamentally depart from the concept of this utility model. These technical solutions are also within the scope of protection of this utility model.

Claims

1. A hoop-type aviation obstruction light, characterized by, include: A support plate, with a base fixedly connected to the middle of the upper part of the support plate, and a transparent protective cover installed on the base; An installation assembly is provided between the base and the transparent protective cover, and a cleaning assembly is provided on the support plate; The cleaning component includes a motor that is fixedly connected to one side of the upper end of the support plate, and a first gear plate is fixedly connected to the output end of the motor.

2. A hoop type aviation obstruction light as defined in claim 1 wherein, The cleaning components also include a toothed ring fitted around the outside of the base; A sliding ring is fixedly connected to the inner wall of the toothed ring near the base, and a circular groove is provided on the outer wall of the base near the sliding ring. The slip ring and the annular groove are slidably connected, and the first gear plate and the circular gear ring are meshed.

3. A hoop type Obstruction Light as claimed in claim 2, wherein, The cleaning assembly also includes an L-shaped fixing rod fixedly connected to the upper end of the toothed ring, a connecting seat rotatably connected to the top of the transparent protective cover, a connecting plate detachably fixedly connected to the upper end of the connecting seat, the other side of the L-shaped fixing rod being fixedly connected to the connecting plate, and a cleaning sponge brush detachably fixedly connected to the side of the L-shaped fixing rod near the transparent protective cover, with the cleaning sponge brush in contact with the surface of the transparent protective cover.

4. A hoop type aviation obstruction light as defined in claim 3 wherein, The base has a mounting groove at the top, and the main body of the aviation obstruction light is installed inside the mounting groove. The upper part of the main body of the aviation obstruction light is located inside the transparent protective cover. There are heat dissipation holes on both sides of the base. The two heat dissipation holes are filled with filler and are connected to the inside of the mounting groove. Filters can be detachably and fixedly connected inside the two heat dissipation holes.

5. A hoop type Obstruction Light as claimed in claim 4, wherein, The mounting components include a sealing rubber ring fixedly connected to the lower end of the inner wall of a transparent protective cover, which contacts the main body of the aviation obstruction light.

6. A hoop type Obstruction Light as defined in claim 1 wherein, The mounting components also include a U-shaped groove formed at the top of the four sides of the base, a magnetic U-shaped block fixedly connected to the bottom of the four sides of the transparent protective cover, a sealing ring fitted on the upper end of the magnetic U-shaped block, a magnetic plate fixedly connected inside the U-shaped groove, the magnetic U-shaped block and the U-shaped groove being inserted into each other, and the magnetic U-shaped block and the magnetic plate being attracted to each other.

7. A hoop type Obstruction Light as claimed in claim 6, wherein, The mounting components also include connecting slots on both sides of the base and the magnetic loop block. Each pair of connecting slots on each side is interconnected. Positioning slots are provided on both sides of the interior of the base. Two positioning slots are connected to the two sides of the loop block. All four connecting slots are connected to the loop block. Pull rods are provided on both sides of the exterior of the base. Positioning rods are fixedly connected to the sides of the two pull rods that are close to each other. The two positioning rods are inserted through the four connecting slots and the two positioning slots. Springs are sleeved on the two positioning rods. One side of the two springs is fixedly connected to the base. The other side of the two springs is fixedly connected to the two pull rods.

8. A hoop type Obstruction Light as defined in claim 1 wherein, A support rod is fixedly connected to the bottom of the support plate. A fixing component is provided at the extended end of the support rod. The fixing component includes a C-shaped frame fixedly connected to the support rod. A screw is provided in the middle of each side of the C-shaped frame. The two screws are threadedly connected to the C-shaped frame. The extended ends of the two screws pass through the two sides of the C-shaped frame and are connected to arc-shaped clamping seats through bearings. Guide rods are fixedly connected to the upper and lower ends of the two arc-shaped clamping seats on the opposite sides. The extended ends of the four guide rods pass through the two sides of the two C-shaped frames and are threadedly connected to limit nuts.

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