Rotary aviation obstruction beacon

By designing rotating and adjusting components, the problems of poor protection and inconvenient installation of aviation obstruction lights were solved, enabling beam rotation and altitude angle adjustment, thereby enhancing the visibility and protection of the obstruction lights.

CN224246108UActive Publication Date: 2026-05-15ANHUI LIYA AVIATION TECH CO LTD
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
ANHUI LIYA AVIATION TECH CO LTD
Filing Date
2025-02-27
Publication Date
2026-05-15

AI Technical Summary

Technical Problem

Existing aviation obstruction lights have poor protection, are easily damaged by external forces, and cannot be adjusted in terms of installation height and angle, making the flashes difficult to observe.

Method used

A rotary aviation obstruction light was designed, comprising a rotating component, an adjusting component, and a snow removal component. The rotating component rotates the beam, the adjusting component adjusts the height and angle, and a protective frame is provided to enhance protection.

Benefits of technology

It improves the visibility and protection of aviation obstruction lights, ensuring clear identification of obstacles at night or in low visibility conditions, and prevents snow adhesion while maintaining the warning effect of the beam.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model is suitable for the technical field of aviation obstruction beacons, and provides a rotary aviation obstruction beacon which comprises a mounting plate, vertical rods are fixedly connected to the two sides of the upper end of the mounting plate respectively, and the same fixing plate is fixedly connected between the upper ends of the two vertical rods; a rotating assembly is arranged on the fixing plate, an adjusting assembly and a snow removing assembly are arranged on the rotating assembly, and by arranging the rotating assembly, the aviation obstruction beacon body can be conveniently rotated through the rotating assembly, light beams are made to rotate, and therefore warning signals are provided in a larger range; according to the aviation obstruction light, it is ensured that an aircraft can clearly recognize obstacles at night or under the low-visibility condition, by arranging the adjusting assembly, the height and angle of the aviation obstruction light body are conveniently adjusted, the visibility of light beams of the aviation obstruction light body is improved, by arranging the protection frame, the aviation obstruction light body is conveniently protected, and meanwhile the light beams are not affected.
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Description

Technical Field

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

[0002] Aviation obstruction lights, also known as navigational aid lighting equipment, are special lighting fixtures used to identify obstacles. They belong to the navigational aid lighting equipment industry, and aviation obstruction lights are a specific category within this industry. To distinguish them from general-purpose lighting, aviation obstruction lights are not constantly lit but flashing. Low-intensity aviation obstruction lights are constantly lit, while medium-intensity and high-intensity aviation obstruction lights flash, with a flashing frequency of no less than 20 times per minute and no more than 60 times per minute. The purpose of aviation obstruction lights is to display the outline of structures, enabling aircraft operators to judge the height and outline of obstacles, thus serving as a warning.

[0003] Application CN202222837075.8 discloses an aviation obstruction light device, including a support plate. A servo motor is bolted to the top of the support plate, and the shaft of the servo motor is fixedly connected to the obstruction light body. A cleaning mechanism is riveted to the left side of the support plate, and a first support plate is riveted to the right side. A first electric push rod is bolted to the bottom of the first support plate, and a drying chamber is fixedly connected to the top of the first electric push rod through the first support plate. A fan is installed through the right side of the drying chamber, and a heating wire is bolted to the bottom of the inner cavity of the drying chamber. A drying hole is provided on the left side of the drying chamber. This invention, through the cooperation of the fan, heating wire, and drying chamber, has the advantage of snow removal function. It can heat-melt the snow on the surface of the obstruction light body in rainy or snowy weather, preventing snow from adhering to the surface of the obstruction light body, thereby improving the subsequent obstruction indication effect.

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

[0005] Existing technologies offer poor protection against aviation obstructions and are easily damaged by external impacts; the installation height and angle of aviation obstruction lights cannot be adjusted, and the flash is not easily observed when the installation angle is inconsistent with that of other aviation obstruction lights. Utility Model Content

[0006] This utility model provides a rotary aviation obstruction light, which aims to solve the problems of poor protection of existing aviation obstruction lights, easy damage from external impacts, inability to adjust the installation height and angle of the aviation obstruction light, and difficulty in observing the flash when the installation angle is inconsistent with other aviation obstruction lights.

[0007] This utility model is implemented as follows: a rotating aviation obstruction light includes: a mounting plate, on which uprights are fixedly connected to both sides of the upper end of the mounting plate, and a fixed plate is fixedly connected between the upper ends of the two uprights; a rotating assembly is provided on the fixed plate, and an adjusting assembly and a snow removal assembly are provided on the rotating assembly; the rotating assembly includes a first motor installed at the bottom of the fixed plate, the output end of the first motor passes through the fixed plate and is fixedly connected to a rotating plate, and guide balls are fixedly connected to both sides of the bottom of the rotating plate.

[0008] Preferably, the rotating assembly further includes a circular groove formed on the fixed plate, and both guide balls are slidably connected to the circular groove; the adjusting assembly includes a fixed cylinder fixedly connected to one side of the upper end of the rotating plate, the upper end of the fixed cylinder has a groove, and a magnetic ring is fixedly connected to the inner wall of the groove; a movable cylinder is slidably connected inside the groove, and several magnetic strips are fixedly connected to the side wall of the movable cylinder, and the several magnetic strips are slidably attracted to the magnetic ring.

[0009] Preferably, the adjustment assembly further includes a C-shaped fixing frame fixedly connected to the upper end of the movable cylinder. A stabilizing plate is fixedly connected to one side of the C-shaped fixing frame, and a second motor is mounted on the stabilizing plate. The output end of the second motor passes through one side of the C-shaped fixing frame and is fixedly connected to a rotating rod. The extended end of the rotating rod is rotatably connected to the inner wall of the other side of the C-shaped fixing frame. Several reinforcing ribs are fixedly connected to the rotating rod, and a mounting base is fixedly connected to the rotating rod.

[0010] Preferably, an aviation obstruction light body is detachably and fixedly connected to the mounting base, and a protective frame is detachably and fixedly connected to the outside of the aviation obstruction light body.

[0011] Preferably, the snow removal assembly includes an electric telescopic rod fixedly connected to the other side of the upper end of the rotating plate, the telescopic end of the electric telescopic rod is fixedly connected to a mounting block, and the upper end of the mounting block is detachably fixedly connected to a U-shaped frame.

[0012] Preferably, the snow removal assembly further includes a plurality of electrically heated wires connected in series and fixedly connected to the inside of the U-shaped frame near the side of the adjustment assembly.

[0013] Preferably, the snow removal assembly further includes a mounting frame disposed in the middle of the U-shaped frame, a connecting rod detachably and fixedly connected between the mounting frame and the inner wall of the U-shaped frame, a fan detachably and fixedly connected to the mounting frame, and a filter screen detachably and fixedly connected to the other side of the inside of the U-shaped frame.

[0014] Preferably, the U-shaped fixing frame is provided with a bird-repelling component, which includes mounting slots on the top of both sides of the U-shaped fixing frame, a third motor is installed inside each of the two mounting slots, and a bird-repelling rod is fixedly connected to the output end of each of the two third motors.

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

[0016] By incorporating a rotating component, the aviation obstruction light body can be rotated, allowing the beam to rotate and thus providing a warning signal over a wider area. This ensures that aircraft can clearly identify obstacles at night or in low visibility conditions. The adjustment component allows for easy adjustment of the height and angle of the aviation obstruction light body, improving the visibility of the beam. The protective frame provides protection for the aviation obstruction light body without affecting the beam. Attached Figure Description

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

[0018] Figure 2 This is a schematic diagram of the structure of the U-shaped fixing bracket of this utility model;

[0019] Figure 3 This is a side view of the structure of the loop-shaped frame of this utility model;

[0020] Figure 4 This is a front view cross-sectional structural diagram of the loop-shaped frame of this utility model;

[0021] Figure 5 This is a utility model Figure 2 Enlarged structural diagram at point A in the middle;

[0022] Figure 6 This is a top view cross-sectional structural diagram of the fixed cylinder of this utility model;

[0023] In the diagram: 1. Mounting plate; 2. Upright pole; 4. Fixing plate; 5. Rotating assembly; 6. First motor; 7. Rotating plate; 8. Guide ball; 9. Circular groove; 10. Snow removal assembly; 11. Adjustment assembly; 12. Fixing cylinder; 13. Magnetic ring; 14. Movable cylinder; 15. Magnetic strip; 17. C-shaped fixing frame; 18. Stabilizing plate; 19. Second motor; 20. Rotating rod; 21. Reinforcing rib; 22. Mounting base; 23. Aviation obstruction light body; 24. Mounting slot; 25. Third motor; 26. Bird deterrent pole; 27. Electric telescopic pole; 28. Mounting block; 29. ​​U-shaped frame; 30. Electric heating wire; 31. Mounting bracket; 32. Fan; 33. Filter screen. Detailed Implementation

[0024] 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.

[0025] 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.

[0026] This utility model embodiment provides a rotary aviation obstruction light, such as Figure 1-6 As shown, it includes: a mounting plate 1, with uprights 2 fixedly connected to both sides of the upper end of the mounting plate 1, and a fixed plate 4 fixedly connected between the upper ends of the two uprights 2; a rotating assembly 5 is provided on the fixed plate 4, and an adjusting assembly 11 and a snow removal assembly 10 are provided on the rotating assembly 5; the rotating assembly 5 includes a first motor 6 installed at the bottom of the fixed plate 4, and a rotating plate 7 is fixedly connected to the output end of the first motor 6 through the fixed plate 4, with guide balls 8 fixedly connected to both sides of the bottom of the rotating plate 7.

[0027] It should be noted that existing technologies offer poor protection against aviation obstructions and are easily damaged by external impacts. Furthermore, the height and angle of the aviation obstruction light cannot be adjusted, making it difficult to observe the flash when the angle differs from other aviation obstruction lights. This solution addresses this by incorporating a rotating component 5, which allows the aviation obstruction light body 23 to be rotated, thus providing a wider warning signal and ensuring clear obstacle identification for aircraft at night or in low visibility conditions. The adjustment component 11 facilitates adjustment of the height and angle of the aviation obstruction light body 23, improving the beam visibility. Finally, a protective frame protects the aviation obstruction light body 23 without affecting the beam.

[0028] In a further preferred embodiment of this utility model, such as Figure 1-6As shown, the rotating assembly 5 also includes a circular groove 9 formed on the fixed plate 4, and the two guide balls 8 are slidably connected to the circular groove 9; the adjusting assembly 11 includes a fixed cylinder 12 fixedly connected to one side of the upper end of the rotating plate 7, the upper end of the fixed cylinder 12 is provided with a groove, and a magnetic ring 13 is fixedly connected to the inner wall of the groove; a movable cylinder 14 is slidably connected inside the groove, and a number of magnetic strips 15 are fixedly connected to the side wall of the movable cylinder 14, and the number of magnetic strips 15 are slidably attracted to the magnetic ring 13.

[0029] In this embodiment, by sliding the movable cylinder 14 upward, it is easy for the movable cylinder 14 to slide out of the fixed cylinder 12, thereby facilitating height adjustment. By setting several magnetic strips 15 to slide and attract the magnetic ring 13, it is easy to fix the sliding distance.

[0030] In a further preferred embodiment of this utility model, such as Figure 1-5 As shown, the adjustment assembly 11 also includes a C-shaped fixing frame 17 fixedly connected to the upper end of the movable cylinder 14. A stabilizing plate 18 is fixedly connected to one side of the C-shaped fixing frame 17. A second motor 19 is mounted on the stabilizing plate 18. The output end of the second motor 19 passes through one side of the C-shaped fixing frame 17 and is fixedly connected to a rotating rod 20. The extended end of the rotating rod 20 is rotatably connected to the inner wall of the other side of the C-shaped fixing frame 17. Several reinforcing ribs 21 are fixedly connected to the rotating rod 20. A mounting base 22 is fixedly connected to the rotating rod 20.

[0031] In this embodiment, by starting the second motor 19, the rotating rod 20 can be driven to rotate, thereby facilitating the rotation of the aviation obstruction light body 23.

[0032] In a further preferred embodiment of this utility model, such as Figure 1-5 As shown, an aviation obstruction light body 23 is detachably and fixedly connected to the mounting base 22, and a protective frame is detachably and fixedly connected to the outside of the aviation obstruction light body 23.

[0033] In this embodiment, protection is facilitated.

[0034] In a further preferred embodiment of this utility model, such as Figure 1-4 As shown, the snow removal assembly 10 includes an electric telescopic rod 27 fixedly connected to the other side of the upper end of the rotating plate 7. The telescopic end of the electric telescopic rod 27 is fixedly connected to a mounting block 28, and the upper end of the mounting block 28 is detachably fixedly connected to a U-shaped frame 29.

[0035] In this embodiment, installation and disassembly are convenient.

[0036] In a further preferred embodiment of this utility model, such as Figure 1-4 As shown, the snow removal assembly 10 also includes a plurality of electrically heated wires 30 connected in series, which are fixedly connected inside the U-shaped frame 29 on the side near the adjustment assembly 11.

[0037] In this embodiment, after the electric heating wire 30 is activated, the wind blown by the fan 32 toward the aviation obstruction light body 23 is hot air.

[0038] In a further preferred embodiment of this utility model, such as Figure 1-4 As shown, the snow removal assembly 10 also includes a mounting bracket 31 in the middle of the U-shaped frame 29. A connecting rod is detachably and fixedly connected between the mounting bracket 31 and the inner wall of the U-shaped frame 29. A fan 32 is detachably and fixedly connected to the mounting bracket 31. A filter screen 33 is detachably and fixedly connected to the other side of the inside of the U-shaped frame 29.

[0039] In this embodiment, it is convenient to install the fan 32, and dust is prevented from adhering to the fan 32 when it is drawing air.

[0040] In a further preferred embodiment of this utility model, such as Figure 1-5 As shown, a bird deterrent assembly is provided on the U-shaped fixing frame 17. The bird deterrent assembly includes mounting slots 24 on the top of both sides of the U-shaped fixing frame 17. A third motor 25 is installed inside the two mounting slots 24 respectively, and the output ends of the two third motors 25 are fixedly connected to bird deterrent rods 26 respectively.

[0041] In this embodiment, the output of the third motor 25 rotates, which drives the bird deterrent rod 26 to rotate, thereby facilitating the bird deterrent rod 26 to drive away birds.

[0042] 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.

[0043] 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.

[0044] 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.

[0045] 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.

[0046] 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 rotating aviation obstruction light, characterized in that, Includes: a mounting plate, with uprights fixedly connected to both sides of the upper end of the mounting plate, and the same fixing plate fixedly connected between the upper ends of the two uprights; A rotating component is provided on the fixed plate, and an adjusting component and a snow removal component are provided on the rotating component; The rotating assembly includes a first motor mounted on the bottom of a fixed plate. The output end of the first motor passes through the fixed plate and is fixedly connected to a rotating plate. Guide balls are fixedly connected to both sides of the bottom of the rotating plate.

2. A rotating aviation obstruction light as described in claim 1, characterized in that, The rotating assembly also includes a circular groove formed on the fixed plate, and both guide balls are slidably connected to the circular groove; The adjustment assembly includes a fixed cylinder that is fixedly connected to one side of the upper end of the rotating plate. The upper end of the fixed cylinder has a groove, and a magnetic ring is fixedly connected to the inner wall of the groove. A movable cylinder is slidably connected inside the groove, and several magnetic strips are fixedly connected to the side wall of the movable cylinder. All the magnetic strips slide and attract the magnetic ring.

3. A rotating aviation obstruction light as described in claim 2, characterized in that, The adjustment assembly also includes a C-shaped fixing frame that is fixedly connected to the upper end of the movable cylinder. A stabilizing plate is fixedly connected to one side of the C-shaped fixing frame, and a second motor is installed on the stabilizing plate. The output end of the second motor passes through one side of the C-shaped fixing frame and is fixedly connected to a rotating rod. The extended end of the rotating rod is rotatably connected to the inner wall of the other side of the C-shaped fixing frame. Several reinforcing ribs are fixedly connected to the rotating rod, and a mounting base is fixedly connected to the rotating rod.

4. A rotating aviation obstruction light as described in claim 3, characterized in that, The mounting base is detachably and fixedly connected to the aviation obstruction light body, and the exterior of the aviation obstruction light body is detachably and fixedly connected to a protective frame.

5. A rotating aviation obstruction light as described in claim 1, characterized in that, The snow removal assembly includes an electric telescopic rod that is fixedly connected to the other side of the upper part of the rotating plate. The telescopic end of the electric telescopic rod is fixedly connected to a mounting block, and the upper end of the mounting block is detachably fixedly connected to a U-shaped frame.

6. A rotating aviation obstruction light as described in claim 5, characterized in that, The snow removal assembly also includes a number of electrically heated wires connected in series, which are fixedly connected inside the U-shaped frame on the side near the adjustment assembly.

7. A rotating aviation obstruction light as described in claim 6, characterized in that, The snow removal assembly also includes a mounting frame in the middle of a U-shaped frame, a connecting rod that is detachably and fixedly connected between the mounting frame and the inner walls of the U-shaped frame, a fan that is detachably and fixedly connected to the mounting frame, and a filter screen that is detachably and fixedly connected to the other side of the inside of the U-shaped frame.

8. A rotating aviation obstruction light as described in claim 3, characterized in that, The U-shaped fixing frame is equipped with a bird deterrent component, which includes mounting slots on the top of both sides of the U-shaped fixing frame. A third motor is installed inside each of the two mounting slots, and the output ends of the two third motors are fixedly connected to bird deterrent rods.