Slide rail type aviation obstruction beacon convenient to fix

Abstract

The invention is suitable for the technical field of illumination, and provides a sliding rail type aviation obstruction beacon convenient to fix, which comprises a support base and a fixed disc arranged in the middle of the support base, an annular sliding rail is arranged on the inner side wall of the supporting base, and a sliding block is arranged on the sliding rail in a sliding fit mode. The sliding block and the fixing disc are provided with the same assembling base, a feeding lead screw is arranged in the assembling base, and a nut block is arranged on the feeding lead screw in a threaded fit mode. The nut block is provided with a first bearing, an upper lamp bracket and an aviation obstruction light; by providing double flexible adjustability of height and position, the aviation obstruction beacon can easily adapt to various complex environments and variable illumination requirements, stable connection of the lamp arms and arrangement of the lamp grooves in the upper lamp bracket are enhanced, and the stability and safety of the aviation obstruction beacon are jointly ensured; due to the effective energy storage and release mechanism of the storage battery, the dependence on traditional energy is remarkably reduced, and the illumination requirement at night or in severe weather is met.

Description

Technical Field

[0001] The invention belongs to the technical field of lighting, and in particular relates to a slide-rail aviation obstruction light that is easy to fix. Background Art

[0002] Aviation obstruction lights are widely used on tall buildings such as high-rise buildings, tower cranes, and bridges to ensure that aircraft can accurately identify these obstacles at night or in bad weather conditions, thereby effectively avoiding potential collision risks; however, the traditional way of fixing aviation obstruction lights faces many challenges and limitations;

[0003] First, the traditional fixing method mostly uses bolts for fastening, which is a cumbersome and complicated process that requires professional installation tools, which not only increases the installation cost but also limits the convenience of installation;

[0004] Secondly, traditional aviation obstruction lights often lack the ability to move flexibly in height, horizontal position and circular area, which limits the expansion of their lighting range and the optimization of lighting effects; in complex and changing lighting environments, this fixed design often cannot provide sufficient flexibility and adaptability;

[0005] Furthermore, traditional aviation obstruction lights are often not usable in remote areas or places lacking stable power supply because they rely on a stable power supply; this not only limits the scope of application of aviation obstruction lights, but also makes it impossible to effectively guarantee aviation safety in these areas at night or in severe weather conditions. Summary of the invention

[0006] The present invention provides a slide rail type aviation obstruction light which is easy to fix, aiming to solve the problems that the traditional aviation obstruction light fixing method has many limitations in terms of installation convenience, adjustment flexibility and application scope.

[0007] The present invention is implemented as follows: a slide rail type aviation obstruction light that is easy to fix includes a support base, the cross section of the support base is circular; a fixed plate is arranged in the middle of the support base; an annular slide rail is provided on the inner side wall of the support base, and a slider is slidably matched on the slide rail; the slider and the fixed plate are provided with the same assembly seat, and the assembly seat and the fixed plate are rotatably matched; a driving motor is provided at the bottom position of the fixed plate, and the output end of the driving motor is fixedly connected with the end key of the assembly seat; a feed screw is provided in the assembly seat, and a nut block is threadedly matched on the feed screw; a lower lamp holder is provided on the nut block; four corners on the upper surface of the lower lamp holder Guide columns are provided at the corner positions; the same upper lamp frame is slidably fitted on the four guide columns; a lamp trough lower than its horizontal height is provided in the middle position of the upper surface of the upper lamp frame; a magnetic pad is provided on the lamp trough; an aviation obstruction light is provided on the magnetic pad, and a magnetic adsorption layer is provided at the bottom of the aviation obstruction light; a group of support seats are provided on both sides of the upper lamp frame adjacent to the aviation obstruction light; arc-shaped support grooves with opposite openings are provided on opposite sides of the two support seats; a number of fastening springs are provided in the two support grooves, and dampers are integrated in the fastening springs; a fastening pad is provided on the side of the fastening springs away from the corresponding support grooves.

[0008] Preferably, the two side edges of the two support seats extend outward to form fastening plates facing each other, and the outer side walls of the fastening plates are provided with press buckles.

[0009] Preferably, a U-shaped fastening sleeve is further included, and limiting slots are provided on both sides of the fastening sleeve, and the inner diameter of the limiting slots matches the outer diameter of the pressing buckle.

[0010] Preferably, a hydraulic cylinder is provided in the middle of the upper surface of the lower lamp frame, and the telescopic end of the hydraulic cylinder is connected to the bottom position of the upper lamp frame.

[0011] Preferably, a plurality of reinforced lamp arms are provided on a side of the fixing plate opposite to the supporting base.

[0012] Preferably, a servo motor is provided on the end side of the assembly seat, and the output end of the servo motor is fixedly connected to the end key of the feed screw.

[0013] Preferably, an extension bracket is provided on the outer side wall of the assembly seat, and a group of solar panels are provided on the extension bracket; an inverter and a battery electrically connected to the solar panels are provided under the extension bracket.

[0014] Preferably, a limit block is provided at the top position of the guide column.

[0015] Compared with the prior art, the embodiments of the present application have the following beneficial effects:

[0016] First, the design of the present invention allows the assembly seat and the aviation obstruction light thereon to rotate and slide at a certain angle. This feature further meets the lighting requirements in different scenarios. At the same time, in conjunction with the horizontally movable nut block, the movement trajectory of the aviation obstruction light is significantly expanded, making the lighting range wider. In addition, the height-adjustable upper lamp frame and the components thereon can be accurately moved up and down along the guide column rod, thereby realizing the flexible adjustment of the height of the aviation obstruction light. This dual flexible adjustability of height and position enables the device to easily adapt to a variety of complex environments and changing lighting requirements, greatly enhancing its practicality and adaptability.

[0017] Second, the reinforced lamp arm of the device is a key component connecting the fixing plate and the supporting base, which significantly improves the connection strength between the two, thereby enhancing the stability of the entire structure. A lamp trough and a magnetic pad are specially designed on the upper surface of the upper lamp frame. This design can initially and firmly fix the aviation obstruction light. At the same time, the support seats on both sides of the aviation obstruction light further ensure that the aviation obstruction light will not fall off due to vibration during flight. In addition, the design of the U-shaped fastening sleeve and the press buckle provides additional support and stability for the entire structure, making the connection between the two support seats more secure and almost impossible to loosen.

[0018] Compared with the traditional fixing method, this stable and reliable structural design is easy to install and disassemble. It not only ensures the continuous working ability of the aviation obstruction light under severe weather conditions, but also significantly improves the safety and reliability of the entire device.

[0019] Thirdly, the storage battery of the present invention can effectively store the electric energy generated by the solar panels when there is excess electric energy, and release the electric energy when needed to supply loads such as aviation obstruction lights. This design not only significantly reduces the dependence on traditional energy, thereby reducing the overall operating cost, but also ensures the continuous working ability of key loads such as aviation obstruction lights, thereby effectively guaranteeing the lighting needs at night or in bad weather. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 It is a three-dimensional structural schematic diagram of the present invention;

[0021] Figure 2 It is a three-dimensional structural schematic diagram of the present invention;

[0022] Figure 3 It is a three-dimensional structural schematic diagram of the present invention;

[0023] Figure 4 is a left ventricular map of the present invention;

[0024] Figure 5 It is a right side view of the present invention;

[0025] Figure 6 It is a partial structural schematic diagram of the present invention;

[0026] Figure 7 It is a partial structural schematic diagram of the present invention;

[0027] Figure 8 It is a schematic diagram of a partial three-dimensional structure of the present invention;

[0028] In the figure: 1. Support base; 2. Fixed plate; 3. Slide rail; 4. Slider; 5. Assembly seat; 6. Drive motor; 7. Feed screw; 8. Nut block; 9. Lower lamp frame; 10. Guide column; 11. Upper lamp frame; 12. Light trough; 13. Magnetic pad; 14. Aviation obstruction light; 15. Support seat; 16. Fastening spring; 17. Fastening pad; 18. Fastening plate; 19. Press buckle; 20. Fastening sleeve; 21. Limiting slot; 22. Hydraulic cylinder; 23. Strengthening lamp arm; 24. Servo motor; 25. Extension bracket; 26. Solar panel; 27. Limiting block. DETAILED DESCRIPTION

[0029] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as those commonly understood by technicians in the technical field of this application; the terms used in the specification of the application herein are only for the purpose of describing specific embodiments and are not intended to limit this application; the terms "including" and "having" and any variations thereof in the specification and claims of this application and the above-mentioned drawings are intended to cover non-exclusive inclusions. The terms "first", "second", etc. in the specification and claims of this application or the above-mentioned drawings are used to distinguish different objects, not to describe a specific order.

[0030] Reference to "embodiments" herein means that a particular feature, structure, or characteristic described in conjunction with the embodiments may be included in at least one embodiment of the present application. The appearance of the phrase in various locations in the specification does not necessarily refer to the same embodiment, nor is it an independent or alternative embodiment that is mutually exclusive with other embodiments. It is explicitly and implicitly understood by those skilled in the art that the embodiments described herein may be combined with other embodiments.

[0031] The embodiment of the present invention provides a slide rail type aviation obstruction light which is easy to fix. Figure 1-8As shown, it includes a support base 1, the cross section of which is circular; a fixed plate 2 is arranged in the middle of the support base 1; an annular slide rail 3 is provided on the inner side wall of the support base 1, and a slider 4 is slidably matched on the slide rail 3; the slider 4 and the fixed plate 2 are provided with the same assembly seat 5, and the assembly seat 5 and the fixed plate 2 are rotationally matched; a driving motor 6 is provided at the bottom position of the fixed plate 2, and the output end of the driving motor 6 is fixedly connected with the end key of the assembly seat 5; a feed screw 7 is provided in the assembly seat 5, and a nut block 8 is threadedly matched on the feed screw 7; a lower lamp holder 9 is provided on the nut block 8; four corner positions on the upper surface of the lower lamp holder 9 are provided with guide posts 10; four guide posts 10 are provided An upper lamp holder 11 is slidably engaged with the pole 10; a lamp trough 12 which is lower than its horizontal height is provided in the middle of the upper surface of the upper lamp holder 11; a magnetic pad 13 is provided on the lamp trough 12; an aviation obstruction light 14 is provided on the magnetic pad 13, and a magnetic adsorption layer is provided at the bottom of the aviation obstruction light 14; a group of support seats 15 are provided on both sides of the upper lamp holder 11 adjacent to the aviation obstruction light 14; arc-shaped support grooves with opposite openings are provided on opposite sides of the two support seats 15; a plurality of fastening springs 16 are provided in the two support grooves, and a damper is integrated in the fastening spring 16; a fastening pad 17 is provided on each side of the plurality of fastening springs 16 away from the corresponding support grooves.

[0032] It should be noted that due to the many limitations of the traditional aviation obstruction light fixing method in terms of installation convenience, adjustment flexibility and scope of application, this solution greatly improves the practicality and adaptability of the device by realizing the dual flexible adjustability of the aviation obstruction light 14 in height and position, so that it can easily cope with a variety of complex environments and changing lighting needs. The strengthening of the lamp arm 23 significantly enhances the structural stability, and the fastening components that are easy to disassemble and assemble ensure the firmness and safety of the aviation obstruction light 14 during flight and severe weather conditions. In addition, the battery's intelligent energy storage and power supply system not only effectively reduces dependence on traditional energy and overall operating costs, but also ensures the continuous working ability of key loads such as aviation obstruction lights 14.

[0033] Specifically, in this embodiment, the scheme mainly includes a support base 1, which is located in the middle of the support base 1 and is provided with a fixed plate 2; an annular slide rail 3 is provided on the inner side wall of the support base 1, and a slider 4 is slidably matched on the slide rail 3, so that an assembly seat 5 connected to the slider 4 can slide freely on the support base 1 to achieve preliminary adjustment of the position;

[0034] The assembly seat 5 and the fixed plate 2 are rotationally matched, which allows the assembly seat 5 to rotate on the fixed plate 2 at a certain angle to meet different lighting requirements; a driving motor 6 is provided at the bottom of the fixed plate 2, and the output end of the driving motor 6 is fixedly connected with the end key of the assembly seat 5. Through the operation of the driving motor 6, the assembly seat 5 and the components connected thereto can be driven to perform precise sliding positioning on the slide rail 3;

[0035] A feed screw 7 is provided inside the assembly seat 5, and a nut block 8 is threadedly matched on the feed screw 7; when the feed screw 7 rotates, the nut block 8 moves horizontally along the feed screw 7, further expanding the movement trajectory of the aviation obstruction light 14, and a lower light frame 9 is provided on the nut block 8, and the upper light frame 11 can slide up and down through the guide column 10, thereby adjusting the height of the aviation obstruction light 14 installed thereon;

[0036] A lamp trough 12 is provided in the middle of the upper surface of the upper lamp frame 11 for installing an aviation obstruction light 14; a magnetic pad 13 is provided on the lamp trough 12, and the magnetic pad 13 is magnetic and can absorb the magnetic adsorption layer at the bottom of the aviation obstruction light 14 to achieve preliminary fixation of the aviation obstruction light 14; in order to ensure that the aviation obstruction light 14 will not fall off due to vibration during flight, a group of support seats 15 are provided on both sides of the upper lamp frame 11 adjacent to the aviation obstruction light 14; arc-shaped support grooves with opposite openings are provided on opposite sides of the two support seats 15, and a plurality of fastening springs 16 are provided in the support grooves, and dampers are integrated in the fastening springs 16 to increase the stability of fastening and the buffering effect; a fastening pad 17 is provided on the side away from the corresponding support groove of the plurality of fastening springs 16, and when the aviation obstruction light 14 is placed on the magnetic pad 13, the fastening pad 17 will be close to the outer side of the aviation obstruction light 14 under the action of the fastening spring 16, so as to further fix the position of the aviation obstruction light 14.

[0037] In a further preferred embodiment of the present invention, Figure 6-8 As shown, the two side edges of the two support seats 15 extend outward to form fastening plates 18 facing each other, and the outer side walls of the fastening plates 18 are provided with pressing buckles 19.

[0038] In this embodiment, the press buckle 19 serves as a connecting component and has the function of quick locking and releasing. When the two support bases 15 need to be further connected together, the user only needs to simply align and bring the two fastening plates 18 close together, and then press the buckle 19 to achieve a firm connection with the external structure.

[0039] In a further preferred embodiment of the present invention, Figure 6-8 As shown, a U-shaped fastening sleeve 20 is also included, and limiting slots 21 are formed through both sides of the fastening sleeve 20 . The inner diameter of the limiting slots 21 matches the outer diameter of the pressing buckle 19 .

[0040] In this embodiment, when the two support seats 15 need to be connected together, the two fastening plates 18 are aligned and brought close together, and then the U-shaped fastening sleeve 20 is inserted from the side to ensure that the pressing buckle 19 is aligned with the limiting slot 21. Then, the pressing buckle 19 is gently pressed, and the lock tongue of the pressing buckle 19 will pop out and firmly embed into the limiting slot 21, forming a stable connection that is not easy to loosen;

[0041] The advantage of this design is that the U-shaped fastening sleeve 20 not only provides additional support and stability, but also avoids the cumbersome process of fixing with tools through the cooperation of the limiting slot 21 and the press buckle 19, thereby achieving a more secure connection. Even under the action of external force, the connection is not easy to loosen or fall off, thereby improving the reliability and durability of the entire structure.

[0042] In a further preferred embodiment of the present invention, Figure 4-5 As shown, a hydraulic cylinder 22 is provided in the middle of the upper surface of the lower lamp frame 9 , and the telescopic end of the hydraulic cylinder 22 is connected to the bottom position of the upper lamp frame 11 .

[0043] In this embodiment, when the height of the aviation obstruction light 14 needs to be adjusted, the telescopic end of the hydraulic cylinder 22 is extended or shortened, thereby driving the upper lamp frame 11 and the components thereon to move up and down. Since the hydraulic cylinder 22 has the characteristics of high precision and strong stability, it can ensure the stability and accuracy of the upper lamp frame 11 during movement, thereby achieving the purpose of height adjustment of the aviation obstruction light 14.

[0044] In a further preferred embodiment of the present invention, Figure 1-3 As shown, a plurality of reinforced lamp arms 23 are provided on a side of the fixing plate 2 opposite to the supporting base 1 .

[0045] In this embodiment, the reinforced lamp arm 23 is a key component for connecting the fixing plate 2 and the supporting base 1 , which not only enhances the connection strength between the two, but also improves the stability of the entire structure.

[0046] In a further preferred embodiment of the present invention, Figure 1-3 As shown, a servo motor 24 is provided on the end side of the assembly seat 5 , and the output end of the servo motor 24 is fixedly connected to the end of the feed screw 7 by a key.

[0047] In this embodiment, the servo motor 24 rotates the feed screw 7 at a specific speed and direction. Due to the threaded fit between the feed screw 7 and the nut block 8, the nut block 8 moves horizontally with the rotation of the feed screw 7. This movement is transmitted to the upper light bracket 11 through the lower light bracket 9, and finally drives the aviation obstruction light 14 to move up and down to the desired position.

[0048] In a further preferred embodiment of the present invention, Figure 1As shown, an extension bracket 25 is disposed on the outer side wall of the mounting base 5 , and a group of solar panels 26 are disposed on the extension bracket 25 ; an inverter and a battery electrically connected to the solar panels 26 are disposed under the extension bracket 25 .

[0049] In this embodiment, the solar panel 26 converts the received solar energy into electrical energy. A battery is also arranged under the inverter. The battery is electrically connected to the inverter and can store electrical energy when there is excess electrical energy generated by the solar panel 26. It can release the electrical energy to supply the load when needed. This design not only improves the energy utilization efficiency of the entire device, but also ensures the continuous working ability of loads such as the aviation obstruction light 14 under severe weather conditions.

[0050] In a further preferred embodiment of the present invention, Figure 7 As shown, a limit block 27 is provided at the top position of the guide column 10 .

[0051] In this embodiment, when the upper lamp frame 11 moves up and down on the guide column 10, the limit block 27 will contact the corresponding part of the upper lamp frame 11 and generate resistance, thereby limiting its movement range, ensuring the accuracy and controllability of the aviation obstruction light 14 when adjusting the height.

[0052] Working principle: The support base 1 of the present invention is provided with a fixing plate 2; the strengthening lamp arm 23 is used as a component connecting the fixing plate 2 and the support base 1, which not only significantly enhances the connection strength between the two, but also greatly improves the stability of the entire structure; the inner side wall of the support base 1 is provided with an annular slide rail 3, and a slider 4 is slidably matched on the slide rail 3. This design enables the assembly seat 5 closely connected with the slider 4 to slide in an annular manner on the support base 1, thereby realizing the preliminary adjustment of the position of the aviation obstruction light 14;

[0053] The assembly seat 5 and the fixed plate 2 are rotated together. This design allows the assembly seat 5 to rotate on the fixed plate 2 at a certain angle to meet various lighting requirements. In order to more accurately control the sliding positioning of the assembly seat 5 and its connected components on the slide rail 3, a drive motor 6 is provided at the bottom of the fixed plate 2. The output end of the drive motor 6 is fixedly connected to the end of the assembly seat 5 through a key. The operation of the drive motor 6 can drive the assembly seat 5 and its connected components to slide accurately on the slide rail 3.

[0054] A feed screw 7 is arranged inside the assembly seat 5, and a nut block 8 is threadedly matched on the feed screw 7; when the servo motor 24 rotates the feed screw 7 at a specific speed and direction, due to the thread matching relationship between the feed screw 7 and the nut block 8, the nut block 8 will move horizontally with the rotation of the feed screw 7, further expanding the movement trajectory of the aviation obstruction light 14;

[0055] The nut block 8 is provided with a lower lamp frame 9, and the upper lamp frame 11 can slide up and down through the guide column 10, so as to conveniently adjust the height of the aviation obstruction light 14 installed thereon; in order to achieve accurate adjustment of the height of the aviation obstruction light 14, the telescopic end of the hydraulic cylinder 22 will be extended or shortened, thereby driving the upper lamp frame 11 and the components thereon to move up and down along the guide column 10; since the hydraulic cylinder 22 has the characteristics of high precision and strong stability, it can ensure the stability and accuracy of the upper lamp frame 11 during the movement;

[0056] A lamp trough 12 is specially provided in the middle of the upper surface of the upper lamp frame 11 for installing the aviation obstruction light 14; a magnetic pad 13 is provided on the lamp trough 12, and the magnetic pad 13 can absorb the magnetic adsorption layer at the bottom of the aviation obstruction light 14 by its magnetism, so as to realize the preliminary fixation of the aviation obstruction light 14; in order to ensure that the aviation obstruction light 14 will not fall off due to vibration during flight, a group of support seats 15 are also provided on both sides of the upper lamp frame 11 adjacent to the aviation obstruction light 14; arc-shaped support grooves with opposite openings are provided on the opposite sides of the two support seats 15, and a plurality of fastening springs 16 are respectively provided in the support grooves; dampers are integrated in these fastening springs 16 to increase the stability and buffering effect of fastening; a fastening pad 17 is respectively provided on the side of the plurality of fastening springs 16 away from the corresponding support grooves; when the aviation obstruction light 14 is placed on the magnetic pad 13, the fastening pad 17 will be close to the outer side of the aviation obstruction light 14 under the action of the fastening spring 16, so as to further fix the position of the aviation obstruction light 14;

[0057] When it is necessary to further connect the two support seats 15 together, the user only needs to align and bring the two fastening plates 18 closer together, and then press the buckle 19 to achieve a firm connection; the design of the U-shaped fastening sleeve 20 provides additional support and stability; when it is necessary to connect the two support seats 15 together, the user only needs to align and bring the two fastening plates 18 closer together, and then insert the U-shaped fastening sleeve 20 from the side, and ensure that the pressing buckle 19 is aligned with the limiting slot 21; then gently press the pressing buckle 19, and the lock tongue of the pressing buckle 19 will pop out and firmly embed into the limiting slot 21, forming a stable connection that is not easy to loosen;

[0058] In addition, the entire device is also equipped with a solar power supply system; the solar panel 26 is responsible for converting the received solar energy into electrical energy, and the battery arranged under the inverter can store electrical energy when there is excess electrical energy generated by the solar panel 26, and release electrical energy when needed to supply the aviation obstruction light 14 load; this design not only improves the energy utilization efficiency of the entire device, but also ensures the continuous working ability of loads such as the aviation obstruction light 14 under severe weather conditions.

[0059] It should be noted that, for the above-mentioned embodiments, for the sake of simplicity, they are all described as a series of action combinations, but those skilled in the art should know that the present invention is not limited by the described order of actions, because according to the present invention, some steps may be performed in other orders or simultaneously. Secondly, those skilled in the art should also know that the embodiments described in the specification are all preferred embodiments, and the actions and modules involved are not necessarily required by the present invention.

[0060] In the several embodiments provided in the present application, it should be understood that the disclosed devices can be implemented in other ways. For example, the device embodiments described above are merely schematic, such as the division of the above-mentioned units. There may be other division methods in actual implementation, such as multiple units or components can be combined or integrated into another system, or some features can be ignored or not executed. Another point is that the mutual coupling or communication connection shown or discussed can be through some interfaces, and the indirect coupling or communication connection between devices or units can be in the form of telecommunication or other forms.

[0061] The units described above as separate components may or may not be physically separated, and the components shown as units may or may not be physical units, that is, they may be located in one place or distributed on multiple network units. Some or all of the units may be selected according to actual needs to achieve the purpose of the solution of this embodiment.

[0062] The above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit the scope of protection of the invention. Obviously, the described embodiments are only some embodiments of the present invention, rather than all embodiments. Based on these embodiments, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of the present invention. Although the present invention has been described in detail with reference to the above embodiments, ordinary technicians in this field can still combine, add, delete or make other adjustments to the features in the various embodiments of the present invention according to the circumstances without conflict, without making creative work, so as to obtain different other technical solutions that do not deviate from the concept of the present invention in essence, and these technical solutions also belong to the scope of protection of the present invention.

Claims

1. A slide rail aviation obstruction light that is easy to fix, characterized in that: include: A support base, wherein the cross section of the support base is circular; A fixed plate arranged in the middle of the supporting base; The inner side wall of the support base is provided with an annular slide rail, and a slider is slidably matched on the slide rail; The slider and the fixed disk are provided with a same assembly seat, and the assembly seat and the fixed disk are rotationally matched; A driving motor is arranged at the bottom of the fixing plate, and an output end of the driving motor is fixedly connected with an end key of the assembly seat; A feed screw is arranged in the assembly seat, and a nut block is matched with a thread on the feed screw; A lower lamp holder is arranged on the nut block; Guide poles are arranged at the four corners of the upper surface of the lower lamp frame; The same upper lamp bracket is slidably matched on the four guide pillars; A lamp trough which is lower than the horizontal height is provided in the middle of the upper surface of the upper lamp frame; A magnetic pad is provided on the lamp trough; An aviation obstruction light is arranged on the magnetic pad, and a magnetic adsorption layer is arranged at the bottom of the aviation obstruction light; A set of support seats are arranged on both sides of the upper light frame adjacent to the aviation obstruction light; The two supporting seats are provided with arc-shaped supporting grooves with openings facing each other on opposite sides; A plurality of fastening springs are arranged in the two supporting grooves, and a damper is integrated in the fastening springs; A fastening pad is respectively arranged on one side of the fastening springs away from the corresponding supporting groove.

2. The slide rail type aviation obstruction light that is easy to fix as claimed in claim 1, characterized in that: The edges of both sides of the two support seats extend outward to form fastening plates facing each other, and the outer side walls of the fastening plates are provided with press buckles.

3. The slide rail type aviation obstruction light that is easy to fix as claimed in claim 2, characterized in that: It also includes a U-shaped fastening sleeve, and limiting slots are provided on both sides of the fastening sleeve, and the inner diameter of the limiting slots is consistent with the outer diameter of the pressing buckle.

4. The slide rail type aviation obstruction light that is easy to fix as claimed in claim 1, characterized in that: A hydraulic cylinder is arranged in the middle of the upper surface of the lower lamp frame, and the telescopic end of the hydraulic cylinder is connected to the bottom position of the upper lamp frame.

5. The slide rail type aviation obstruction light that is easy to fix as claimed in claim 1, characterized in that: A plurality of reinforced lamp arms are arranged on one side of the fixing plate opposite to the supporting base.

6. The slide rail type aviation obstruction light that is easy to fix as claimed in claim 2, characterized in that: A servo motor is arranged on the end side of the assembly seat, and the output end of the servo motor is fixedly connected with the end key of the feed screw rod.

7. The slide rail type aviation obstruction light that is easy to fix as claimed in claim 6, characterized in that: An extension bracket is arranged on the outer side wall of the assembly seat, a group of solar panels are arranged on the extension bracket; an inverter and a storage battery electrically connected with the solar panels are arranged under the extension bracket.

8. The slide rail type aviation obstruction light that is easy to fix as claimed in claim 1, characterized in that: A limit block is arranged at the top position of the guide column rod.

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