Aviation obstruction beacon device

By designing the combination structure of the plug-in rod and fixing sleeve of the aviation obstacle light device, and using the clamping mechanism of the limit block and the fastening block, the time-consuming and labor-intensive installation and disassembly of the aviation obstacle light in the prior art is solved, and rapid installation and disassembly are achieved, and maintenance efficiency is improved.

CN222849148UActive Publication Date: 2025-05-09SANYA AVIATION TOURISM VOCATIONAL COLLEGE
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Patent Information

Application Number
CN202421606920.3
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-07-09
Publication Date
2025-05-09
Estimated Expiration
2034-07-09

AI Technical Summary

Technical Problem

The installation and disassembly of existing aviation obstacle lights is time-consuming and laborious, and later disassembly takes a certain amount of time, which delays the maintenance.

Method used

An aviation obstacle light device is designed, adopting a combined structure of a plug-in rod and a fixing sleeve. It can quickly install and disassemble through the clamping mechanism of the limit block and the fastening block, and use the role of the spring and limit plate to achieve rapid diffusion and contraction of the fastening block, which facilitates the insertion and removal of the limit block.

Benefits of technology

It realizes rapid installation and disassembly of aviation obstacle lights, saves installation and disassembly time, and improves maintenance efficiency.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of aviation obstruction lights, and discloses an aviation obstruction light device which comprises a light body, an inserting mechanism is installed at the bottom of the light body, a fixing mechanism is installed at the bottom of the inserting mechanism, and a fixing block is fixedly connected to the outer side of the fixing mechanism. According to the aviation obstruction beacon device, through the arranged fixing mechanism, in the practical process, an inserting rod is directly inserted into a fixing sleeve, at the moment, clamping connection is conducted through a limiting block and a fastening block at the bottom of the fixing sleeve, rapid installation of the whole beacon body can be achieved, and during later-period disassembling, the whole beacon body only needs to be pulled out of the fixing sleeve forcibly; and the inserting rod with a certain length has elasticity, so that clamping and separation between the limiting block at the bottom of the inserting rod and the fastening block are facilitated, and the problems that time and labor are wasted in the mounting mode, a certain time is needed in the later dismounting process, and the maintenance effort is delayed can be effectively solved.
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Description

Technical Field

[0001] The utility model relates to the technical field of aviation obstruction lights, in particular to an aviation obstruction light device. Background Art

[0002] Aviation obstruction lights, also known as navigation lighting equipment or aviation warning lights, are special lamps used to mark obstacles. They are mainly used to provide aviation safety signs at night and in low visibility conditions to prevent aircraft from colliding with buildings, structures or other tall structures.

[0003] At present, in the process of installing aviation obstruction lights, bolts are mostly reserved on cement or hard ground, or holes are drilled, and the aviation obstruction lights are installed by expansion screws and nuts. This installation method is time-consuming and labor-intensive. At the same time, it takes a certain amount of time to disassemble in the later stage, which delays the maintenance work, so it needs to be improved. Utility Model Content

[0004] The purpose of the utility model is to provide an aviation obstruction light device to solve the problems raised in the above background technology.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an aviation obstruction light device, comprising a lamp body, a plug-in mechanism is installed at the bottom of the lamp body, a fixing mechanism is installed at the bottom of the plug-in mechanism, and a fixing block is fixedly connected to the outside of the fixing mechanism;

[0006] The plug-in mechanism comprises a fixed plate, the fixed plate is fixedly connected to the bottom of the lamp body, a plug-in rod is fixedly connected to the middle of the bottom of the fixed plate, and the bottom end of the plug-in rod is fixedly connected to a limit block;

[0007] The fixing mechanism includes a fixing sleeve, which is sleeved on the outside of the plug-in rod, a mounting seat is fixedly connected to the bottom of the fixing sleeve, a second supporting block is fixedly connected to the inside of the mounting seat, a limiting rod is slidably connected in the middle of the second supporting block, a fastening block is fixedly connected to the inner end of the limiting rod, an outer wall of the limiting rod is fixedly connected to the limiting plate on the outside of the second supporting block, a spring is sleeved on the outer wall of the limiting rod on the outside of the limiting plate, and a first supporting block is fixedly connected to the inner side of the mounting seat near the outer end of the limiting rod.

[0008] Preferably, the plug-in rods are arranged in a circle at equal intervals on the bottom of the fixed plate, and the plug-in rods and the limit blocks are distributed at right angles to each other.

[0009] Preferably, the plug-in rods are arranged in a circle at equal intervals and have intervals between them, and the plug-in rods arranged in a circle are arranged in an inner circle of the fixing sleeve.

[0010] Preferably, the limit blocks are arranged at the bottom of the fastening blocks, and the fastening blocks are arranged and distributed at equal intervals corresponding to the limit blocks.

[0011] Preferably, a sliding hole is provided in the middle of the first support block corresponding to the limiting rod, and the first support block is slidably connected to the limiting rod near the outer end through the sliding hole.

[0012] Preferably, a protective shell is fixedly connected to the outer wall of the fixing sleeve, and the protective shell wraps the entire bottom of the fixing sleeve.

[0013] Compared with the prior art, the utility model provides an aviation obstruction light device, which has the following beneficial effects:

[0014] 1. The aviation obstruction light device, through the setting of the fixing mechanism, in the practical process, directly plugs the plug-in rod into the fixing sleeve, at this time, the limit block and the fastening block at the bottom of the fixing sleeve are clamped, so that the whole lamp body can be quickly installed. When disassembling later, it is only necessary to pull the whole lamp body out of the fixing sleeve with force. The plug-in rod with a certain length itself has elasticity to facilitate the clamping and disengagement between the limit block at the bottom of the plug-in rod and the fastening block, which can effectively solve the problem that this installation method is time-consuming and labor-intensive, and at the same time, a certain amount of time is required in the later disassembly process, delaying the maintenance work.

[0015] 2. The aviation obstruction light device has a fixing mechanism. When the plug-in rod is inserted into the fixing sleeve, the fastening block spreads to the surroundings under the action of the spring and the limiting plate during the contact between the limit block and the fastening block. When the limit block moves to the bottom of the fastening block, the fastening block is further connected to the bottom of the limit block under the action of the spring. On the contrary, when the limit block is to be separated from the fastening block, due to the action of the spring, the fastening block will spread to the surroundings after receiving a certain force, which is convenient for the separation of the limit block, can achieve a quick plug-in and pull-out effect, and further achieve a good installation and disassembly purpose. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the following briefly introduces the drawings required for use in the description of the embodiments. Obviously, the drawings described below are only some embodiments of the present invention. For those skilled in the art, other drawings can be obtained based on these drawings without creative labor:

[0017] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0018] Figure 2 It is a schematic cross-sectional view of the overall structure of the utility model;

[0019] Figure 3 This is a schematic diagram of the lamp body and the plug-in mechanism;

[0020] Figure 4 Schematic diagram of the separation of the fixing mechanism.

[0021] In the figure: 1. lamp body; 2. fixing mechanism; 21. fixing sleeve; 22. first support block; 23. limiting rod; 24. limiting plate; 25. fastening block; 26. spring; 27. mounting seat; 28. second support block; 29. ​​protective shell; 3. fixing block; 4. plug-in mechanism; 41. fixing plate; 42. plug-in rod; 43. limiting block. DETAILED DESCRIPTION

[0022] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0023] In the present invention, unless otherwise clearly specified and limited, the terms "install", "connect", "connect", "fix" and the like should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between two elements. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0024] The utility model provides the following technical solutions:

[0025] Embodiment 1

[0026] See also Figure 1-4 An aviation obstruction light device comprises a lamp body 1, a plug-in mechanism 4 is installed at the bottom of the lamp body 1, a fixing mechanism 2 is installed at the bottom of the plug-in mechanism 4, and a fixing block 3 is fixedly connected to the outer side of the fixing mechanism 2;

[0027] The plug-in mechanism 4 includes a fixing plate 41, which is fixedly connected to the bottom of the lamp body 1, a plug-in rod 42 is fixedly connected to the middle of the bottom of the fixing plate 41, and a limit block 43 is fixedly connected to the bottom end of the plug-in rod 42;

[0028] Through the setting of the fixing mechanism 2, in practical use, the plug-in rod 42 is directly plugged into the fixing sleeve 21. At this time, the limiting block 43 and the fastening block 25 at the bottom of the fixing sleeve 21 are clamped, so that the entire lamp body 1 can be quickly installed. When disassembling later, it is only necessary to pull the entire lamp body 1 out of the fixing sleeve 21 with force. The plug-in rod 42 with a certain length itself has elasticity to facilitate the clamping and disengagement between the limiting block 43 at the bottom of the plug-in rod 42 and the fastening block 25, which can effectively solve the problem that this installation method is time-consuming and labor-intensive, and at the same time, a certain amount of time is required in the later disassembly process, which delays the maintenance work.

[0029] The fixing mechanism 2 includes a fixing sleeve 21, which is sleeved on the outside of the plug-in rod 42. A mounting seat 27 is fixedly connected to the bottom of the fixing sleeve 21. A second support block 28 is fixedly connected to the inner side of the mounting seat 27. A limiting rod 23 is slidably connected in the middle of the second support block 28. A fastening block 25 is fixedly connected to the inner end of the limiting rod 23. The outer wall of the limiting rod 23 is fixedly connected to the outer side of the second support block 28. A spring 26 is sleeved on the outer wall of the limiting rod 23 on the outer side of the limiting plate 24. The first support block 22 is fixedly connected to the inner side of the mounting seat 27 near the outer end of the limiting rod 23.

[0030] Through the provided fixing mechanism 2, when the plug-in rod 42 is inserted into the fixing sleeve 21, during the contact between the limit block 43 and the fastening block 25, under the action of the spring 26 and the limit plate 24, the fastening block 25 spreads out to the surroundings, and when the limit block 43 moves to the bottom of the fastening block 25, further under the action of the spring 26, the fastening block 25 is clamped to the bottom of the limit block 43, on the contrary, when the limit block 43 is to be separated from the fastening block 25, due to the action of the spring 26, the fastening block 25 will spread out to the surroundings after receiving a certain force, which is convenient for the separation of the limit block 43, and can achieve a quick plug-in and pull-out effect, and further achieve a good installation and disassembly purpose.

[0031] The plugging rods 42 are arranged in a circle at equal intervals at the bottom of the fixing plate 41, and the plugging rods 42 and the limiting blocks 43 are arranged at right angles to each other.

[0032] The plug-in rods 42 are arranged in a circle at equal intervals and are spaced apart from each other. The plug-in rods 42 arranged in a circle are arranged in the inner circle of the fixing sleeve 21 .

[0033] Embodiment 2

[0034] See also Figure 4 On the basis of the first embodiment, it is further obtained that the limit block 43 is arranged at the bottom of the fastening block 25, and the fastening blocks 25 are arranged and distributed at equal intervals corresponding to the limit blocks 43.

[0035] A sliding hole is provided in the middle of the first support block 22 corresponding to the limiting rod 23 , and the first support block 22 is slidably connected to the limiting rod 23 near the outer end through the sliding hole.

[0036] A protective shell 29 is fixedly connected to the outer wall of the fixing sleeve 21 , and the protective shell 29 wraps the entire bottom of the fixing sleeve 21 .

[0037] In actual operation, when this device is used, in practical use, the plug-in rod 42 is directly plugged into the fixing sleeve 21. At this time, the limiting block 43 and the fastening block 25 at the bottom of the fixing sleeve 21 are clamped, so that the entire lamp body 1 can be quickly installed. When disassembling later, it is only necessary to pull the entire lamp body 1 out of the fixing sleeve 21 with force. The plug-in rod 42 with a certain length itself has elasticity to facilitate the clamping and disengagement between the limiting block 43 at the bottom of the plug-in rod 42 and the fastening block 25, which can effectively solve the problem that this installation method is time-consuming and labor-intensive, and at the same time, a certain amount of time is required in the later disassembly process, which delays the maintenance effort.

[0038] When the connecting rod 42 is inserted into the fixing sleeve 21, during the contact between the limit block 43 and the fastening block 25, under the action of the spring 26 and the limit plate 24, the fastening block 25 spreads out to the surroundings. When the limit block 43 moves to the bottom of the fastening block 25, further under the action of the spring 26, the fastening block 25 is clamped to the bottom of the limit block 43. On the contrary, when the limit block 43 is about to be separated from the fastening block 25, due to the action of the spring 26, the fastening block 25 will spread out to the surroundings after receiving a certain force, which is convenient for the separation of the limit block 43, and can achieve a quick plug-in and pull-out effect, and further achieve a good installation and disassembly purpose.

[0039] It should be noted that, in this article, relational terms such as first and second, etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device. In the absence of further restrictions, the elements defined by the statement "comprise a ..." do not exclude the presence of other identical elements in the process, method, article or device including the elements.

Claims

1. An aviation obstruction light device, comprising a light body (1), characterized in that: A plug-in mechanism (4) is installed at the bottom of the lamp body (1), a fixing mechanism (2) is installed at the bottom of the plug-in mechanism (4), and a fixing block (3) is fixedly connected to the outside of the fixing mechanism (2); The plug-in mechanism (4) comprises a fixing plate (41), the fixing plate (41) is fixedly connected to the bottom of the lamp body (1), a plug-in rod (42) is fixedly connected to the middle of the bottom of the fixing plate (41), and the bottom end of the plug-in rod (42) is fixedly connected to a limiting block (43); The fixing mechanism (2) comprises a fixing sleeve (21), the fixing sleeve (21) being sleeved on the outside of the plug-in rod (42), the fixing sleeve (21) being fixedly connected to a mounting seat (27) at the bottom, the mounting seat (27) being fixedly connected to a second support block (28) at the inside, a limiting rod (23) being slidably connected in the middle of the second support block (28), a fastening block (25) being fixedly connected to the inner end of the limiting rod (23), an outer wall of the limiting rod (23) being fixedly connected to a limiting plate (24) at the outside of the second support block (28), a spring (26) being sleeved on the outer side of the limiting plate (24) at the outer wall of the limiting rod (23), and a first support block (22) being fixedly connected to the inner side of the mounting seat (27) near the outer end of the limiting rod (23).

2. An aviation obstruction light device according to claim 1, characterized in that: The plugging rods (42) are arranged in a circle at equal intervals at the bottom of the fixed plate (41), and the plugging rods (42) and the limiting blocks (43) are arranged at right angles to each other.

3. The aviation obstruction light device according to claim 1, characterized in that: The plug-in rods (42) are arranged in a circle at equal intervals and are spaced apart from each other. The plug-in rods (42) arranged in a circle are arranged in the inner circle of the fixing sleeve (21).

4. The aviation obstruction light device according to claim 1, characterized in that: The limit blocks (43) are arranged at the bottom of the fastening blocks (25), and the fastening blocks (25) are arranged and distributed at equal intervals corresponding to the limit blocks (43).

5. The aviation obstruction light device according to claim 1, characterized in that: A sliding hole is provided in the middle of the first support block (22) corresponding to the limiting rod (23), and the first support block (22) is slidably connected to the limiting rod (23) near the outer end through the sliding hole.

6. The aviation obstruction light device according to claim 1, characterized in that: The outer wall of the fixing sleeve (21) is fixedly connected to a protective shell (29), and the protective shell (29) wraps the entire bottom of the fixing sleeve (21).