High-strength aviation flash obstruction light

Abstract

The utility model relates to the field of aviation flash obstruction lights, and discloses a high-strength aviation flash obstruction light which comprises an obstruction light body, the bottom of the obstruction light body is fixedly connected with a fixing column, the outer wall of the fixing column is sleeved with a guide column, the bottom of the guide column is fixedly connected with a mounting block, and the mounting block is fixedly connected with the bottom of the obstruction light body. A supporting frame is fixedly connected to the position, close to the outer side of the fixing column, of the bottom of the obstruction light body, a first movable rod is movably connected to the outer wall of the supporting frame, a supporting shaft is fixedly connected to the bottom of the first movable rod, a torsional spring is arranged on the outer wall of the supporting shaft, and a second movable rod is arranged on the outer ring of the torsional spring. According to the high-strength aviation flash obstruction light, the damping function is achieved, so that buffering is facilitated when the high-strength aviation flash obstruction light is vibrated, then the shaking condition is prevented, the using stability is effectively improved, the damage condition caused by collision is effectively prevented through buffering, and then the using strength is improved.

Description

Technical Field

[0001] This utility model relates to the field of aviation flash obstruction light technology, specifically a high-intensity aviation flash obstruction light. Background Technology

[0002] Aviation obstruction lights, also known as navigational lighting equipment, are special lights used to mark obstacles. They belong to the navigational lighting equipment industry, and aviation obstruction lights are a category of lights within it.

[0003] Existing aviation flash obstruction lights lack shock absorption capabilities, making them prone to shaking upon impact, thus reducing stability and increasing the risk of damage, thereby diminishing their durability. Utility Model Content

[0004] (a) Technical problems to be solved

[0005] In view of the shortcomings of the prior art, this utility model provides a high-intensity aviation flashing obstruction light with easy shock absorption function, thus solving the problems in the background art mentioned above.

[0006] (II) Technical Solution

[0007] To achieve the above objectives, this utility model provides the following technical solution: a high-intensity aviation flashing obstruction light, comprising an obstruction light body, a fixed column fixedly connected to the bottom of the obstruction light body, a guide column sleeved on the outer wall of the fixed column, an installation block fixedly connected to the bottom of the guide column, a support frame fixedly connected to the bottom of the obstruction light body near the outer side of the fixed column, a first movable rod movably connected to the outer wall of the support frame, a support shaft fixedly connected to the bottom of the first movable rod, a torsion spring provided on the outer wall of the support shaft, a second movable rod provided on the outer ring of the torsion spring, a movable block fixedly connected to the bottom of the second movable rod, a reinforcing rod fixedly connected to the top of the installation block near the outer side of the guide column, a through groove opened on the inner wall of the reinforcing rod, a shock absorber fixedly connected to the inner wall of the through groove, and a shock-absorbing spring sleeved on the outer wall of the movable end of the shock absorber, thereby realizing the shock absorption function, which is beneficial for buffering when subjected to vibration, thus preventing shaking, effectively improving the stability during use, and through the buffering setting, effectively preventing damage caused by collision, thereby improving the strength of use.

[0008] Furthermore, the fixed column and the guide column form a sliding structure, and the guide column and the mounting block are distributed in a "T" shape. The setting of the guide column facilitates the guidance of the fixed column, thereby preventing the shaking of the obstacle light body to a certain extent.

[0009] Furthermore, the top of the first movable rod is rotatably connected to the support frame, and the first movable rod is distributed in an inclined manner, which facilitates the rotation of the first movable rod.

[0010] Furthermore, the bottom of the first movable rod is rotatably connected to the second movable rod via a support shaft, and the second movable rod forms a rotating structure with the support shaft via a torsion spring. This facilitates the first movable rod to drive the second movable rod to rotate, and the elasticity of the torsion spring helps to perform a certain degree of shock absorption.

[0011] Furthermore, the second movable rod is inclined in the opposite direction to the first movable rod, and the bottom of the second movable rod is rotatably connected to the movable block through a shaft, which facilitates the sliding of the movable block when the second movable rod rotates.

[0012] Furthermore, the movable end of the shock absorber is fixedly connected to the outer wall of the movable block, and the movable block is distributed in a "U" shape, which facilitates the movement of the shock absorber after the movable block slides, thereby absorbing the elastic potential energy of the torsion spring and the damping spring through the shock absorber, further improving the shock absorption effect.

[0013] Furthermore, the movable block is slidably connected to the reinforcing rod through a through groove, and the reinforcing rod is distributed at equal angles along the axial center line of the guide column, which facilitates limiting and guiding the movable block when it slides, and is also beneficial for reinforcing and supporting the guide column.

[0014] Beneficial effects

[0015] Compared with the prior art, this utility model provides a high-intensity aviation flash obstruction light, which has the following beneficial effects:

[0016] 1. This high-intensity aviation flashing obstruction light, through its obstruction light body, fixed column, guide column, mounting block, support frame, first movable rod, support shaft, torsion spring, second movable rod, reinforcing rod, through groove, shock absorber, shock-absorbing spring, and movable block, achieves a shock absorption function, thereby helping to buffer when subjected to vibration, thus preventing shaking and effectively improving stability during use. The buffer setting also effectively prevents damage caused by collisions, thereby improving the strength of use. Attached Figure Description

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

[0018] Figure 2 This utility model Figure 1 Enlarged structural diagram at point A in the middle;

[0019] Figure 3 This is a partial bottom view of the structure of this utility model;

[0020] Figure 4 This is a schematic diagram of the connection structure between the first movable rod and the second movable rod of this utility model.

[0021] In the diagram: 1. Obstruction light body; 2. Fixed column; 3. Guide column; 4. Mounting block; 5. Support frame; 6. First movable rod; 7. Support shaft; 8. Torsion spring; 9. Second movable rod; 10. Reinforcing rod; 11. Through slot; 12. Vibration damper; 13. Vibration damping spring; 14. Movable block. Detailed Implementation

[0022] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0023] Example 1

[0024] A preferred embodiment of the high-intensity aviation flash obstruction light provided by this utility model is, for example... Figures 1 to 4 As shown: A high-intensity aviation flash obstruction light includes an obstruction light body 1. A fixing post 2 is fixedly connected to the bottom of the obstruction light body 1. A guide post 3 is sleeved on the outer wall of the fixing post 2. A mounting block 4 is fixedly connected to the bottom of the guide post 3. A support frame 5 is fixedly connected to the bottom of the obstruction light body 1 near the outer side of the fixing post 2. A first movable rod 6 is movably connected to the outer wall of the support frame 5. A support shaft 7 is fixedly connected to the bottom of the first movable rod 6. A torsion spring 8 is provided on the outer wall of the support shaft 7. A second movable rod 9 is provided on the outer ring of the torsion spring 8. A movable block 14 is fixedly connected to the bottom. A reinforcing rod 10 is fixedly connected to the top of the mounting block 4 near the outer side of the guide post 3. A through groove 11 is opened on the inner wall of the reinforcing rod 10. A shock absorber 12 is fixedly connected to the inner wall of the through groove 11. A shock-absorbing spring 13 is sleeved on the outer wall of the movable end of the shock absorber 12, which realizes the function of shock absorption. This helps to buffer when subjected to vibration, thereby preventing shaking and effectively improving the stability during use. Through the buffer setting, it effectively prevents damage caused by collision, thereby improving the strength of use.

[0025] Furthermore, the fixed post 2 and the guide post 3 form a sliding structure, and the guide post 3 and the mounting block 4 are distributed in a "T" shape. The setting of the guide post 3 facilitates the guidance of the fixed post 2, thereby preventing the shaking of the obstacle light body 1 to a certain extent.

[0026] Furthermore, the top of the first movable rod 6 is rotatably connected to the support frame 5, and the first movable rod 6 is distributed in an inclined manner, which facilitates the rotation of the first movable rod 6.

[0027] Furthermore, the bottom of the first movable rod 6 is rotatably connected to the second movable rod 9 via the support shaft 7, and the second movable rod 9 forms a rotating structure with the support shaft 7 via the torsion spring 8, which facilitates the first movable rod 6 to drive the second movable rod 9 to rotate, and the elasticity of the torsion spring 8 is beneficial for a certain degree of shock absorption.

[0028] Furthermore, the second movable rod 9 is inclined in the opposite direction to the first movable rod 6, and the bottom of the second movable rod 9 is rotatably connected to the movable block 14 through a shaft, which facilitates the sliding of the movable block 14 when the second movable rod 9 rotates.

[0029] Furthermore, the movable end of the shock absorber 12 is fixedly connected to the outer wall of the movable block 14, and the movable block 14 is arranged in a "U" shape, which facilitates the movement of the shock absorber 12 after the movable block 14 slides. In this way, the shock absorber 12 absorbs the elastic potential energy of the torsion spring 8 and the damping spring 13, thereby further improving the shock absorption effect.

[0030] Furthermore, the movable block 14 is slidably connected to the reinforcing rod 10 through the through groove 11, and the reinforcing rod 10 is distributed at equal angles along the axial center line of the guide column 3, which facilitates limiting and guiding the movable block 14 when it slides, and is also beneficial for reinforcing and supporting the guide column 3.

[0031] When the obstacle light body 1 is impacted, the fixed column 2 will slide under the guidance of the guide column 3, causing the support frame 5 to rotate the first movable rod 6. The first movable rod 6 will then rotate the second movable rod 9 in the opposite direction, causing the torsion spring 8 to deform. The elasticity of the torsion spring 8 will provide initial shock absorption. At the same time, after the second movable rod 9 rotates, the movable block 14 will slide inside the reinforcing rod 10 under the guidance of the through groove 11. The movable block 14 will then deform the damping spring 13, causing the movable end of the shock absorber 12 to slide. The shock absorber 12 will absorb the elastic potential energy of the torsion spring 8 and the damping spring 13 through hydraulic pressure, thereby effectively ensuring shock absorption and preventing the obstacle light body 1 from shaking during use. This improves the stability during use, solves the problem of damage caused by impact to the obstacle light body 1, and increases its strength.

[0032] It should be noted that, in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such process, method, article, or apparatus.

[0033] It should be noted that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", and "counterclockwise" indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or component referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.

[0034] Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of this utility model, "a plurality of" means two or more, unless otherwise explicitly specified.

[0035] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A high-intensity aviation flashing obstruction light, comprising an obstruction light body (1), characterized in that: A fixed post (2) is fixedly connected to the bottom of the obstruction light body (1). A guide post (3) is sleeved on the outer wall of the fixed post (2). A mounting block (4) is fixedly connected to the bottom of the guide post (3). A support frame (5) is fixedly connected to the outer side of the bottom of the obstruction light body (1) near the fixed post (2). A first movable rod (6) is movably connected to the outer wall of the support frame (5). A support shaft (7) is fixedly connected to the bottom of the first movable rod (6). The outer side of the support shaft (7) is... A torsion spring (8) is provided on the wall, and a second movable rod (9) is provided on the outer ring of the torsion spring (8). A movable block (14) is fixedly connected to the bottom of the second movable rod (9). A reinforcing rod (10) is fixedly connected to the top of the mounting block (4) near the outer side of the guide post (3). A through groove (11) is provided on the inner wall of the reinforcing rod (10). A shock absorber (12) is fixedly connected to the inner wall of the through groove (11). A shock-absorbing spring (13) is sleeved on the outer wall of the movable end of the shock absorber (12).

2. The high-intensity aviation flash obstruction light according to claim 1, characterized in that: The fixed column (2) and the guide column (3) form a sliding structure, and the guide column (3) and the mounting block (4) are distributed in a "T" shape.

3. A high-intensity aviation flashing obstruction light according to claim 1, characterized in that: The top of the first movable rod (6) is rotatably connected to the support frame (5), and the first movable rod (6) is distributed in an inclined manner.

4. A high-intensity aviation flash obstruction light according to claim 1, characterized in that: The bottom of the first movable rod (6) is rotatably connected to the second movable rod (9) through the support shaft (7), and the second movable rod (9) forms a rotating structure with the support shaft (7) through the torsion spring (8).

5. A high-intensity aviation flashing obstruction light according to claim 1, characterized in that: The second movable rod (9) is inclined in the opposite direction to the first movable rod (6), and the bottom of the second movable rod (9) is rotatably connected to the movable block (14) via a shaft.

6. A high-intensity aviation flash obstruction light according to claim 1, characterized in that: The movable end of the shock absorber (12) is fixedly connected to the outer wall of the movable block (14), and the movable block (14) is distributed in a "U" shape.

7. A high-intensity aviation flashing obstruction light according to claim 1, characterized in that: The movable block (14) is slidably connected to the reinforcing rod (10) through the through groove (11), and the reinforcing rod (10) is distributed at equal angles along the axial center line of the guide column (3).

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