Aviation obstruction light with adjustable light emitting angle

Abstract

The utility model relates to the technical field of aviation obstruction lights, and discloses an aviation obstruction light with adjustable light-emitting angle, including an aviation obstruction light body, the side of the aviation obstruction light body close to the bottom is rotatably connected with a side plate, the bottom of the side plate is fixedly equipped with a bottom plate, the bottom of the bottom plate is provided with a fixing seat, the side of the side plate is fixedly equipped with a motor, and the output shaft of the motor is fixedly sleeved with a rotating shaft. Through the coordinated use of the motor and the rotating shaft, the cylinder is used to drive the card plate to move in a direction away from the gear, and then the motor is used to drive the rotating shaft to rotate, so as to drive the aviation obstruction light body to rotate, and then the aviation obstruction light body is used to drive the gear to rotate through the auxiliary shaft, and then the motor is turned off and the card plate is driven to move up by the cylinder, so as to dock the top of the card plate with the bottom of the gear, thereby assisting the rotation of the aviation obstruction light and assisting the stable limiting of the aviation obstruction light.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation obstruction lights, in particular to an aviation obstruction light with an adjustable light-emitting angle. Background Art

[0002] The function of aviation obstruction lights is to display the outline of structures, so that aircraft operators can judge the height and outline of obstacles and serve as a warning. In order to distinguish them from general-purpose lighting, aviation obstruction lights are not always on but flashing. Low-intensity aviation obstruction lights are always on, while medium-intensity aviation obstruction lights and high-intensity aviation obstruction lights flash.

[0003] During use, traditional aviation obstruction lights are installed on the roof of a residential building using bolts and nuts to install a fixed base. The aviation obstruction lights are then used to flash to assist aircraft in warning. However, traditional aviation obstruction lights are fixed and installed using bolts, and their light direction cannot be adjusted, resulting in the aircraft operator being unable to observe the obstruction lights in time when driving at different angles, thereby affecting the stable flight of the aircraft. In addition, when traditional aviation obstruction lights fail and need to be disassembled and replaced, the bolts and nuts need to be disassembled and installed in the forward and reverse directions, thereby affecting the installation efficiency of the device. Utility Model Content

[0004] In view of the deficiencies of the prior art, the utility model provides an aviation obstruction light with adjustable light-emitting angle to solve the problems raised by the above-mentioned background technology.

[0005] The utility model provides the following technical solution: an aviation obstruction light with adjustable light-emitting angle, comprising an aviation obstruction light body, wherein the side surface of the aviation obstruction light body close to the bottom is rotatably connected with a side plate, the bottom of the side plate is fixedly equipped with a bottom plate, a fixing seat is provided at the bottom of the bottom plate, a motor is fixedly equipped with the side surface of the side plate, an output shaft of the motor is fixedly sleeved with a rotating shaft, and the side surface of the rotating shaft is fixedly assembled with the side surface of the aviation obstruction light body, an auxiliary shaft is fixedly assembled with a side of the aviation obstruction light body away from the rotating shaft, and the outer edge of the auxiliary shaft is rotatably sleeved with the inner wall of the side plate, a gear is fixedly assembled with the side surface of the auxiliary shaft, a slide groove 1 is provided on the inner wall of the bottom plate, a docking tube is fixedly assembled with the top of the bottom plate, a docking plate is slidably sleeved on the inner wall of the slide groove 1, an auxiliary rod is fixedly assembled with the bottom of the docking plate, a limiting plate is fixedly assembled with the bottom of the auxiliary rod, and the outer edge of the limiting plate is slidably sleeved with the auxiliary plate.

[0006] As a preferred technical solution of the utility model, a cylinder is fixedly mounted on the side of the side plate, a clamping plate is fixedly mounted on the output end of the cylinder, and the shape and size of the top of the clamping plate are matched with the shape and size of the convex teeth on the outer edge of the gear.

[0007] As a preferred technical solution of the utility model, a second slide groove is provided at the bottom of the docking tube, a circular groove is provided at the top of the inner wall of the second slide groove, a docking groove is provided at the top of the inner wall of the circular groove, and the shape and size of the inner wall of the docking groove are matched with the shape and size of the outer edge of the docking plate, and the shape and size of the inner wall of the second slide groove are completely consistent with the shape and size of the inner wall of the first slide groove.

[0008] As a preferred technical solution of the utility model, a spring 1 is fixedly connected to the top of the inner wall of the docking tube, a circular plate is fixedly connected to the bottom of the spring 1, and the outer edge of the circular plate is slidably sleeved with the inner wall of the circular groove.

[0009] As a preferred technical solution of the utility model, a through groove is provided at the bottom of the fixed seat, and the inner wall of the through groove is movably connected to the outer edge of the auxiliary rod, and the top of the limit plate is fixedly connected to a spring 2, and the top of the spring 2 is fixedly connected to the bottom of the auxiliary plate.

[0010] As a preferred technical solution of the utility model, a control panel is fixedly mounted on the side of the side panel, and the control panel is electrically connected to the cylinder and the motor.

[0011] Compared with the prior art, the utility model has the following beneficial effects:

[0012] 1. The aviation obstruction light with adjustable luminous angle uses a motor and a rotating shaft to drive the card plate to move away from the gear by using a cylinder, and then the motor drives the rotating shaft to rotate, thereby driving the aviation obstruction light body to rotate by using the rotating shaft, and then the aviation obstruction light body drives the gear to rotate through the auxiliary shaft, and then the motor is turned off and the card plate is driven up by the cylinder, so that the top of the card plate is connected with the bottom of the gear, thereby assisting the rotation of the aviation obstruction light and assisting the stable limit of the aviation obstruction light.

[0013] 2. The aviation obstruction light with adjustable luminous angle is used in conjunction with the docking plate and the docking tube. The auxiliary rod is used to drive the outer edge of the docking plate to pass through the inner wall of the slide groove 1 and the inner wall of the slide groove 2 to the inner wall of the circular groove. Then the auxiliary rod is rotated and the auxiliary rod is released, so that the circular plate is pushed downward by the spring 1, and the outer edge of the docking plate is driven by the circular plate to dock with the inner wall of the docking groove for limiting position, and the auxiliary plate is pushed upward by the spring 2, and then the auxiliary plate and the docking plate are used to assist the bottom plate and the fixing seat to stabilize and limit. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 It is a schematic diagram of the three-dimensional structure of the utility model;

[0015] Figure 2 This is a schematic diagram of the front section structure of the utility model;

[0016] Figure 3This is a schematic diagram of the front section structure of the utility model from another angle;

[0017] Figure 4 For this utility model Figure 3 The enlarged structural diagram at A in the middle;

[0018] Figure 5 It is a schematic diagram of the three-dimensional structure of the card board of the utility model.

[0019] In the figure: 1. Aviation obstruction light body; 2. Side panel; 3. Bottom panel; 4. Motor; 5. Rotating shaft; 6. Auxiliary shaft; 7. Gear; 8. Clamp; 9. Cylinder; 10. Fixed seat; 11. Through slot; 12. Slide slot 1; 13. Slide slot 2; 14. Round slot; 15. Docking slot; 16. Spring 1; 17. Round plate; 18. Docking plate; 19. Auxiliary rod; 20. Limiting plate; 21. Spring 2; 22. Auxiliary plate; 23. Control panel; 24. Docking tube. DETAILED DESCRIPTION

[0020] 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.

[0021] See also Figure 1-Figure 5 The invention discloses an aviation obstruction light with adjustable light-emitting angle, comprising an aviation obstruction light body 1, wherein the side of the aviation obstruction light body 1 close to the bottom thereof is rotatably connected with a side plate 2, the bottom of the side plate 2 is fixedly equipped with a bottom plate 3, the bottom of the bottom plate 3 is provided with a fixing seat 10, the side of the side plate 2 is fixedly equipped with a motor 4, the output shaft of the motor 4 is fixedly sleeved with a rotating shaft 5, and the side of the rotating shaft 5 is fixedly assembled with the side of the aviation obstruction light body 1, the side of the aviation obstruction light body 1 away from the rotating shaft 5 is fixedly equipped with an auxiliary shaft 6, and the outer edge of the auxiliary shaft 6 is rotatably sleeved with the inner wall of the side plate 2, and the side of the auxiliary shaft 6 is fixedly equipped with a rotating shaft 5. It is equipped with a gear 7, a slide groove 12 is provided on the inner wall of the bottom plate 3, a docking tube 24 is fixedly installed on the top of the bottom plate 3, a docking plate 18 is slidably sleeved on the inner wall of the slide groove 12, an auxiliary rod 19 is fixedly installed on the bottom of the docking plate 18, a limit plate 20 is fixedly installed on the bottom of the auxiliary rod 19, an auxiliary plate 22 is slidably sleeved on the outer edge of the limit plate 20, and the fixing seat 10 is the required installation place of the aviation obstruction light body 1, the outer edge of the auxiliary rod 19 is used to assist the fixing seat 10 and the bottom plate 3 to limit, and the auxiliary plate 22 and the docking plate 18 are used to further assist the bottom plate 3 and the fixing seat 10 to stably dock.

[0022] In a preferred embodiment, a cylinder 9 is fixedly mounted on the side of the side panel 2, and a card plate 8 is fixedly mounted on the output end of the cylinder 9, and the shape and size of the top of the card plate 8 are adapted to the shape and size of the convex teeth on the outer edge of the gear 7. By using the cylinder 9 and the card plate 8 in coordination, the cylinder 9 is used to drive the card plate 8 to adjust its height, so that the top of the card plate 8 is connected to the bottom of the gear 7, thereby assisting the gear 7 to drive the aviation obstruction light body 1 to be stably limited.

[0023] In a preferred embodiment, a second slide groove 13 is provided at the bottom of the docking tube 24, a circular groove 14 is provided at the top of the inner wall of the second slide groove 13, a docking groove 15 is provided at the top of the inner wall of the circular groove 14, and the shape and size of the inner wall of the docking groove 15 are adapted to the shape and size of the outer edge of the docking plate 18, and the shape and size of the inner wall of the second slide groove 13 are completely consistent with the shape and size of the inner wall of the first slide groove 12. By the coordinated use of the second slide groove 13 and the circular groove 14, the outer edge of the docking plate 18 is used to pass through the inner wall of the first slide groove 12 and the inner wall of the second slide groove 13 to the inner wall of the circular groove 14, and the outer edge of the docking plate 18 is assisted by rotating the docking plate 18 to limit the docking of the inner wall of the docking groove 15.

[0024] In a preferred embodiment, a spring 16 is fixedly connected to the top of the inner wall of the docking tube 24, a circular plate 17 is fixedly connected to the bottom of the spring 16, and the outer edge of the circular plate 17 is slidably sleeved with the inner wall of the circular groove 14. By using the spring 16 and the circular plate 17 in coordination, the spring 16 is used to push the circular plate 17 downward, and then the bottom of the circular plate 17 is used to push the outer edge of the docking plate 18 and the inner wall of the docking groove 15 to stabilize the docking limit position.

[0025] In a preferred embodiment, a through slot 11 is provided at the bottom of the fixed seat 10, and the inner wall of the through slot 11 is movably connected to the outer edge of the auxiliary rod 19, and the top of the limiting plate 20 is fixedly connected with a spring 21, and the top of the spring 21 is fixedly connected to the bottom of the auxiliary plate 22. By opening the through slot 11, the diameter of the inner wall of the through slot 11 is a, and the diameter of the inner wall of the slide groove 12 is b, and a>b, thereby ensuring that the outer edge of the docking plate 18 stably passes through the inner wall of the through slot 11 to the inner wall of the slide groove 12, and the spring 21 is used to drive the top of the auxiliary plate 22 and the bottom of the fixed seat 10 to limit.

[0026] In a preferred embodiment, a control panel 23 is fixedly mounted on the side of the side panel 2, and the control panel 23 is electrically connected to the cylinder 9 and the motor 4. By installing the control panel 23, the control panel 23 is utilized to assist in the stable operation of the internal components of the control device.

[0027] Working principle: when the device is in use, the cylinder 9 is used to drive the card plate 8 to move in the direction away from the gear 7, and then the motor 4 is used to drive the rotating shaft 5 to rotate, so that the rotating shaft 5 drives the aviation obstruction light body 1 to rotate, and then the aviation obstruction light body 1 drives the gear 7 to rotate through the auxiliary shaft 6, and then the motor 4 is turned off and the cylinder 9 is used to drive the card plate 8 to move up, so that the top of the card plate 8 is connected with the bottom of the gear 7, thereby assisting the rotation of the aviation obstruction light body 1 and assisting the aviation obstruction light body 1 to stabilize the limit, and the auxiliary rod 19 is used to drive the outer edge of the docking plate 18 through the inner wall of the slide groove 12 and the inner wall of the slide groove 2 13 to the inner wall of the circular groove 14, and then the auxiliary rod 19 is rotated and the auxiliary rod 19 is released, so that the spring 16 is used to push the circular plate 17 downward, and the circular plate 17 is used to drive the outer edge of the docking plate 18 to dock and limit with the inner wall of the docking groove 15, and the spring 21 is used to push the auxiliary plate 22 upward, and then the auxiliary plate 22 and the docking plate 18 assist the bottom plate 3 and the fixing seat 10 to stabilize the limit.

[0028] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An aviation obstruction light with adjustable light-emitting angle, comprising an aviation obstruction light body (1), characterized in that: The side of the aviation obstruction light body (1) close to the bottom is rotatably connected to a side plate (2), the bottom of the side plate (2) is fixedly mounted with a bottom plate (3), the bottom of the bottom plate (3) is provided with a fixing seat (10), the side of the side plate (2) is fixedly mounted with a motor (4), the output shaft of the motor (4) is fixedly sleeved with a rotating shaft (5), and the side of the rotating shaft (5) is fixedly mounted with the side of the aviation obstruction light body (1), and the side of the aviation obstruction light body (1) away from the rotating shaft (5) is fixedly mounted with an auxiliary shaft (6), and the auxiliary shaft (6) is fixedly mounted on the side of the aviation obstruction light body (1). ) is rotatably sleeved with the inner wall of the side plate (2), the side of the auxiliary shaft (6) is fixedly equipped with a gear (7), the inner wall of the bottom plate (3) is provided with a slide groove (12), the top of the bottom plate (3) is fixedly equipped with a docking tube (24), the inner wall of the slide groove (12) is slidably sleeved with a docking plate (18), the bottom of the docking plate (18) is fixedly equipped with an auxiliary rod (19), the bottom of the auxiliary rod (19) is fixedly equipped with a limit plate (20), and the outer edge of the limit plate (20) is slidably sleeved with an auxiliary plate (22).

2. The aviation obstruction light with adjustable light-emitting angle according to claim 1, characterized in that: A cylinder (9) is fixedly mounted on the side of the side plate (2), and a clamping plate (8) is fixedly mounted on the output end of the cylinder (9), and the shape and size of the top of the clamping plate (8) are compatible with the shape and size of the outer convex teeth of the gear (7).

3. The aviation obstruction light with adjustable light-emitting angle according to claim 1, characterized in that: The bottom of the docking tube (24) is provided with a second slide groove (13), the top of the inner wall of the second slide groove (13) is provided with a circular groove (14), the top of the inner wall of the circular groove (14) is provided with a docking groove (15), and the shape and size of the inner wall of the docking groove (15) are adapted to the shape and size of the outer edge of the docking plate (18), and the shape and size of the inner wall of the second slide groove (13) are completely consistent with the shape and size of the inner wall of the first slide groove (12).

4. The aviation obstruction light with adjustable light-emitting angle according to claim 1, characterized in that: The top of the inner wall of the docking tube (24) is fixedly connected to a spring 1 (16), the bottom of the spring 1 (16) is fixedly connected to a circular plate (17), and the outer edge of the circular plate (17) is slidably sleeved with the inner wall of the circular groove (14).

5. The aviation obstruction light with adjustable light-emitting angle according to claim 1, characterized in that: A through slot (11) is provided at the bottom of the fixing seat (10), and the inner wall of the through slot (11) is movably sleeved with the outer edge of the auxiliary rod (19); a second spring (21) is fixedly connected to the top of the limiting plate (20), and the top of the second spring (21) is fixedly connected to the bottom of the auxiliary plate (22).

6. The aviation obstruction light with adjustable light-emitting angle according to claim 1, characterized in that: A control panel (23) is fixedly mounted on the side of the side panel (2), and the control panel (23) is electrically connected to the cylinder (9) and the motor (4).

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