Hand-held LED aviation obstruction beacon

Abstract

The utility model discloses a hand-held LED aviation obstruction beacon, and relates to the technical field of aviation obstruction beacons. The handheld LED aviation obstruction beacon comprises a bottom plate, a mounting column is fixedly connected to the upper surface of the bottom plate, a movable ball is fixedly connected to the upper end of the mounting column, a mounting base is arranged above the mounting column, a movable groove matched with the movable ball is formed in the lower surface of the mounting base, and a fault lamp is fixedly connected to the upper surface of the mounting base. An adjusting assembly is arranged on the lower surface of the mounting base and comprises two mounting plates which are fixedly connected to the lower surface of the mounting base, connecting rods are rotationally connected to the surfaces of the close sides of the two mounting plates, and sliding grooves are formed in the outer surface of the mounting base. The fault lamp can be adjusted at will only by unlocking the fault lamp through the control assembly, adjustment is convenient, angle limitation is avoided, and then the application range of the fault lamp is widened.

Description

Technical Field

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

[0002] Aviation obstruction lights, also known as navigation lighting equipment, are special lights that mark obstacles and belong to the navigation lighting equipment industry. 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 and high-intensity aviation obstruction lights flash, with a flashing frequency of no less than 20 times per minute and no more than 60 times per minute. The 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.

[0003] However, in the prior art, most aviation fault lights are fixedly installed and the angle cannot be adjusted, which requires additional work when installing on walls with different slopes, thereby increasing the difficulty of installing aviation fault lights and simultaneously reducing the installation efficiency of aviation fault lights. In view of this, we propose a portable LED aviation obstruction light. Utility Model Content

[0004] The purpose of the utility model is to solve at least one of the technical problems existing in the prior art and to provide a portable LED aviation obstruction light that can solve the problem that the angle of aviation fault lights cannot be adjusted, which increases the difficulty of installation in some situations.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a portable LED aviation obstruction light, comprising a base plate, a mounting column fixedly connected to the upper surface of the base plate, a movable ball fixedly connected to the upper end of the mounting column, a mounting seat arranged above the mounting column, a movable groove matched with the movable ball is provided on the lower surface of the mounting seat, a fault light is fixedly connected to the upper surface of the mounting seat, an adjustment component is provided on the lower surface of the mounting seat, the adjustment component comprises two mounting plates, both of which are fixedly connected to the lower surface of the mounting seat, a connecting rod is rotatably connected to the adjacent side surfaces of the two mounting plates, a sliding groove is provided on the outer surface of the mounting seat, a first telescopic rod is slidably connected to the inside of the sliding groove, a second mounting plate is provided on the outer surface of the mounting column, the first telescopic rod is fixedly connected to the second mounting plate, and a control component is provided on the outer surface of the mounting column.

[0006] Preferably, a side surface of the second mounting plate away from the first telescopic rod is also fixedly connected to two mounting plates, the other end of the connecting rod is rotatably connected to a side surface of the two lower mounting plates that are close to each other, the internal sliding sleeve of the first telescopic rod is provided with a second telescopic rod, a cavity is opened inside the mounting column, the sliding groove is communicated with the interior of the cavity, the other end of the second telescopic rod extends into the interior of the cavity, a spring is fixedly connected between the first telescopic rod and the second telescopic rod, and the other end of the second telescopic rod is fixedly connected to a locking plate.

[0007] Preferably, the control assembly includes a knob, which is rotatably connected to the outer surface of the mounting column, a worm is fixedly connected to the left surface of the knob, a second cavity is opened inside the mounting column, and the worm rotatably penetrates into the interior of the second cavity.

[0008] Preferably, the bottom wall of the second cavity is rotatably connected to a rotating rod, and the upper end of the rotating rod rotates and penetrates into the interior of the cavity.

[0009] Preferably, a plum blossom column is fixedly connected to the upper end of the rotating rod, and the plum blossom column is arranged in a cross shape as a whole. A worm gear is sleeved on the outer surface of the rotating rod, and the outer surface of the worm gear is meshingly connected with the outer surface of the worm.

[0010] Preferably, a storage groove is provided on the lower surface of the bottom plate, and a handle is rotatably connected to the inner wall of the storage groove.

[0011] Compared with the prior art, the beneficial effects of the utility model are:

[0012] (1) When the angle of the fault light of the portable LED aviation obstruction light needs to be adjusted, the adjustment component is unlocked through the control component, and then the angle of the fault light is manually adjusted directly. When the fault light changes its angle, the movable groove and the movable ball limit and support it. When the angle of the fault light changes, the connecting rod will synchronously drive the second mounting plate to move, so that the second mounting plate can cooperate with the connecting rod to support the fault light at any angle. Through the above structure, when the installation angle of the fault light needs to be adjusted, it only needs to be unlocked by using the control component, and it can be adjusted at will. Not only is the adjustment more convenient, but there is no angle limitation, thereby improving the application range of the fault light.

[0013] (2) In the portable LED aviation obstruction light, after the locking plate is squeezed, the force is transmitted to the second telescopic rod. The second telescopic rod is retracted into the first telescopic rod and the spring is compressed. The locking plate is locked after contacting the inner wall of the cavity. At the same time, when moving the fault light, the handle at the bottom can be used for easy picking. Through the above structure, not only can the angle of the fault light be adjusted at will, but the handle can also be used to facilitate the staff to move the fault light, thereby improving the overall convenience. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] The present invention is further described below with reference to the accompanying drawings and embodiments:

[0015] Figure 1 This is a schematic diagram of the structure of a portable LED aviation obstruction light of the utility model;

[0016] Figure 2 This is a schematic diagram of the activity ball of the utility model;

[0017] Figure 3 This is a cross-sectional schematic diagram of the installation column of the utility model;

[0018] Figure 4 This is a cross-sectional schematic diagram of a first telescopic rod of the utility model;

[0019] Figure 5 for Figure 3 Enlarged view of point A in the middle.

[0020] Figure numerals: 1. base plate; 2. mounting column; 3. movable ball; 4. mounting seat; 5. movable slot; 6. fault light; 7. mounting plate; 8. connecting rod; 9. sliding slot; 10. first telescopic rod; 11. second mounting plate; 12. second telescopic rod; 13. cavity; 14. locking plate; 15. knob; 16. worm; 17. second cavity; 18. rotating rod; 19. plum blossom column; 20. worm gear; 21. storage slot; 22. handle. DETAILED DESCRIPTION

[0021] This section will describe in detail the specific embodiments of the utility model. The preferred embodiments of the utility model are shown in the accompanying drawings. The purpose of the accompanying drawings is to supplement the description of the text part of the specification with graphics, so that people can intuitively and vividly understand each technical feature and the overall technical solution of the utility model, but it cannot be understood as a limitation on the protection scope of the utility model.

[0022] See also Figure 1-5The utility model provides a technical solution: a portable LED aviation obstruction light, comprising a base plate 1, a mounting column 2 is fixedly connected to the upper surface of the base plate 1, a movable ball 3 is fixedly connected to the upper end of the mounting column 2, a mounting seat 4 is arranged above the mounting column 2, a movable groove 5 adapted to the movable ball 3 is provided on the lower surface of the mounting seat 4, a fault light 6 is fixedly connected to the upper surface of the mounting seat 4, an adjustment component is arranged on the lower surface of the mounting seat 4, the adjustment component comprises two mounting plates 7, both of which are fixedly connected to the lower surface of the mounting seat 4, a connecting rod 8 is rotatably connected to the adjacent side surfaces of the two mounting plates 7, a sliding groove 9 is provided on the outer surface of the mounting seat 4, a first telescopic rod 10 is slidably connected to the inner part of the sliding groove 9, a second mounting plate 11 is arranged on the outer surface of the mounting column 2, and the first telescopic rod 10 is It is fixedly connected to the second mounting plate 11, and a control component is provided on the outer surface of the mounting column 2. When the angle of the fault light 6 needs to be adjusted, the adjustment component is unlocked through the control component, and then the angle of the fault light 6 is manually adjusted directly. When the fault light 6 changes its angle, it is limited and supported by the movable groove 5 and the movable ball 3. When the angle of the fault light 6 changes, the connecting rod 8 is synchronously used to drive the second mounting plate 11 to move, so that the second mounting plate 11 can cooperate with the connecting rod 8 to support the fault light 6 at any angle. Through the above structure, when the installation angle of the fault light 6 needs to be adjusted, it only needs to be unlocked by using the control component, and it can be adjusted at will. Not only is the adjustment more convenient, but there is also no angle limitation, thereby improving the application range of the fault light 6.

[0023] Furthermore, a side surface of the second mounting plate 11 away from the first telescopic rod 10 is also fixedly connected to two mounting plates 7, and the other end of the connecting rod 8 is rotatably connected to a side surface of the two mounting plates 7 below. The first telescopic rod 10 is internally slidably sleeved with a second telescopic rod 12, and a cavity 13 is provided inside the mounting column 2, and the sliding groove 9 is communicated with the interior of the cavity 13. The other end of the second telescopic rod 12 extends into the interior of the cavity 13, and a spring is fixedly connected between the first telescopic rod 10 and the second telescopic rod 12. The other end of the second telescopic rod 12 is fixedly connected to a locking plate 14. The control component includes a knob 15, which is rotatably connected to the outer surface of the mounting column 2, and a worm 16 is fixedly connected to the left surface of the knob 15. A second cavity 17 is provided inside the mounting column 2, and the worm 16 rotates and penetrates into the interior of the second cavity 17. The bottom wall of the second cavity 17 is rotatably connected to a rotating rod 18, and the upper end of the rotating rod 18 rotates and penetrates into the interior of the cavity 13, and the upper end of the rotating rod 18 is fixedly connected to the plum blossom column 1 9, the plum blossom column 19 is set in a cross shape as a whole, the outer surface of the rotating rod 18 is sleeved with a worm wheel 20, the outer surface of the worm wheel 20 is meshed with the outer surface of the worm 16, the lower surface of the bottom plate 1 is provided with a storage groove 21, the inner wall of the storage groove 21 is rotatably connected with a handle 22, the worm 16 is synchronously driven to rotate by rotating the knob 15, the worm 16 is synchronously driven to rotate by the worm wheel 20 after the worm 16 rotates, the rotating rod 18 is synchronously driven to rotate by the worm wheel 20 after the rotating rod 18 rotates, the plum blossom column 19 is synchronously driven to rotate after the rotating rod 18 rotates, and the plum blossom column 19 is rotated by its cross The U-shaped protrusion squeezes the locking plate 14, and the locking plate 14 transmits the force to the second telescopic rod 12 after being squeezed. The second telescopic rod 12 is retracted into the first telescopic rod 10 and the spring is compressed. The locking plate 14 is locked after contacting the inner wall of the cavity 13. At the same time, when moving the fault light, the handle 22 at the bottom can be used for easy picking. Through the above structure, not only the angle of the fault light 6 can be adjusted at will, but also the handle 22 can be used to facilitate the staff to move the fault light 6, thereby improving the overall convenience.

[0024] Working principle: when it is necessary to adjust the angle of the fault light 6, the adjustment component is unlocked through the control component, and then the angle of the fault light 6 is directly adjusted manually. When the fault light 6 changes its angle, it is limited and supported by the movable groove 5 and the movable ball 3. When the angle of the fault light 6 changes, the connecting rod 8 is synchronously used to drive the second mounting plate 11 to move, so that the second mounting plate 11 can cooperate with the connecting rod 8 to support the fault light 6 at any angle, and the worm 16 is synchronously driven to rotate by turning the knob 15. After the worm 16 rotates, the rotating rod 18 is synchronously driven to rotate by the worm gear 20. After the rotating rod 18 rotates, the plum blossom column 19 is synchronously driven to rotate. After the plum blossom column 19 rotates, its cross-shaped protrusion is used to squeeze the locking plate 14. After the locking plate 14 is squeezed, the force is transmitted to the second telescopic rod 12. The second telescopic rod 12 is retracted into the first telescopic rod 10 and the spring is compressed. The locking plate 14 is locked after contacting the inner wall of the cavity 13. At the same time, when moving the fault light, it can be easily taken through the handle 22 at the bottom.

[0025] The embodiments of the present invention are described in detail above in conjunction with the accompanying drawings, but the present invention is not limited to the above embodiments. Various changes can be made within the knowledge scope of ordinary technicians in the technical field without departing from the purpose of the present invention.

Claims

1. A portable LED aviation obstruction light, comprising a base plate (1), characterized in that: The upper surface of the base plate (1) is fixedly connected with a mounting column (2), the upper end of the mounting column (2) is fixedly connected with a movable ball (3), a mounting seat (4) is arranged above the mounting column (2), the lower surface of the mounting seat (4) is provided with a movable groove (5) adapted to the movable ball (3), the upper surface of the mounting seat (4) is fixedly connected with a fault light (6), the lower surface of the mounting seat (4) is provided with an adjustment component, the adjustment component comprises two mounting plates (7), both of which are fixedly connected to the lower surface of the mounting seat (4), the adjacent side surfaces of the two mounting plates (7) are rotatably connected with a connecting rod (8), the outer surface of the mounting seat (4) is provided with a sliding groove (9), the interior of the sliding groove (9) is slidably connected with a first telescopic rod (10), the outer surface of the mounting column (2) is provided with a second mounting plate (11), the first telescopic rod (10) is fixedly connected to the second mounting plate (11), and the outer surface of the mounting column (2) is provided with a control component.

2. A portable LED aviation obstruction light according to claim 1, characterized in that: The second mounting plate (11) is also fixedly connected to two mounting plates (7) on a side surface away from the first telescopic rod (10); the other end of the connecting rod (8) is rotatably connected to a side surface of the two mounting plates (7) below that is close to each other; the first telescopic rod (10) is internally slidably sleeved with a second telescopic rod (12); a cavity (13) is provided inside the mounting column (2); the sliding groove (9) is communicated with the inside of the cavity (13); the other end of the second telescopic rod (12) extends into the inside of the cavity (13); a spring is fixedly connected between the first telescopic rod (10) and the second telescopic rod (12); and the other end of the second telescopic rod (12) is fixedly connected to a locking plate (14).

3. A portable LED aviation obstruction light according to claim 1, characterized in that: The control assembly comprises a knob (15), the knob (15) is rotatably connected to the outer surface of the mounting column (2), a worm (16) is fixedly connected to the left surface of the knob (15), a second cavity (17) is provided inside the mounting column (2), and the worm (16) rotatably penetrates into the interior of the second cavity (17).

4. A portable LED aviation obstruction light according to claim 3, characterized in that: The bottom wall of the second cavity (17) is rotatably connected to a rotating rod (18), and the upper end of the rotating rod (18) rotates and penetrates into the interior of the cavity (13).

5. A portable LED aviation obstruction light according to claim 4, characterized in that: The upper end of the rotating rod (18) is fixedly connected with a plum blossom column (19), which is arranged in a cross shape as a whole. The outer surface of the rotating rod (18) is sleeved with a worm wheel (20), and the outer surface of the worm wheel (20) is meshedly connected with the outer surface of the worm (16).

6. A portable LED aviation obstruction light according to claim 1, characterized in that: The lower surface of the bottom plate (1) is provided with a storage groove (21), and the inner wall of the storage groove (21) is rotatably connected with a handle (22).

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