CN219036401U

CN219036401U - Aviation warning lamp for high-altitude wires

Info

Publication number: CN219036401U
Application number: CN202320295066.2U
Authority: CN
Inventors: 钟民; 张伟; 易凡超; 高宇
Original assignee: Wuhan Zhongyuan Huihe Technology Co ltd
Current assignee: Wuhan Zhongyuan Huihe Technology Co ltd
Priority date: 2023-02-23
Filing date: 2023-02-23
Publication date: 2023-05-16
Anticipated expiration: 2033-02-23

Abstract

The utility model discloses an aviation warning lamp for a high-altitude wire, which comprises two opposite U-shaped plates, wherein a first groove is formed in the vertical end of the U-shaped plate above the U-shaped plate, a plugboard matched with the first groove is arranged at the vertical end of the U-shaped plate below the U-shaped plate, a limit bolt is inserted in the first groove in a rotating mode, a plurality of semicircular rings are sequentially sleeved in the U-shaped plate, a second vertical groove which is opposite left and right is respectively arranged on the front side wall and the rear side wall of the U-shaped plate, the cross section of the second groove is of a T-shaped structure, the width of the bottom of the second groove is larger than that of an opening, T-shaped plates are arranged in the second groove in a sliding mode up and down, a limit plate is connected between the T-shaped plates of the same U-shaped plate, a limit screw is inserted in the front side of the limit plate in a rotating mode, and a warning lamp is connected below the U-shaped plate below the limit plate. The utility model has wide application range and high safety.

Description

Aviation warning lamp for high-altitude wires

Technical Field

The utility model relates to the technical field of aviation warning lamps, in particular to an aviation warning lamp for high-altitude wires.

Background

The aviation warning lamp is a special lamp for identifying the obstacle, and has the function of displaying the outline of the structure, so that an aircraft operator can judge the height and the outline of the obstacle, and the warning function is achieved.

As is well known, in a power transmission system, a high-voltage wire is a very common electric auxiliary device, and in order to avoid external damage during use, many high-voltage wires are generally erected at high altitude by using a telegraph pole, but at night, the color of the high-voltage wire is also deep, so that the high-voltage wire is easily dissolved in night and is not easily found by people, and great risks exist for aviation and related industries.

The aviation warning light that uses at present, the volume is great, runs into under the influence of bad weather, and the rocking of production can drive the electric wire and rock, and the security performance remains to improve.

Disclosure of Invention

The utility model aims to solve the problems and provides an aviation warning lamp for high-altitude wires.

In order to solve the technical problems, the technical scheme provided by the utility model is as follows: the utility model provides an aviation warning light for high altitude wire, includes two relative U-shaped boards, two U-shaped boards be located upper and lower both sides respectively, and the opening is close to mutually, U-shaped board inner wall be semicircle annular structure, be located the top U-shaped board vertical one end be equipped with recess one respectively, be located the below U-shaped board vertical one end be equipped with recess one complex picture peg, the picture peg lateral wall be equipped with about to internal thread through-hole one, recess one be close to the inner wall in center be equipped with internal thread through-hole one corresponding internal thread blind hole, keep away from the inner wall in center be equipped with internal thread through-hole two, internal thread through-hole one and internal thread blind hole between rotate and peg graft there is stop bolt, the U-shaped board in proper order cup joint a plurality of semicircle ring-shaped structures, U-shaped board front and back lateral wall be equipped with respectively about relative vertical recess two, recess two cross sections be T-shaped structure, and the width of bottom be greater than open-ended width, recess two in slide from top to bottom be equipped with T, be located same U-shaped board's internal thread through-hole one is equipped with spacing bolt of internal thread through-hole one, U-shaped through hole one and internal thread through-hole one have a limit bolt.

As improvement, the length of the limit bolt with threads is equal to the length between the second internal thread through hole, the first internal thread through hole and the blind hole.

As an improvement, a solar panel matched with the warning lamp is connected below the U-shaped plate positioned above.

As an improvement, the length of the limiting screw rod is greater than the thickness of the limiting plate, two ends of the limiting screw rod are respectively connected with a disc, the diameter of each disc is greater than that of the limiting screw rod, and one disc is attached to the U-shaped plate.

As an improvement, the side wall of the semicircular ring is provided with anti-skid patterns.

Compared with the prior art, the utility model has the advantages that: according to the aviation warning lamp for the high-altitude wire, the device can be installed on the wire by connecting the two U-shaped plates, and the plurality of semicircular rings are installed in the U-shaped plates according to the diameter of the wire, so that the device can tightly clamp the wire and fix the position of the wire on the wire, warning is provided for a driver, and the weight of the warning lamp is concentrated on the lower side, so that the warning lamp is not easy to shake on the wire, and the safety performance is high.

Drawings

Fig. 1 is a schematic structural diagram of an aviation warning lamp for high-altitude wires in use according to the present utility model.

Fig. 2 is a schematic diagram of an exploded structure of an aviation warning lamp for high-altitude wires according to the present utility model.

Fig. 3 is a schematic diagram of a connection structure of a limiting plate of an aviation warning lamp for high-altitude wires.

As shown in the figure: 1. a U-shaped plate; 2. a groove I; 3. inserting plate; 4. an internal thread through hole I; 5. an internal thread blind hole; 6. an internal thread through hole II; 7. a limit bolt; 8. a semicircular ring; 9. a second groove; 10. a T-shaped plate; 11. a limiting plate; 12. a limit screw; 13. a warning light; 14. a solar panel; 15. a disk.

Detailed Description

The present utility model will be described in further detail with reference to the accompanying drawings.

Referring to fig. 1-3, an aviation warning lamp for high-altitude wires comprises two opposite U-shaped plates 1, wherein the two U-shaped plates 1 are respectively positioned at the upper side and the lower side, openings are close to each other, the inner wall of each U-shaped plate 1 is of a semicircular structure, a groove I2 is respectively arranged at the vertical end of the U-shaped plate 1 positioned above, an inserting plate 3 matched with the groove I2 is arranged at the vertical end of the U-shaped plate 1 positioned below, a left internal thread through hole I4 and a right internal thread through hole I4 are arranged on the side wall of the inserting plate 3, an internal thread blind hole 5 corresponding to the internal thread through hole I4 is arranged on the inner wall of the groove I2 close to the center, an internal thread through hole II 6 corresponding to the internal thread through hole I4 is arranged on the inner wall far from the center, a limit bolt 7 is rotationally inserted between the internal thread through hole II 6 and the internal thread through hole I4 and the internal thread blind hole 5, the U-shaped plate 1 is internally and sequentially sleeved with a plurality of semicircular rings 8, the front side wall and the rear side wall of the U-shaped plate 1 are respectively provided with a left vertical groove II 9 and a right vertical groove II, the cross section of the groove II is of a T-shaped structure, the width of the bottom is larger than the width of the opening, the groove II is internally and vertically provided with a T-shaped plate 10 in a sliding manner, a limiting plate 11 is connected between the T-shaped plates 10 of the same U-shaped plate 1, the front side of the limiting plate 11 is rotationally inserted with a limiting screw rod 12, the lower side of the U-shaped plate 1 is connected with a warning lamp 13, the semicircular rings 8 with corresponding sizes are arranged in the U-shaped plate 1 according to the diameter of a wire, the diameter of the inner wall of the semicircular rings 8 is equal to the diameter of the wire, the position of the semicircular rings 8 is slid up and down, the limiting plate 11 is positioned at the front side of the semicircular rings 8, the limiting screw rod 12 is rotated to limit the semicircular rings 8, the positions of the semicircular rings 8 are fixed, the U-shaped plate 1 is sleeved on the lead, the inserting plate 3 is inserted into the first groove 2, the plug-in limiting bolt 7 is fixed by rotating the plug-in limiting bolt between the second internal thread through hole 6, the first internal thread through hole 4 and the first internal thread blind hole 5, the device is fixed on the lead, warning is provided for a driver, and the weight is concentrated on the lower side due to the fact that the warning lamp 13 is located below, so that the plug-in limiting bolt is not easy to shake on the lead, and the safety performance is higher.

The length of the threads of the limit bolt 7 is equal to the length between the second internal thread through hole 6, the first internal thread through hole 4 and the internal thread blind hole 5, so that the limit bolt 7 is just attached to the U-shaped plate 1 when being inserted into the device.

The solar panel 14 matched with the warning lamp 13 is connected below the U-shaped plate 1 positioned above, and can provide energy for the warning lamp 13 for long-term use.

The length of the limiting screw 12 is greater than the thickness of the limiting plate 11, two ends of the limiting screw 12 are respectively connected with a disc 15, the diameter of each disc 15 is greater than that of the limiting screw 12, one disc 15 is attached to the U-shaped plate 1, the limiting screw 12 is convenient to rotate, and the discs 15 are better than the semicircular rings 8.

The side wall of the semicircular ring 8 is provided with anti-skidding patterns, so that the device clamps the wire firmly and prevents the wire from sliding on the wire.

In the implementation of the utility model, the aviation warning lamp for the high-altitude wire is characterized in that a semicircular ring 8 with a corresponding size is arranged in a U-shaped plate 1 according to the diameter of the wire, the diameter of the inner wall of the semicircular ring 8 is equal to the diameter of the wire, the position of a limiting plate 11 is slid up and down, the limiting plate 11 is positioned at the front side of the semicircular ring 8, a limiting screw 12 is rotated to limit the semicircular ring 8, the position of the semicircular ring 8 is fixed, the U-shaped plate 1 is sleeved on the wire, a plugboard 3 is inserted into a groove I2, and an inserting limiting bolt 7 is rotated between an internal thread through hole II 6, an internal thread through hole I4 and an internal thread blind hole 5 for fixation, so that the device is fixed on the wire to provide warning for a driver, and the warning lamp 13 is positioned below, so that the weight is concentrated at the lower side, the device is not easy to shake on the wire, and the safety performance is higher.

Meanwhile, the length of the threads of the limit bolt 7 is equal to the length between the second internal thread through hole 6, the first internal thread through hole 4 and the internal thread blind hole 5, so that the limit bolt 7 is just attached to the U-shaped plate 1 when being inserted into the device; a solar panel 14 matched with the warning lamp 13 is connected below the U-shaped plate 1 above, and can provide energy for the warning lamp 13 for long-term use; the length of the limiting screw rod 12 is greater than the thickness of the limiting plate 11, two ends of the limiting screw rod 12 are respectively connected with a disc 15, the diameter of each disc 15 is greater than that of the limiting screw rod 12, one disc 15 is attached to the U-shaped plate 1, the limiting screw rod 12 is convenient to rotate, and the discs 15 are better than the semicircular rings 8; the side wall of the semicircular ring 8 is provided with anti-slip patterns, so that the device clamps the wire firmly and prevents the wire from sliding on the wire.

The utility model and its embodiments have been described above with no limitation, and the actual construction is not limited to the embodiments of the utility model as shown in the drawings. In summary, if one of ordinary skill in the art is informed by this disclosure, a structural manner and an embodiment similar to the technical solution should not be creatively devised without departing from the gist of the present utility model.

Claims

1. An aviation warning light for high altitude conductors, comprising two opposite U-shaped plates (1), characterized in that: two U-shaped plates (1) are respectively positioned at the upper side and the lower side, openings are close to each other, the inner wall of each U-shaped plate (1) is of a semicircular annular structure, the vertical end of each U-shaped plate (1) is respectively provided with a groove I (2), the vertical end of each U-shaped plate (1) is positioned below, an inserting plate (3) matched with the groove I (2) is arranged at one end of each U-shaped plate, the side wall of each inserting plate (3) is provided with a left inner threaded through hole I (4) and a right inner threaded through hole I (4), the inner wall of each groove I (2) close to the center is provided with an inner threaded through hole II (6) corresponding to the inner threaded through hole I (4), the inner threaded through hole II (6), the inner threaded through hole I (4) and the inner threaded through hole (5) are rotationally inserted with a limit bolt (7), a plurality of semi-circular ring plates (8) are sequentially sleeved in each U-shaped plate (1), the front side wall and the rear side wall of each U-shaped plate (1) are respectively provided with a left inner threaded through hole II (9) and a right inner threaded through hole II (9), the inner wall far away from the center is provided with an inner threaded through hole II (6) corresponding to the inner threaded through hole II (4) corresponding to the inner threaded through hole I (4), the inner threaded through hole II (4) is provided with a limit bolt (9) corresponding to the inner threaded through hole II, the front side of the limiting plate (11) is rotatably inserted with a limiting screw rod (12), and a warning lamp (13) is connected below the U-shaped plate (1) positioned below.

2. An aviation warning light for high-altitude conductors according to claim 1, characterized in that: the length of the limit bolt (7) with threads is equal to the length among the second internal thread through hole (6), the first internal thread through hole (4) and the blind hole (5).

3. An aviation warning light for high-altitude conductors according to claim 1, characterized in that: the solar panel (14) matched with the warning lamp (13) is connected below the U-shaped plate (1) positioned above.

4. An aviation warning light for high-altitude conductors according to claim 1, characterized in that: the length of the limiting screw (12) is greater than the thickness of the limiting plate (11), two ends of the limiting screw (12) are respectively connected with a disc (15), the diameter of the disc (15) is greater than the diameter of the limiting screw (12), and one disc (15) is attached to the U-shaped plate (1).

5. An aviation warning light for high-altitude conductors according to claim 1, characterized in that: the side wall of the semicircular ring (8) is provided with anti-skid patterns.