CN209960361U

CN209960361U - Special aviation obstruction beacon for bridge

Info

Publication number: CN209960361U
Application number: CN201920468725.1U
Authority: CN
Inventors: 余秋实; 徐达军; 范建平; 闵艳
Original assignee: WUHAN LEIGUANG LIGHTNING CO Ltd
Current assignee: WUHAN LEIGUANG LIGHTNING CO Ltd
Priority date: 2019-04-09
Filing date: 2019-04-09
Publication date: 2020-01-17
Anticipated expiration: 2029-04-09

Abstract

The utility model relates to the technical field of aviation obstruction lamps, in particular to a special aviation obstruction lamp for a bridge, which comprises a bridge deck, a support fixedly connected with the top end of the bridge deck, a steel wire fixedly connected between the support and the bridge deck, a chute arranged at the inner side of the support, a slide block slidably connected with the inner side of the chute, a connecting block fixedly connected with the front section of the slide block, a mounting block fixedly connected with the front section of the connecting block, a first motor fixedly connected with the front end face of the mounting block, a gear fixedly connected with the end of a main shaft of the first motor, a rack fixedly connected with the inner side of the right end of the support, the gear and the rack mutually meshed, and a storage battery fixedly connected with the top end of the mounting block, in the utility model, the installation of the aviation obstruction lamp on the support is convenient through the arranged gear, the rack, the, the installation and the dismantlement are very convenient, save the cost of labor, and safe operation, easy operation, labour saving and time saving.

Description

Special aviation obstruction beacon for bridge

Technical Field

The utility model relates to an aviation obstruction light technical field specifically is special aviation obstruction light of bridge.

Background

According to the national standard, the aviation obstruction light is required to be arranged in a high-rise building with the top being higher than the ground by more than 45 meters, in order to be distinguished from a lighting lamp with general use, the aviation obstruction light is not always on but is flashing, the low-light-intensity aviation obstruction light is always on, the medium-light-intensity aviation obstruction light and the high-light-intensity aviation obstruction light are flashing, the flashing frequency is not lower than 20 times per minute and is not higher than 70 times per minute, the aviation obstruction light is used for displaying the outline of a structure, so that an aircraft operator can judge the height and the outline of the obstacle to play a warning role, and therefore, the demand for the special aviation obstruction light for bridges is increasing day by day.

Aviation obstruction beacon on most bridge that exists on the existing market all is the manual work and installs on the bridge, and aviation obstruction beacon support top on traditional bridge is the highest point, and needs artifical installation, and high altitude construction is very dangerous, and is difficult to the installation, inconvenient maintenance, and aviation obstruction beacon on the bridge also needs the installation at the steel wire high elevation part, and installation operation is troublesome, wastes time and energy, inconvenient installation, consequently, proposes the special aviation obstruction beacon of bridge to above-mentioned problem.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a special aviation obstruction beacon of bridge to solve the problem that proposes among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme:

the aviation obstruction light special for the bridge comprises a bridge deck, wherein a support is fixedly connected to the top end of the bridge deck, a steel wire is fixedly connected between the support and the bridge deck, a sliding groove is formed in the inner side of the support, a sliding block is slidably connected to the inner side of the sliding groove, a connecting block is fixedly connected to the front section face of the sliding block, an installing block is fixedly connected to the front section face of the connecting block, a first motor is fixedly connected to the front end face of the installing block, a gear is fixedly connected to the tail end of a main shaft of the first motor, a rack is fixedly connected to the inner side of the right end of the support, the gear and the rack are meshed with each other, a storage battery is fixedly connected to the top end of the installing block, a solar cell panel is fixedly connected to the outer side, the tail end of the second motor spindle is fixedly connected with a roller, one side of the second motor is fixedly connected with a rubber block, the outer side of the rubber block is connected with a steel wire in a sliding mode, and the bottom end of the mounting shell is fixedly connected with a gravity compensation block.

Preferably, the spout inside wall is "protruding" font setting, the slider and the connecting block combination outside with the spout inside wall is laminated mutually, the connecting block outside with spout inside wall sliding connection.

Preferably, the movement track of the mounting shell is in a linear state, the maximum length of the movement track of the mounting shell is equal to the height of the sliding groove, and the rear end face of the mounting block is in sliding connection with the support.

Preferably, the gyro wheel is "worker" font setting, the quantity of gyro wheel is two, is located the bottom the gyro wheel inboard through the pivot with the installation shell inside wall rotates to be connected, the steel wire sets up two between the gyro wheel.

Preferably, the rubber block is formed by a rubber cylindrical structure with large friction force, the rubber block is arranged on the outer side of the middle of the roller, and the storage battery, the solar panel and the aviation obstruction light which are positioned at the left end are arranged at the top end of the mounting shell.

Compared with the prior art, the beneficial effects of the utility model are that:

1. the utility model discloses in, through gear, rack, slider and the installation piece that sets up, first motor rotates and drives the gear rotation, and the gear moves on the rack, drives the slider and slides in the spout, and the installation of the aviation obstruction lamp on the support of being convenient for, and conveniently move down aviation worker's obstruction lamp, the daily maintenance of being convenient for, it is very convenient to install and dismantle, saves the cost of labor, safe operation, easy operation, labour saving and time saving.

2. The utility model discloses in, through the installation shell that sets up, the gyro wheel, block rubber and gravity compensation piece, the second motor operation drives the gyro wheel and rotates, two gyro wheels pass through the block rubber and press from both sides the steel wire tightly, then make the installation shell move on the steel wire through the frictional force of block rubber, drive the motion of aviation obstruction beacon, the installation of the aviation obstruction beacon of the elevation part of being higher than on the steel wire of being convenient for, convenient to use is swift, the installation problem of steel wire superelevation part contour beacon has been solved, the operation of being convenient for, convenient daily maintenance.

Drawings

FIG. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a schematic view of the structure at A of FIG. 1 according to the present invention;

FIG. 3 is a schematic view of the installation structure of the roller of the present invention;

fig. 4 is a schematic view of the mounting structure of the sliding block of the present invention.

In the figure: 1-bridge deck, 2-bracket, 3-steel wire, 4-slide block, 5-connecting block, 6-mounting block, 7-first motor, 8-gear, 9-rack, 10-storage battery, 11-solar panel, 12-aviation obstruction light, 13-mounting shell, 14-second motor, 15-roller, 16-rubber block and 17-gravity compensation block.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-4, the present invention provides a technical solution:

the aviation obstruction light special for the bridge comprises a bridge deck 1, wherein a support 2 is fixedly connected to the top end of the bridge deck 1, a steel wire 3 is fixedly connected between the support 2 and the bridge deck 1, a sliding groove is formed in the inner side of the support 2, a sliding block 4 is slidably connected to the inner side of the sliding groove, the mounting block 6 is convenient to limit, the stability of the device is improved, the movement of the mounting block 6 is convenient, a connecting block 5 is fixedly connected to the front end face of the sliding block 4, the mounting block 6 is fixedly connected to the front end face of the connecting block 5, a first motor 7 is fixedly connected to the front end face of the mounting block 6, a gear 8 is fixedly connected to the tail end of a main shaft of the first motor 7, a rack 9 is fixedly connected to the inner side of the right end of the support 2, the gear 8 and the rack 9 are mutually meshed, the aviation, be convenient for supply power to the device, battery 10 top fixedly connected with

aviation obstruction lamp

12, 3 outside sliding connection of steel wire has installation shell 13, the inboard fixedly connected with second motor 14 of installation shell 13 rear end face, the terminal fixedly connected with gyro wheel 15 of the 14 main shafts of second motor makes things convenient for aviation obstruction lamp 12 to move on

steel wire

3, 14 one side fixedly connected with rubber block 16 of second motor, increase frictional force, the 16 outsides of rubber block and 3 sliding connection of steel wire, installation shell 13 bottom fixedly connected with gravity compensation piece 17 makes left side aviation obstruction lamp 12 upwards all the time.

The inside wall of the sliding groove is in a convex shape, the outside of the combination of the sliding block 4 and the connecting block 5 is attached to the inside wall of the sliding groove, the outside of the connecting block 5 is in sliding connection with the inside wall of the sliding groove, the arrangement is favorable for improving the stability of the device, the installation and the disassembly of the aviation obstruction light 12 on the bracket 2 are convenient, the motion track of the installation shell 13 is in a linear state, the maximum length of the motion track of the installation shell 13 is equal to the height of the sliding groove, the rear end surface of the installation block 6 is in sliding connection with the bracket 2, the arrangement is favorable for facilitating the motion of the aviation obstruction light 12 on the bracket 2, the storage battery 10 is conveniently charged by the sunlight received by the solar cell panel 11, the rollers 15 are in an I-shaped arrangement, the number of the rollers 15 is two, and the inner side of the rollers 15 at the bottom end is rotatably, the steel wire 3 sets up two between the gyro wheel 15, this kind of setting is favorable to making things convenient for aviation obstruction light 12 to move on the steel wire 3, the assembly of being convenient for, the block rubber 16 comprises the great rubber system cylinder structure of frictional force, the block rubber 16 sets up in the 15 middle parts outsides of gyro wheel, is located the left end battery 10, solar cell panel 11 and aviation obstruction light 12 set up installation shell 13 top, this kind of being provided with does benefit to the power supply of aviation obstruction light 12 of being convenient for, improves the motion of installation shell 13 on steel wire 3.

The model of the first motor 7 is an MSMA502D servo motor, the model of the second motor 14 is an MSMA502D servo motor, and the model of the aviation obstruction light 12 is an ST-SAL-001 aviation obstruction light.

The working process is as follows: the device uses a storage battery 10 for power supply, a power supply is switched on to operate equipment, a first motor 7 operates an electric gear 8 to rotate, the gear 8 moves on a rack 9 to drive an installation block 6 to move, a sliding block 4 is driven to slide in a sliding groove through the connection of a connecting block 5, the sliding block 4 has a limiting function, then an aviation obstruction light 12 moves, the aviation obstruction light 12 moves to the top end of a support 2, a solar panel 11 can charge the storage battery 10, the aviation obstruction light 12 at the right end and the first motor 7 are powered by the storage battery 10 at the right end, the aviation obstruction light 12 on the support 2 is convenient to install and move down, the daily maintenance is convenient, the installation and disassembly are very convenient, the labor cost is saved, the safe operation is simple, the time and labor are saved, then a second motor 14 operates to drive rollers 15 to rotate, two rollers 15 clamp a steel wire 3 through a rubber block 16, make installation shell 13 move on steel wire 3, the aviation obstruction light 12 of left end is guaranteed in gravity compensation piece 17 in 3 tops of steel wire, and the battery 10 of left end supplies power to the aviation obstruction light 12 of second motor 14 and right-hand member, and the aviation obstruction light 12's of height mark part is gone up to the steel wire 3 installation of being convenient for, and convenient to use is swift, has solved the installation problem of 3 superelevation part profile lights of steel wire, the operation of being convenient for, convenient routine maintenance.

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

Claims

1. Special aviation obstruction beacon of bridge, including bridge floor (1), its characterized in that: the steel wire bridge is characterized in that a support (2) is fixedly connected to the top end of the bridge deck (1), a steel wire (3) is fixedly connected between the support (2) and the bridge deck (1), a sliding groove is formed in the inner side of the support (2), a sliding block (4) is slidably connected to the inner side of the sliding groove, a connecting block (5) is fixedly connected to the front section of the sliding block (4), an installation block (6) is fixedly connected to the front section of the connecting block (5), a first motor (7) is fixedly connected to the front end face of the installation block (6), a gear (8) is fixedly connected to the tail end of a main shaft of the first motor (7), a rack (9) is fixedly connected to the inner side of the right end of the support (2), the gear (8) and the rack (9) are meshed with each other, a storage battery (, battery (10) top fixedly connected with aviation obstruction beacon (12), steel wire (3) outside sliding connection has installation shell (13), installation shell (13) inboard fixedly connected with second motor (14) of rear end face, second motor (14) terminal fixedly connected with gyro wheel (15) of main shaft, second motor (14) one side fixedly connected with block rubber (16), block rubber (16) outside and steel wire (3) sliding connection, installation shell (13) bottom fixedly connected with gravity compensation piece (17).

2. The aviation obstruction light for bridges of claim 1, wherein: the spout inside wall is "protruding" font setting, slider (4) and connecting block (5) combination outside with the laminating of spout inside wall mutually, the connecting block (5) outside with spout inside wall sliding connection.

3. The aviation obstruction light for bridges of claim 1, wherein: the motion trail of the mounting shell (13) is in a linear state, the maximum length of the motion trail of the mounting shell (13) is equal to the height of the sliding groove, and the rear end face of the mounting block (6) is in sliding connection with the support (2).

4. The aviation obstruction light for bridges of claim 1, wherein: the roller (15) is arranged in an I shape, the number of the rollers (15) is two, the inner side of the roller (15) at the bottom end is rotatably connected with the inner side wall of the mounting shell (13) through a rotating shaft, and the steel wire (3) is arranged between the rollers (15).

5. The aviation obstruction light for bridges of claim 1, wherein: the rubber block (16) is formed by a rubber cylindrical structure with large friction force, the rubber block (16) is arranged on the outer side of the middle of the roller (15), and the storage battery (10), the solar cell panel (11) and the aviation obstruction light (12) which are positioned at the left end are arranged at the top end of the installation shell (13).