CN218268632U

CN218268632U - Portable solar aviation obstruction beacon

Info

Publication number: CN218268632U
Application number: CN202222496809.0U
Authority: CN
Inventors: 张明明
Original assignee: Xinyi Keli Wanhui Technology Co ltd
Current assignee: Xinyi Keli Wanhui Technology Co ltd
Priority date: 2022-09-21
Filing date: 2022-09-21
Publication date: 2023-01-10
Anticipated expiration: 2032-09-21

Abstract

The utility model discloses a portable solar energy aviation obstruction beacon of warning light technical field, including the aviation obstruction beacon, the mount pad is installed to the bottom of aviation obstruction beacon, the spout has all been seted up to the both sides outer wall of mount pad, the internally mounted of mount pad has the base, and its is rational in infrastructure, the utility model discloses a be equipped with dismouting mechanism, with dismouting mechanism setting on the base to install the aviation obstruction beacon on the base by the mount pad, make the aviation obstruction beacon carry out horizontal migration from top to bottom on the one hand on the base, can carry out altitude mixture control after making things convenient for the installation of aviation obstruction beacon to handle, on the other hand dismouting mechanism has adjustable installation and fixed effect, makes things convenient for the installation of aviation obstruction beacon, and need not to install fixedly through fastening bolt, and the effectual troublesome condition of solar energy aviation obstruction beacon dismouting of having avoided takes place, while simple structure, simple to operate, saves a large amount of loaded down with trivial details steps, the effectual dismouting efficiency that has improved.

Description

Portable solar aviation obstruction beacon

Technical Field

The utility model relates to a warning light technical field specifically is portable solar energy aviation obstruction beacon.

Background

The aviation obstruction light is that according to the national standard, the top of a high-rise building which is higher than the ground by more than 45 meters must be provided with the aviation obstruction light. In order to be distinguished from a general purpose illuminating lamp, the aviation obstruction light is not normally on but is flashing, the low-light-intensity aviation obstruction light is normally 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 not higher than 70 times per minute, and 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 obstruction to play a role in warning.

The defects of the existing solar aviation obstruction light are as follows: when solar energy aviation obstruction beacon installation, adopt fastening bolt fixed mode to install fixedly, because change the position at any time to solar energy aviation obstruction beacon according to user's needs to carry to when another position is laid, during must dismantle the processing to fastening bolt, and the dismantlement method need just can accomplish through corresponding instrument and dismantle, the process is comparatively loaded down with trivial details, and troublesome, lead to solar energy aviation obstruction beacon installation and dismantlement inefficiency on the one hand, on the other hand also causes the influence to solar energy aviation obstruction beacon convenience.

Therefore, the development of portable solar aviation obstruction lights is needed.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a portable solar energy aviation obstruction lamp, through being equipped with dismouting mechanism, set up dismouting mechanism on the base, and install aviation obstruction lamp on the base by the mount pad, make aviation obstruction lamp horizontal migration about can going on the base on the one hand, can carry out the altitude mixture control after making things convenient for aviation obstruction lamp to install and handle, on the other hand dismouting mechanism has adjustable installation and fixed effect, make things convenient for aviation obstruction lamp to install, and need not to install fixedly through fastening bolt, the effectual troublesome condition of solar energy aviation obstruction lamp dismouting of having avoided takes place, simple structure simultaneously, high durability and convenient installation, save a large amount of loaded down with trivial details steps, the effectual dismouting efficiency that has improved, with the problem of the troublesome influence of the dismouting of proposing solar energy aviation obstruction lamp in solving above-mentioned background art, and change the effect.

In order to achieve the above object, the utility model provides a following technical scheme: the portable solar aviation obstruction light comprises an aviation obstruction light, wherein a mounting seat is mounted at the bottom of the aviation obstruction light, sliding grooves are formed in the outer walls of two sides of the mounting seat, a base is mounted inside the mounting seat, and a dismounting mechanism is mounted at the bottom of the base;

the disassembly and assembly mechanism comprises an installation part and a fixed part, the installation part is connected with the base, and the fixed part is connected with the installation part.

Preferably, the support is installed in the both sides outer wall central point of mount pad, install solar panel on the outer wall of one side of support.

Preferably, the outer walls of the two sides of the base are provided with fixing screws, and the outer walls of the fixing screws are connected with the inner walls of the sliding grooves in a sliding mode.

Preferably, a locking nut A is installed on one side of the outer wall of the fixing screw rod, and the inner wall of the locking nut A is in threaded connection with the outer wall of the fixing screw rod.

Preferably, the mounting component comprises a U-shaped mounting frame, the top of the U-shaped mounting frame is fixedly connected with the bottom of the base, and threaded holes are formed in the center positions of the outer walls of the two sides of the U-shaped mounting frame.

Preferably, the threaded hole is internally provided with a jacking screw, the outer wall of the jacking screw is in threaded connection with the inner wall of the threaded hole, and the positioning holes are formed in the upper part and the lower part of the outer walls of the two sides of the U-shaped mounting frame.

Preferably, the fixing part comprises a fixing plate, and positioning rods are arranged above and below the outer wall of one side of the fixing plate.

Preferably, a locking nut B is installed on one side of the outer wall of the positioning rod, the inner wall of the locking nut B is in threaded connection with the outer wall of the positioning rod, and an anti-slip pad is arranged on the outer wall of the other side of the fixing plate.

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

through being equipped with dismouting mechanism, with the setting of dismouting mechanism on the base, and install the aviation obstruction lamp on the base by the mount pad, horizontal migration about making the aviation obstruction lamp can carry out on the base on the one hand, make things convenient for the installation of aviation obstruction lamp to carry out altitude mixture control and handle, on the other hand dismouting mechanism has adjustable installation and fixed effect, make things convenient for the installation of aviation obstruction lamp, and need not to install fixedly through fastening bolt, the effectual troublesome condition of solar energy aviation obstruction lamp dismouting of having avoided takes place, and is simple in structure simultaneously, high durability and convenient installation, save a large amount of loaded down with trivial details steps, the effectual dismouting efficiency that has improved.

Drawings

FIG. 1 is a front sectional view of the present invention;

fig. 2 is a front view provided by the present invention;

fig. 3 is an enlarged view of the structure at a in fig. 1 according to the present invention;

FIG. 4 is a front sectional view of the mounting and dismounting mechanism provided by the present invention;

fig. 5 is a perspective view of the mounting base structure provided by the present invention.

In the figure: 1. an aviation obstruction light; 2. a mounting seat; 201. a chute; 202. a support; 203. a solar panel; 3. a base; 301. fixing the screw rod; 302. locking the nut A; 4. a disassembly and assembly mechanism; 401. a U-shaped mounting bracket; 402. a threaded hole; 403. tightly pushing the screw rod; 404. positioning holes; 405. a fixing plate; 406. positioning a rod; 407. a locking nut B; 408. provided is a non-slip mat.

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.

The utility model provides a following technical scheme: the portable solar aviation obstruction light can effectively improve the assembly and disassembly efficiency of the portable solar aviation obstruction light in the use process, and is additionally provided with an assembly and disassembly mechanism 4, please refer to fig. 1-5, the portable solar aviation obstruction light comprises an aviation obstruction light 1, an installation seat 2 is installed at the bottom of the aviation obstruction light 1, sliding grooves 201 are formed in the outer walls of the two sides of the installation seat 2, brackets 202 are installed at the central positions of the outer walls of the two sides of the installation seat 2, a solar panel 203 is installed on the outer wall of one side of each bracket 202, a base 3 is installed in the installation seat 2, fixing screws 301 are arranged above the outer walls of the two sides of the base 3, the outer walls of the fixing screws 301 are in sliding connection with the inner walls of the sliding grooves 201, the installation seat 2 on the bottom of the aviation obstruction light 1 is installed on the outer wall of the base 3 in a sliding manner, fixing screws 301 on the outer walls of two sides of the base 3 penetrate through sliding grooves 201 in the mounting base 2, the mounting base 2 is enabled to move horizontally up and down on the outer wall of the base 3, meanwhile, limiting processing is carried out through the fixing screws 301, the situation that the mounting base 2 is separated from the base 3 is prevented, a locking nut A302 is installed on one side of the outer wall of the fixing screws 301, the inner wall of the locking nut A302 is in threaded connection with the outer wall of the fixing screws 301, after the aviation obstruction lamp 1 is installed in the later period, when height adjustment is needed, the height of the mounting base 2 can be adjusted, after the adjustment is finished, the locking nut A302 is rotated to carry out locking processing, the fixing of the position of the aviation obstruction lamp 1 can be achieved, and a dismounting mechanism 4 is installed at the bottom of the base 3;

the dismounting mechanism 4 comprises a mounting part and a fixing part, the mounting part is connected with the base 3, the fixing part is connected with the mounting part, the mounting part comprises a U-shaped mounting frame 401, the top of the U-shaped mounting frame 401 is fixedly connected with the bottom of the base 3, the center positions of the outer walls of two sides of the U-shaped mounting frame 401 are both provided with a threaded hole 402, a jacking screw 403 is arranged in the threaded hole 402, the outer wall of the jacking screw 403 is in threaded connection with the inner wall of the threaded hole 402, two groups of jacking screws 403 are correspondingly arranged in the threaded hole 402 on the U-shaped mounting frame 401 in a threaded connection mode, the jacking screw 403 rotates forwards or reversely and can horizontally move leftwards or rightwards on the U-shaped mounting frame 401, the upper part and the lower part of the outer walls of two sides of the U-shaped mounting frame 401 are both provided with positioning holes 404, the fixing part comprises a fixing plate 405, and the upper part and the lower part of the outer wall of one side of the fixing plate 405 are both provided with positioning rods 406, two sets of fixing plates 405 are arranged inside the U-shaped mounting frame 401, the fixing plates 405 are inserted into the positioning holes 404 on the U-shaped mounting frame 401 in a sliding manner through the positioning rods 406, so that the fixing plates 405 can horizontally move left and right in the U-shaped mounting frame 401, one side of the outer wall of each positioning rod 406 is provided with a locking nut B407, the inner wall of each locking nut B407 is in threaded connection with the outer wall of each positioning rod 406, the locking nuts B407 are arranged on the outer walls of the positioning rods 406 in a threaded connection manner, on one hand, the locking nuts B407 limit the fixing plates 405 to prevent the fixing plates 405 from being separated from the U-shaped mounting frame 401, on the other hand, the locking nuts B407 are disassembled, so that the fixing plates 405 can be disassembled, the anti-skid pads 408 are arranged on the outer walls on the other side of the fixing plates 405, and the anti-skid and protection treatment can be carried out on the fixing plates 405 by the anti-skid pads 408 by utilizing the effect of increasing friction and reducing wear of the anti-skid pads 408, the surface of the fixing plate 405 is prevented from being worn later.

The working principle is as follows: when the utility model is used, the mounting seat 2 on the bottom of the aviation obstruction light 1 is arranged on the outer wall of the base 3 in a sliding way, the fixing screw rods 301 on the outer walls on two sides of the base 3 penetrate through the sliding grooves 201 on the mounting seat 2, so that the mounting seat 2 can horizontally move up and down on the outer wall of the base 3, the fixing screw rods 301 can carry out limit treatment to prevent the mounting seat 2 from being separated from the base 3, the locking nut A302 is arranged on the outer wall of the fixing screw rods 301 in a threaded connection way, after the aviation obstruction light 1 is mounted in the later period, when the height adjustment is needed, the height of the mounting seat 2 can be adjusted, after the adjustment is finished, the locking nut A302 is rotated to carry out locking treatment, the position fixation of the aviation obstruction light 1 can be achieved, the U-shaped mounting rack 401 on the mechanism 4 is arranged at the bottom of the base 3, and two sets of tightening screw rods 403 are correspondingly arranged in the threaded holes 402 on the U-shaped mounting rack 401 in a threaded connection way, the tightening screw 403 is rotated forward or backward to horizontally move left or right on the U-shaped mounting rack 401, two sets of fixing plates 405 are arranged inside the U-shaped mounting rack 401, the fixing plates 405 are inserted into the positioning holes 404 on the U-shaped mounting rack 401 by the positioning rods 406 in a sliding manner, so that the fixing plates 405 can horizontally move left and right in the U-shaped mounting rack 401, the locking nuts B407 are arranged on the outer walls of the positioning rods 406 in a threaded manner, on one hand, the locking nuts B407 limit the fixing plates 405 to prevent the fixing plates 405 from being separated from the U-shaped mounting rack 401, on the other hand, the locking nuts B407 are disassembled, so that the fixing plates 405 can be disassembled, the anti-skid pads 408 are arranged on the outer walls of the other sides of the fixing plates 405, and the anti-skid pads 408 are used for increasing friction and reducing wear, make slipmat 408 carry out antiskid and protection to fixed plate 405 and handle, the condition emergence of wearing and tearing appears in the surperficial later stage of avoiding fixed plate 405, when installing aviation obstruction lamp 1, carry aviation obstruction lamp 1 and remove appointed place, and with U type mounting bracket 401 collocation fixed plate 405 centre gripping in the wall top on roof, through rotating tight screw rod 403 in top, make fixed plate 405 hug closely the wall surface, it is fixed to reach fixed plate 405 centre gripping, thereby it is fixed to reach to install aviation obstruction lamp 1, and need not to install fixedly through fastening bolt, the effectual troublesome condition emergence of solar energy aviation obstruction lamp dismouting of having avoided, moreover, the steam generator is simple in structure, high durability and convenient installation, save a large amount of loaded down with trivial details steps, the effectual dismouting efficiency that has improved.

While the invention has been described above with reference to an embodiment, various modifications may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In particular, the various features of the disclosed embodiments can be used in any combination that is not specifically enumerated in this specification for the sake of brevity and resource savings, provided that no structural conflict exists. Therefore, it is intended that the invention not be limited to the particular embodiments disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.

Claims

1. Portable solar energy aviation obstruction beacon, including aviation obstruction beacon (1), mount pad (2) are installed to the bottom of aviation obstruction beacon (1), spout (201) have all been seted up to the both sides outer wall of mount pad (2), the internally mounted of mount pad (2) has base (3), its characterized in that: the bottom of the base (3) is provided with a dismounting mechanism (4);

the dismounting mechanism (4) comprises a mounting part and a fixing part, the mounting part is connected with the base (3), and the fixing part is connected with the mounting part.

2. The portable solar aviation obstruction light of claim 1, wherein: support (202) are all installed to the both sides outer wall central point of mount pad (2) position, install solar panel (203) on the one side outer wall of support (202).

3. The portable solar aviation obstruction light of claim 1, wherein: the outer wall top of the both sides of base (3) all is provided with clamping screw (301), the outer wall of clamping screw (301) and the inner wall sliding connection of spout (201).

4. The portable solar aviation obstruction light of claim 3, wherein: and a locking nut A (302) is installed on one side of the outer wall of the fixing screw rod (301), and the inner wall of the locking nut A (302) is in threaded connection with the outer wall of the fixing screw rod (301).

5. The portable solar aviation obstruction light of claim 1, wherein: the mounting component comprises a U-shaped mounting frame (401), the top of the U-shaped mounting frame (401) is fixedly connected with the bottom of the base (3), and threaded holes (402) are formed in the center positions of the outer walls of the two sides of the U-shaped mounting frame (401).

6. The portable solar aviation obstruction light of claim 5, wherein: the inside mounting of screw hole (402) has top tight screw rod (403), the outer wall of top tight screw rod (403) and the inner wall threaded connection of screw hole (402), locating hole (404) have all been seted up to the both sides outer wall top and the below of U type mounting bracket (401).

7. The portable solar aviation obstruction light of claim 1, wherein: the fixing part comprises a fixing plate (405), and positioning rods (406) are arranged above and below the outer wall of one side of the fixing plate (405).

8. The portable solar aviation obstruction light of claim 7, wherein: a locking nut B (407) is installed on one side of the outer wall of the positioning rod (406), the inner wall of the locking nut B (407) is in threaded connection with the outer wall of the positioning rod (406), and an anti-skid pad (408) is arranged on the outer wall of the other side of the fixing plate (405).