CN213746527U

CN213746527U - Solar aviation obstruction beacon convenient to transportation

Info

Publication number: CN213746527U
Application number: CN202023184737.3U
Authority: CN
Inventors: 刘东三; 刘泽斌; 李宁嘉; 谭锂; 孙腾
Original assignee: Hunan Lingte Technology Co ltd
Current assignee: Hunan Lingte Technology Co ltd
Priority date: 2020-12-25
Filing date: 2020-12-25
Publication date: 2021-07-20
Anticipated expiration: 2030-12-25

Abstract

The utility model discloses a solar energy aviation obstruction beacon convenient to transportation, including the obstruction beacon body, the battery box, solar cell panel and solar cell panel support, the obstruction beacon body sets up on the battery box, the battery sets up in the battery box, solar cell panel is fixed to be set up on the solar cell panel support, the solar cell panel support has two, every solar cell panel support includes the fixed bolster, movable support and spacing support, the fixed bolster sets up on the lateral wall of battery box, movable support's upper end is articulated with the fixed bolster, movable support's lower extreme is articulated with the one end of spacing support, the screens recess has been seted up to the other end of spacing support, still be provided with the screens bolt with screens recess matched with on the lateral wall of battery box. The utility model discloses after well solar cell panel support is folding, the packing space of solar energy aviation obstruction beacon has reduced nearly half, effectively practices thrift the cost of transportation.

Description

Solar aviation obstruction beacon convenient to transportation

Technical Field

The utility model relates to an aviation obstruction beacon technical field especially relates to a solar energy aviation obstruction beacon convenient to transportation.

Background

An Aviation Obstruction light (also called navigation light equipment) is a special lamp for marking obstacles, belongs to the industry of navigation light equipment, and is a range of lamp types under the seat of the Aviation Obstruction light. In order to be different from a general purpose illuminating lamp, 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 in flashing, the flashing frequency of the medium-light-intensity aviation obstruction light is 20-60 times per minute, and the flashing frequency of the high-light-intensity obstruction light is 40-60 times. 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.

Solar energy aviation obstruction lamp is often used in on higher building, for being convenient for the installation, installs solar panel whole packing on the obstruction lamp fixed bolster usually, causes solar energy aviation obstruction lamp to need occupy great space when packing, has reduced the convenient degree of solar energy aviation obstruction lamp transportation.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a solar energy aviation obstruction beacon convenient to transportation to solve the current solar energy aviation obstruction beacon packing volume that proposes in the background art big, the inconvenient problem of transportation, effectively reduce the cost of transportation.

In order to achieve the purpose, the utility model provides a solar aviation obstruction light convenient to transport, which comprises an obstruction light body, a storage battery box, solar panels and solar panel supports, wherein the obstruction light body is arranged on the top of the storage battery box, the storage battery is arranged in the storage battery box, the solar panels are arranged on the solar panel supports, the two solar panel supports are arranged on the solar panel supports in parallel and oppositely arranged on one side of the storage battery box, each solar panel support comprises a fixed support, a movable support and a limiting support, the fixed support is arranged on one of the outer side walls of the storage battery box, one end of the movable support is hinged with the fixed support, the other end of the movable support is hinged with one end of the limiting support, the other end of the limiting bracket is provided with a clamping groove; the battery box is provided with a fixing support, the fixing support is arranged on the outer side wall of the battery box, and the outer side wall of the battery box is adjacent to the outer side wall of the battery box.

Furthermore, the movable support is hinged to the fixed support through a first hinge device, the movable support is hinged to the limiting support through a second hinge device, and the first hinge device and the second hinge device both comprise a bolt and a nut which are matched with each other.

Furthermore, a first bolt sleeve is arranged on the fixed support, a second bolt sleeve is arranged on the movable support, and the fixed support and the movable support are both plates with L-shaped sections.

Furthermore, a connecting pin for fixing the solar cell panel is arranged on the supporting surface of the movable support.

Further, a support seat is fixed at the bottom of the storage battery box; when the solar cell panel support is in a folded state, the lower ends of the movable support and the solar cell panel are not lower than the lower surface of the supporting seat.

Furthermore, the storage battery box and the solar cell panel support are both made of high-strength stainless steel materials, and rustproof outdoor powder is sprayed on the outer surfaces of the storage battery box and the solar cell panel support.

Compared with the prior art, the utility model discloses following beneficial effect has:

the utility model relates to an among the solar energy aviation obstruction beacon convenient to transportation, every solar cell panel support all includes fixed bolster, movable support and spacing support, sets up on one of them lateral wall of battery box, and movable support's both ends are articulated respectively with spacing support and fixed bolster. When the solar cell panel bracket is used, the clamping bolt is positioned in the clamping groove on the limiting bracket, and the solar cell panel bracket is in an unfolded state; when the solar aviation obstruction light needs to be packaged and transported, the second hinge device is used as a rotation point to rotate the limiting support, so that the clamping bolt is separated from the clamping groove, and the solar panel support is folded and folded on the side part of the storage battery box. The utility model discloses a solar energy aviation obstruction beacon, solar cell panel support folding back solar energy aviation obstruction beacon's packaging space has reduced nearly half, practices thrift the cost of transportation.

In addition to the above-described objects, features and advantages, the present invention has other objects, features and advantages. The present invention will be described in further detail with reference to the drawings.

Drawings

The accompanying drawings, which are incorporated in and constitute a part of this application, are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification. In the drawings:

fig. 1 is a schematic structural view of a solar aviation obstruction light bracket according to a preferred embodiment of the invention in an unfolded state;

FIG. 2 is a schematic structural view of a folded state of a solar aviation obstruction light bracket according to a preferred embodiment of the invention;

fig. 3 is a schematic perspective view of the solar aviation obstruction light bracket according to the preferred embodiment of the present invention in an expanded state;

the obstacle lamp comprises a body 1, a storage battery 2, a storage battery box 3, a solar panel 4, a solar panel support 5, a fixed support 5.1, a movable support 5.2, a limiting support 5.3, a clamping groove 5.3, a first hinge device 5.4, a second hinge device 5.5, a first bolt sleeve 5.6, a second bolt sleeve 5.7, a clamping bolt 6, a connecting pin 7 and a supporting seat 8.

Detailed Description

The embodiments of the invention will be described in detail hereinafter with reference to the accompanying drawings, but the invention can be implemented in many different ways, which are defined and covered by the claims.

Referring to fig. 1 and 2, the embodiment provides a solar aviation obstruction light convenient to transport, which includes an obstruction light body 1, a storage battery 2, a storage battery box 3, a solar panel 4 and a solar panel bracket 5. The barrier lamp body 1 is fixedly arranged on the top of the storage battery box, and the storage battery is arranged in the storage battery box. Preferably, the obstruction light body 1 can be a standard B-type medium-intensity obstruction light with the model number being LT-01-MB/DC (L) or other types.

Referring to fig. 3, an exploded structure of the solar panel support is shown. The solar aviation obstruction light comprises two solar cell panel supports, and the two solar cell panels are parallel and are oppositely arranged on the same side of the storage battery box. Every solar cell panel support 5 all includes fixed bolster 5.1, movable support 5.2 and spacing support 5.3, and fixed bolster and movable support all are the plate of cross-section for the L type, and spacing support is banding flat board. The fixed support is fixedly arranged on one outer side wall of the storage battery box, the upper end of the movable support is hinged with the fixed support through a first hinge device 5.4, and the lower end of the movable support is hinged with one end of the limiting support through a second hinge device 5.5; the first hinge means and the second hinge means each comprise a bolt and a nut. Specifically, the bolts in the first hinge devices penetrate through the hinge holes of the movable support and the fixed support, the bolts in the second hinge devices penetrate through the hinge holes of the movable support and the limiting support, and the nuts in the first hinge devices and the second hinge devices can be matched with the bolts to limit rotation between the movable support and the fixed support and between the movable support and the limiting support when the solar cell panel support is in the unfolded state.

In the preferred embodiment of the utility model, the fixed bracket is provided with a first bolt sleeve 5.6 which is used for matching with the first hinge device, and the movable bracket is provided with a second bolt sleeve 5.7 which is used for matching with the second hinge device; the first bolt sleeve and the second bolt sleeve are arranged corresponding to the hinge holes. The other end of the limiting bracket is provided with a clamping groove 5.3 a; two clamping bolts 6 are respectively arranged on the other two outer side walls adjacent to the outer side wall provided with the fixing support on the storage battery box, and the two clamping bolts are respectively used for being matched with the clamping grooves on the two limiting supports. The structure can change the matching relation between the clamping bolt and the clamping groove, so that the solar cell panel support is limited to be in an unfolded or folded state.

In the preferred embodiment of the present invention, two ends of the supporting surface of each movable support are respectively provided with a connecting pin 7, and the solar cell panel is fixedly mounted on the two solar cell panel supports through a plurality of connecting pins. The bottom of the storage battery box is also provided with a supporting seat 8; when the solar aviation obstruction light is in a folded state, the lower ends of the movable support and the solar cell panel are not lower than the lower surface of the supporting seat. The structure can further ensure that the packaging space of the solar aviation obstruction light is effectively saved and the transportation cost is reduced when the solar cell panel support is in a furled state.

The utility model discloses in the preferred embodiment, battery box and solar cell panel support are made by high strength stainless steel material, and battery box and solar cell panel support's surface all sprays has rust-resistant outdoor powder to guarantee that this solar energy aviation obstruction beacon can stable work in abominable environment for a long time.

The utility model discloses in preferred embodiment, when the solar cell panel support is in the expansion state, screens recess and the cooperation of screens bolt on the spacing support, also be in the screens recess for the screens bolt. Meanwhile, the clamping bolt, the first hinge device and the second hinge device respectively lock and fix the position between the limiting support and the storage battery box, the position between the movable support and the fixed support and the position between the movable support and the limiting support. Therefore, a triangular support is formed among the fixed support, the movable support and the limiting support of the solar cell panel support, and a stable supporting effect can be achieved.

The utility model discloses in the preferred embodiment, the concrete folding process of solar cell panel support as follows: firstly, unscrewing the clamping bolt, the first hinge device and the second hinge device, then enabling the limiting bracket to rotate by taking the second hinge device as a center, and enabling the limiting bracket to be separated from the limitation of the clamping bolt; meanwhile, the movable support is rotated and folded by taking the first hinge device as a center, the movable support is finally arranged on one side of the storage battery box, the limiting support is supported and erected on the clamping bolt, and the effect after folding is shown in fig. 2. Before the solar cell panel support is unfolded and after the folding, the packaging space of the solar aviation obstruction light is reduced by nearly half, the transportation is safe, and the cost is low.

The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The solar aviation obstruction light convenient to transport is characterized by comprising an obstruction light body (1), a storage battery (2), a storage battery box (3), two solar cell panels (4) and two solar cell panel supports (5), wherein the obstruction light body is arranged on the top of the storage battery box, the storage battery is arranged in the storage battery box, the solar cell panels are arranged on the solar cell panel supports, the two solar cell panel supports are arranged on one side of the storage battery box in parallel and oppositely, each solar cell panel support comprises a fixed support (5.1), a movable support (5.2) and a limiting support (5.3), the fixed support is arranged on one outer side wall of the storage battery box, one end of the movable support is hinged with the fixed support, the other end of the movable bracket is hinged with one end of the limiting bracket, and the other end of the limiting bracket is provided with a clamping groove (5.3 a); the battery box is provided with a fixing support, the battery box is provided with a clamping groove, the clamping groove is arranged on the outer side wall of the battery box, the other two adjacent outer side walls of the outer side walls provided with the fixing support are respectively provided with a clamping bolt (6), and the clamping bolts are used for being matched with the clamping groove to position the limiting support.

2. Solar aircraft obstruction light according to claim 1, characterized in that the mobile bracket is hinged to the fixed bracket by a first hinge means (5.4) and to the limit bracket by a second hinge means (5.5), the first and second hinge means each comprising a cooperating bolt and nut.

3. The solar aviation obstruction light of claim 2, wherein the fixed support is provided with a first bolt sleeve (5.6), the movable support is provided with a second bolt sleeve (5.7), and the fixed support and the movable support are both plate members with L-shaped sections.

4. The solar aviation obstruction light of claim 1, wherein a connecting pin (7) for fixing the solar panel is arranged on the supporting surface of the movable bracket.

5. The solar aviation obstruction light of claim 1, wherein a support base (8) is fixed to the bottom of the battery box; when the solar cell panel support is in a folded state, the lower ends of the movable support and the solar cell panel are not lower than the lower surface of the supporting seat.

6. The solar aviation obstruction light of any one of claims 1 to 5, wherein the battery box and the solar panel bracket are both made of high-strength stainless steel material, and the outer surfaces of the battery box and the solar panel bracket are sprayed with anti-rust outdoor powder.