CN210219580U

CN210219580U - Solar low-light-intensity aviation obstruction light

Info

Publication number: CN210219580U
Application number: CN201921241735.8U
Authority: CN
Inventors: Weiguo Yan; 严为国; Yuxiang Wang; 汪钰翔
Original assignee: Jiangsu Pengxiang Aviation Technology Co Ltd
Current assignee: Jiangsu Pengxiang Aviation Technology Co Ltd
Priority date: 2019-08-02
Filing date: 2019-08-02
Publication date: 2020-03-31
Anticipated expiration: 2029-08-02

Abstract

The utility model discloses a solar energy low light intensity aviation obstruction beacon, including unable adjustment base, solar cell is installed through the mounting pad in unable adjustment base's inside, and unable adjustment base's top fixed mounting has the mount pad, the inside fixed mounting of mount pad has the heat conduction mount pad, and the top fixed mounting of heat conduction mount pad has the heat conduction mounting bracket that extends to the mount pad top, the mount pad top fixed mounting in the LED lamp pearl outside has transparent lamp shade, the top fixed mounting of solar panel mounting bracket has the solar photovoltaic board. The utility model discloses solar storage battery and solar photovoltaic board have been set up for the barrier lamp can absorb solar energy through the solar photovoltaic board and turn into the electric energy when daytime, and store through solar storage battery, thereby provide the electric energy for the barrier lamp when also using night, and then saved the electric power resource, improved the feature of environmental protection of barrier lamp.

Description

Solar low-light-intensity aviation obstruction light

Technical Field

The utility model relates to an aviation obstruction light technical field specifically is a solar energy low light intensity aviation obstruction light.

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 lamp range under the seat of 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 of the medium-light-intensity aviation obstruction light is 20 times/min to 60 times/min, and the flashing frequency of the high-light-intensity aviation obstruction light is 40 times/min to 60 times/min; the aviation obstruction light has the function of 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, and the function of the low-light-intensity aviation obstruction light is particularly important.

The existing low-light intensity aviation obstruction light has the following defects: 1. the existing low-light-intensity barrier lamp generally adopts an external power supply mode to supply power, and has the problem of large power consumption under the condition that the barrier lamp is used for a long time, so that the existing low-light-intensity barrier lamp is poor in environmental protection; 2. the existing low-light-intensity aviation obstruction lamp is generally integrated and cannot be disassembled, so that the light-emitting element cannot be maintained and replaced according to the requirement, and the practicability is poor.

Therefore, there is a need for improvement of the prior art to solve the above problems.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a solar energy low light intensity aviation obstruction beacon 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 utility model provides a solar energy low light intensity aviation obstruction beacon, includes unable adjustment base, solar cell is installed through the mounting pad in unable adjustment base's inside, and unable adjustment base's top fixed mounting has the mount pad, the inside fixed mounting of mount pad has the heat conduction mount pad, and the top fixed mounting of heat conduction mount pad has the heat conduction mounting bracket that extends to the mount pad top, the top fixed mounting of heat conduction mounting bracket has LED lamp pearl mounting base, and LED lamp pearl is evenly installed at the top of LED lamp pearl mounting base, the mount pad top fixed mounting in the LED lamp pearl outside has transparent lamp shade, the front and the back at unable adjustment base top all have the mounting bar through bolt structure fixed mounting, and the end fixed mounting of mounting bar has the solar panel mounting bracket, the top fixed mounting of solar panel mounting bracket has the solar photovoltaic board.

Preferably, the bottom of the fixed base is fixedly provided with a fixed bottom plate, and four sides of the fixed bottom plate are fixedly provided with fixing screws.

Preferably, the inside fixed mounting of heat conduction mount pad has the wiring board, and the wiring board passes through wire and solar cell electric connection, and the positive fixedly connected with power connecting wire of wiring board position department mount pad, LED lamp pearl mounting base passes through wire and wiring board electric connection.

Preferably, the center position department fixed mounting at transparent lamp shade top has the guide bar, and the inside wall fixed mounting of transparent lamp shade has red lens.

Preferably, the transparent lampshade is fixedly installed in four groups of installation grooves at the top of the installation seat through four groups of fixing feet at the four sides of the bottom, and the fixing feet are fixedly connected with the installation seat through fixing bolts.

Preferably, one side fixed mounting that unable adjustment base is close to the solar photovoltaic board has the wiring jack with solar battery electric connection, and the solar photovoltaic board passes through solar panel connecting wire and wiring jack electric connection, fixed mounting has spacing supporting seat on the solar panel mounting bracket of solar photovoltaic board low side, and unable adjustment base's front has the battery maintenance board through bolt structure fixed mounting.

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

1. this low light intensity aviation obstruction lamp of solar energy has set up solar battery and solar photovoltaic board for the obstruction lamp can absorb solar energy through solar photovoltaic board and turn into the electric energy when the day, and store through solar battery, thereby provide the electric energy for the obstruction lamp when also using night, and then saved the electric power resource, improved the feature of environmental protection of obstruction lamp.

2. This solar energy low light intensity aviation obstruction lamp is through the transparent lamp shade of fixed foot and fixing bolt installation for the obstruction lamp can be dismantled according to the demand, and the maintenance panel that sets up simultaneously can make things convenient for maintainer to the maintenance and the change of the light-emitting component of obstruction lamp and battery, thereby has improved the practicality of obstruction lamp, and can increase the life of obstruction lamp.

Drawings

Fig. 1 is a schematic structural view of the present invention;

fig. 2 is a front view of the present invention;

fig. 3 is a top view of the present invention;

fig. 4 is a partial structure diagram of the present invention.

In the figure: 1. fixing the bottom plate; 101. fixing the screw rod; 2. a fixed base; 3. a solar storage battery; 4. mounting a bar; 5. a mounting seat; 501. mounting grooves; 6. a fixing leg; 601. fixing the bolt; 7. a transparent lampshade; 701. a red lens; 702. a guide rod; 8. LED lamp beads; 9. an LED lamp bead mounting base; 10. a thermally conductive mounting bracket; 11. a heat conducting mounting base; 12. a wiring board; 1201. a power connection line; 13. a wiring jack; 14. a solar panel connecting line; 15. a solar photovoltaic panel; 16. a solar panel mounting frame; 1601. a limiting support seat; 17. and a storage battery maintenance board.

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.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Referring to fig. 1-4, the present invention provides an embodiment: a solar low-light-intensity aviation obstruction light comprises a fixed base 2, a solar storage battery 3 is installed inside the fixed base 2 through a mounting pad, a mounting seat 5 is fixedly installed at the top of the fixed base 2, a heat conduction mounting seat 11 is fixedly installed inside the mounting seat 5, a heat conduction mounting frame 10 extending to the top of the mounting seat 5 is fixedly installed at the top of the heat conduction mounting seat 11, the mounting seat 5 facilitates the fixed installation of the heat conduction mounting seat 11, the heat conduction mounting seat 11 facilitates the fixed installation of an LED lamp bead mounting base 9, so that the heat conduction and radiation effects are improved, an LED lamp bead mounting base 9 is fixedly installed at the top of the heat conduction mounting frame 10, LED lamp beads 8 are uniformly installed at the top of the LED lamp bead mounting base 9, the LED lamp bead mounting base 9 facilitates the fixed installation of the LED lamp beads 8, the LED lamp beads 8 can emit light under the action of electric energy, so as to illuminate, a transparent lampshade 7 is fixedly installed at the top of, transparent lamp shade 7 can play lighting protection's effect, and can change the colour of illumination light, the front and the back at 2 tops of unable adjustment base all have mounting bar 4 through bolt structure fixed mounting, and the end fixed mounting of mounting bar 4 has solar panel mounting bracket 16, the top fixed mounting of solar panel mounting bracket 16 has solar photovoltaic board 15, the solar panel mounting bracket 16 is convenient for the fixed mounting of solar photovoltaic board 15, solar photovoltaic board 15 can be with solar energy transformation to the electric energy store to solar battery 3 in, thereby provide the electric energy for LED lamp pearl 8.

Further, the bottom of unable adjustment base 2 is fixed mounting has PMKD 1, and the all fixed mounting of four sides of PMKD 1 has clamping screw 101, and in the embodiment, PMKD 1 can make things convenient for the fixed mounting of PMKD 2, and clamping screw 101 can make things convenient for PMKD 1 fixed mounting at work area.

Further, the inside fixed mounting of heat conduction mount pad 11 has wiring board 12, and wiring board 12 passes through wire and 3 electric connection of solar cell, the positive fixedly connected with power connecting wire 1201 of wiring board 12 position department mount pad 5, LED lamp pearl mount pad 9 passes through wire and wiring board 12 electric connection, in the embodiment, wiring board 12 can make things convenient for solar cell 3 to supply power for LED lamp pearl mount pad 9, and can make things convenient for the electric connection of power connecting wire 1201, make LED lamp pearl mount pad 9 realize that two kinds of different powers supply power under the effect of wiring board 12.

Further, the central point department fixed mounting at transparent lamp shade 7 top has guide bar 702, and transparent lamp shade 7's inside wall fixed mounting has red lens 701, and in the embodiment, guide bar 702 can increase the effect of obstacle guide, and red lens 701 can turn into red with the light that LED lamp pearl 8 sent to the effect of obstacle indication has been improved.

Further, transparent lamp shade 7 is through four groups of fixed feet 6 fixed mounting of bottom four sides in four groups of mounting grooves 501 at mount pad 5 top, and fixed foot 6 passes through fixing bolt 601 and mount pad 5 fixed connection, and in the embodiment, fixed foot 6 can be installed in the mounting groove 501 at mount pad 5 top through fixing bolt 601 embedding to make things convenient for transparent lamp shade 7's dismouting.

Further, one side fixed mounting that unable adjustment base 2 is close to solar photovoltaic board 15 has wiring jack 13 with 3 electric connection of solar cell, and solar photovoltaic board 15 passes through solar panel connecting wire 14 and wiring jack 13 electric connection, fixed mounting has spacing supporting seat 1601 on the solar panel mounting bracket 16 of 15 low sides of solar photovoltaic board, and unable adjustment base 2's front has battery maintenance board 17 through bolt structure fixed mounting, in the embodiment, wiring jack 13 can make things convenient for solar photovoltaic board 15 to pass through the electric connection of solar panel connecting wire 14 with solar cell 3, thereby make things convenient for free connection and the disconnection of solar photovoltaic board 15 and solar cell 3.

The working principle is as follows: during the use, solar photovoltaic board 15 can be stored through solar battery 3 with the electric energy transformation with light energy under the sunless condition, connects external power supply's mode through solar battery 3 and power connecting wire 1201 to LED lamp pearl 8 provides the electric energy night.

It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Claims

1. The utility model provides a low light intensity aviation obstruction beacon of solar energy, includes unable adjustment base (2), its characterized in that: the solar energy storage battery (3) is installed in the fixing base (2) through a mounting pad, a mounting seat (5) is fixedly installed at the top of the fixing base (2), a heat conduction mounting seat (11) is fixedly installed in the fixing base (5), a heat conduction mounting frame (10) extending to the top of the mounting seat (5) is fixedly installed at the top of the heat conduction mounting seat (11), an LED lamp bead mounting base (9) is fixedly installed at the top of the heat conduction mounting frame (10), LED lamp beads (8) are uniformly installed at the top of the LED lamp bead mounting base (9), a transparent lampshade (7) is fixedly installed at the top of the mounting seat (5) outside the LED lamp beads (8), mounting bars (4) are fixedly installed on the front and the back of the top of the fixing base (2) through bolt structures, and a solar panel mounting frame (16) is fixedly installed at the end of the mounting bars (4), the top of the solar panel mounting frame (16) is fixedly provided with a solar photovoltaic panel (15).

2. The solar low-light-intensity aviation obstruction light of claim 1, wherein: the bottom of unable adjustment base (2) is fixed mounting has PMKD (1), and the four sides of PMKD (1) all fixed mounting have clamping screw (101).

3. The solar low-light-intensity aviation obstruction light of claim 1, wherein: the inside fixed mounting of heat conduction mount pad (11) has wiring board (12), and wiring board (12) pass through wire and solar cell (3) electric connection, and the positive fixedly connected with power connecting wire (1201) of wiring board (12) position department mount pad (5), LED lamp pearl mounting base (9) pass through wire and wiring board (12) electric connection.

4. The solar low-light-intensity aviation obstruction light of claim 1, wherein: the center position department fixed mounting at transparent lamp shade (7) top has guide bar (702), and the inside wall fixed mounting of transparent lamp shade (7) has red lens (701).

5. The solar low-light-intensity aviation obstruction light of claim 1, wherein: transparent lamp shade (7) are through four groups of fixed foot (6) fixed mounting of bottom four sides in four groups of mounting groove (501) at mount pad (5) top, and fixed foot (6) are through fixing bolt (601) and mount pad (5) fixed connection.

6. The solar low-light-intensity aviation obstruction light of claim 1, wherein: one side fixed mounting that unable adjustment base (2) are close to solar photovoltaic board (15) has wiring jack (13) with solar battery (3) electric connection, and solar photovoltaic board (15) pass through solar panel connecting wire (14) and wiring jack (13) electric connection, fixed mounting has spacing supporting seat (1601) on solar panel mounting bracket (16) of solar photovoltaic board (15) low side, and the front of unable adjustment base (2) has battery maintenance board (17) through bolt construction fixed mounting.