CN213599273U

CN213599273U - Solar helicopter airport lamp beacon

Info

Publication number: CN213599273U
Application number: CN202023264762.2U
Authority: CN
Inventors: 唐学兵
Original assignee: Dongguan Tianxiang Aerospace Technology Co ltd
Current assignee: Dongguan Tianxiang Aerospace Technology Co ltd
Priority date: 2020-12-29
Filing date: 2020-12-29
Publication date: 2021-07-02
Anticipated expiration: 2030-12-29

Abstract

The utility model discloses a solar energy heliport beacon, including motor casing and hot plate, motor casing's internally mounted has motor body, and motor body's top is provided with the gear train, the power supply box is installed to the top of gear train, and the below of power supply box is provided with the ball, the casing apron is installed to motor casing's outside front end, one side of power supply box is fixed with the bulb pole. This solar energy heliport beacon compares with current ordinary solar energy heliport beacon, humidity sensor can the humidity in this solar energy heliport beacon of real-time supervision, when humidity was too high, the hot plate can heat this solar energy heliport beacon, melt the frost fog attached to on the lens, reach the effect of defrosting defogging, avoid lens frosting fog to influence this solar energy heliport beacon's use, this solar energy heliport beacon has the characteristics that the defrosting fog effect is obvious, suitable in the environment that humidity is great, easily produce the water smoke and use.

Description

Solar helicopter airport lamp beacon

Technical Field

The utility model relates to an airport lamp mark technical field specifically is solar energy heliport lamp mark.

Background

The airport beacon is one of airport navigation aid lamps, is generally arranged in civil airports, military airports, helicopters or helicopter parking aprons, is provided with different luminous intensities, different flash frequencies and different luminous colors according to different differences of using airports and is used for marking the position of the airports or the helicopter parking aprons, and the solar helicopter airport beacon is also one of the airport beacons.

Current solar energy heliport light beacon function singleness, simple structure does not possess the function of defrosting fog and dehumidification, when meetting the heavier environment of moisture, and solar energy heliport light beacon outside has frosty fog easily, and solar energy heliport light beacon can't exert complete performance, the user demand of satisfying people that can not be fine, to above-mentioned condition, carries out technical innovation on current solar energy heliport light beacon basis.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a solar energy heliport lamp mark to propose general solar energy heliport lamp mark function singleness in solving above-mentioned background art, simple structure does not possess the function of defrosting fog and dehumidification, when meetting the heavier environment of moisture, the solar energy heliport lamp mark outside becomes frosty fog easily, the unable complete performance of solar energy heliport lamp mark, the not fine user demand problem that satisfies people.

In order to achieve the above object, the utility model provides a following technical scheme: solar energy heliport beacon, including motor casing and hot plate, the internally mounted of motor casing has motor body, and motor body's top is provided with the gear train, the power supply box is installed to the top of gear train, and the below of power supply box is provided with the ball, the casing apron is installed to motor casing's outside front end, one side of power supply box is fixed with the bulb pole, and the externally mounted of bulb pole has concave bulb piece, the externally fixed of concave bulb piece has solar panel, the top of power supply box is provided with the recess seat, the inside of recess seat is fixed with the sealing washer, and the outside of sealing washer is provided with the lamp shade, LED luminescence unit is installed to the outside below of recess seat, the hot plate is located the inboard of lamp shade, lens are installed to the outside top of lamp shade, and the below of lens is provided with humidity transducer.

Preferably, the motor housing and the power box form a rotating structure through balls, and the balls are arranged along the circumference of the center of the circle of the motor housing.

Preferably, the ball head rod is movably connected with the concave ball head block, and the concave ball head block and the solar panel form a welding integrated structure.

Preferably, the groove seat is fixedly connected with the sealing ring, and the inner surface of the sealing ring is tightly attached to the outer surface of the lampshade.

Preferably, be fixed connection between hot plate and the lamp shade, and the axis of hot plate coincides mutually with the axis of lamp shade.

Preferably, be fixed connection between lens and the humidity transducer, and the axis of lens coincides mutually with the axis of lamp shade.

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

1. the utility model discloses a motor casing, motor body, gear train, power supply box, ball, casing apron, bulb pole, concave bulb piece and solar panel's setting for this solar energy heliport beacon possesses revolution mechanic and angle modulation structure, can adjust solar panel, and solar panel can autogiration, and real-time rotatory absorption sun illumination, thereby let solar panel can better absorption solar energy, improved the efficiency of solar panel work;

2. the solar helicopter field light beacon has a multi-sealing structure through the arrangement of the groove seat and the sealing ring, the sealing ring is attached to the joint of the parts of the solar helicopter field light beacon, and the special parts are sealed by matching the groove with the sealing ring, so that the solar helicopter field light beacon cannot have the conditions of water seepage and the like even in long-time use;

3. the utility model discloses a setting of hot plate and humidity transducer, humidity transducer can the humidity in this solar energy heliport beacon of real-time supervision, when humidity is too high, the hot plate can heat this solar energy heliport beacon, melt the frost fog of adhering to on the lens, reach the effect of defrosting defogging, avoid lens frosting fog to influence this solar energy heliport beacon's use, the characteristics that this solar energy heliport beacon has are that defrosting fog effect is obvious, it is great to suit at humidity, use in the environment of easy production water smoke.

Drawings

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

FIG. 2 is a schematic view of the structure of the present invention;

fig. 3 is an enlarged schematic view of a portion a in fig. 1 according to the present invention.

In the figure: 1. a motor housing; 2. a motor body; 3. a gear set; 4. a power supply box; 5. a ball bearing; 6. a housing cover plate; 7. a ball-head rod; 8. a concave ball head block; 9. a solar panel; 10. a groove seat; 11. a seal ring; 12. a lamp shade; 13. an LED light emitting unit; 14. heating plates; 15. a lens; 16. a humidity sensor.

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. 1-3, the present invention provides a technical solution: a solar heliport beacon comprises a motor shell 1 and a heating plate 14, wherein a motor body 2 is installed inside the motor shell 1, a gear set 3 is arranged above the motor body 2, a power supply box 4 is installed above the gear set 3, balls 5 are arranged below the power supply box 4, the motor shell 1 and the power supply box 4 form a rotating structure through the balls 5, the balls 5 are arranged along the circumference of the circle center of the motor shell 1, a shell cover plate 6 is installed at the front end of the outer portion of the motor shell 1, a ball rod 7 is fixed on one side of the power supply box 4, a concave ball head block 8 is installed on the outer portion of the ball rod 7, the ball rod 7 is movably connected with the concave ball head block 8, a welding integrated structure is formed between the concave ball head block 8 and the solar panel 9, a solar panel 9 is fixed on the outer portion of the concave ball head block 8, and a solar panel 9 is fixed on the outer portion of the motor, The arrangement of the balls 5, the shell cover plate 6, the ball head rod 7, the concave ball head block 8 and the solar panel 9 enables the solar heliport beacon to have a rotating structure and an angle adjusting structure, the solar panel 9 can be adjusted, the solar panel 9 can automatically rotate, and the solar panel 9 can rotate in real time to absorb solar light, so that the solar panel 9 can better absorb solar energy, and the working efficiency of the solar panel 9 is improved;

a groove seat 10 is arranged above the power box 4, a sealing ring 11 is fixed inside the groove seat 10, a lampshade 12 is arranged outside the sealing ring 11, the groove seat 10 is fixedly connected with the sealing ring 11, the inner surface of the sealing ring 11 is tightly attached to the outer surface of the lampshade 12, the solar helicopter airport lamp beacon is provided with a multi-sealing structure through the arrangement of the groove seat 10 and the sealing ring 11, the sealing ring 11 is attached to the joint of parts of the solar helicopter airport lamp beacon, and the special parts are sealed by matching the groove with the sealing ring 11, so that the solar helicopter airport lamp beacon cannot leak water and the like when being used for a long time;

the LED light-emitting unit 13 is installed below the outer portion of the groove seat 10, the heating plate 14 is located on the inner side of the lampshade 12, the heating plate 14 is fixedly connected with the lampshade 12, the central axis of the heating plate 14 is coincident with the central axis of the lampshade 12, the lens 15 is installed above the outer portion of the lampshade 12, the humidity sensor 16 is arranged below the lens 15, the lens 15 is fixedly connected with the humidity sensor 16, the central axis of the lens 15 is coincident with the central axis of the lampshade 12, through the arrangement of the heating plate 14 and the humidity sensor 16, the humidity sensor 16 can monitor the humidity in the solar helicopter field beacon in real time, when the humidity is too high, the heating plate 14 can heat the solar helicopter field beacon to melt frost attached to the lens 15, the defrosting and demisting effects are achieved, and the frost and fog of the lens 15 are prevented from forming to influence the use of the solar helicopter field beacon, the solar helicopter airport beacon has the characteristics of obvious defrosting fog effect and suitability for being used in an environment with high humidity and easy water fog generation.

The working principle is as follows: when the solar heliport beacon is used, firstly, a motor body 2 arranged inside a motor shell 1 is started, the motor body 2 drives a power supply box 4 to rotate through a gear set 3, a bulb rod 7 is welded on one side of the power supply box 4, a concave bulb block 8 fixed outside a solar panel 9 is movably connected with the bulb rod 7, so that the angle and the direction of the solar panel 9 are adjusted, the solar panel 9 can better absorb solar energy, the power supply box 4 is used for storing electricity of the solar panel 9 and supplying power to the solar heliport beacon, a groove seat 10 is arranged on the power supply box 4, a lampshade 12 is arranged in a groove of the groove seat 10, the sealing performance is enhanced by matching with a sealing ring 11, a plurality of sealing rings 11 are attached to the connection position of parts, so that the solar heli port beacon cannot have water seepage and the like even in long-time use, when frost is formed outside a lens 15 or moisture exists inside the solar heliport beacon, the heating plate 14 heats the lamp housing 12 to remove frost on the outer surface of the lens 15 and moisture inside the lamp housing 12, and the humidity sensor 16 installed below the lens 15 monitors the moisture inside the solar heliport beacon in real time, which is the working principle of the solar heliport beacon.

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. Solar energy heliport beacon, including motor casing (1) and hot plate (14), its characterized in that: the motor shell is characterized in that a motor body (2) is mounted inside the motor shell (1), a gear set (3) is arranged above the motor body (2), a power box (4) is mounted above the gear set (3), balls (5) are arranged below the power box (4), a shell cover plate (6) is mounted at the front end of the outer portion of the motor shell (1), a ball head rod (7) is fixed to one side of the power box (4), a concave ball head block (8) is mounted outside the ball head rod (7), a solar panel (9) is fixed to the outer portion of the concave ball head block (8), a groove seat (10) is arranged above the power box (4), a sealing ring (11) is fixed to the inner portion of the groove seat (10), a lampshade (12) is arranged outside the sealing ring (11), and an LED light-emitting unit (13) is mounted below the outer portion of the groove seat (10), the heating plate (14) is located on the inner side of the lampshade (12), a lens (15) is installed above the outer portion of the lampshade (12), and a humidity sensor (16) is arranged below the lens (15).

2. The solar heliport beacon of claim 1, characterized in that: the motor shell (1) and the power box (4) form a rotating structure through the balls (5), and the balls (5) are arranged along the circle center circumference of the motor shell (1).

3. The solar heliport beacon of claim 1, characterized in that: the ball head rod (7) is movably connected with the concave ball head block (8), and a welding integrated structure is formed between the concave ball head block (8) and the solar panel (9).

4. The solar heliport beacon of claim 1, characterized in that: the groove seat (10) is fixedly connected with the sealing ring (11), and the inner surface of the sealing ring (11) is tightly attached to the outer surface of the lampshade (12).

5. The solar heliport beacon of claim 1, characterized in that: the heating plate (14) is fixedly connected with the lampshade (12), and the central axis of the heating plate (14) coincides with the central axis of the lampshade (12).

6. The solar heliport beacon of claim 1, characterized in that: be fixed connection between lens (15) and humidity transducer (16), and the axis of lens (15) and the axis of lamp shade (12) coincide mutually.