CN212456662U

CN212456662U - Durable solar energy aviation lamp of rotation

Info

Publication number: CN212456662U
Application number: CN202021572237.4U
Authority: CN
Inventors: 宋红雨
Original assignee: Baoding Tianshan Electric Technology Dev Co ltd
Current assignee: Baoding Tianshan Electric Technology Dev Co ltd
Priority date: 2020-08-02
Filing date: 2020-08-02
Publication date: 2021-02-02
Anticipated expiration: 2030-08-02

Abstract

The utility model discloses a rotary durable solar energy aviation lamp, which comprises a base and an adjusting structure, wherein a cavity is arranged in a fixed seat, a telescopic cylinder B is fixedly arranged in the cavity, an operator can drive a support plate and a lamp component to adjust the vertical direction by utilizing a switch, the flying direction can be conveniently guided in the directions with different heights, a protective layer is arranged on the inner wall of the lamp shade, the lamp shade can be protected, the durability of the lamp shade is improved, a loud-speaking structure is fixedly arranged on one side of the fixed seat, the operator can make the loud-speaking structure sound by utilizing the switch, flying birds can be conveniently repelled by utilizing sound, the phenomenon that the lamp component is damaged by mistakenly hitting the lamp component is avoided, the influence on the guiding work is influenced, a protective cover is fixedly arranged at the upper end of the loud-speaking structure, the rain shielding and the like can be carried, the normal use of the loudspeaking structure is prevented from being influenced by the infiltration of rainwater.

Description

Durable solar energy aviation lamp of rotation

Technical Field

The utility model relates to an aviation lamp technical field specifically is a durable type solar energy aviation lamp of rotation.

Background

Aviation lamps, which are traditionally light-guiding systems, are mainly used to guide objects or paths by means of lights depending on the related control system, and are mainly used to guide the flight trajectory of an aerial vehicle or the flight direction as one of the applications.

Aviation lamp mainly used high-rise building roof, airport etc. ground, for aircraft direction or height, but when utilizing aviation lamp to guide, general position is comparatively fixed, can only use at same height, and in the use, probably have the flight birds to hit aviation lamp for lamps and lanterns are impaired, reduce life.

To the problem, the utility model provides a durable type solar energy aviation lamp of rotation.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a durable solar energy aviation lamp of rotation possesses the height that can adjust lamp components, is convenient for guide, and can utilize sound to drive birds, protects effectual advantage to the problem in the background art has been solved.

In order to achieve the above object, the utility model provides a following technical scheme: a rotary durable solar aviation lamp comprises a base and an adjusting structure, wherein the adjusting structure is arranged at the upper end of the base, the base comprises a fixed seat, a supporting plate, a lamp component, a loudspeaking structure and a protective cover, the fixed seat is arranged at the upper end of the base, the supporting plate is arranged at the upper end of the fixed seat, the lamp component is fixedly arranged at the upper end of the supporting plate, the loudspeaking structure is arranged on one side of the fixed seat, and the protective cover is fixedly arranged at the upper end of the loudsp;

the adjusting structure comprises a support column, a telescopic cylinder A, a placing plate and a solar panel, the support column is fixedly installed at the upper end of the base, the telescopic cylinder A is arranged on one side of the support column, the placing plate is arranged at the upper ends of the support column and the telescopic cylinder A, and the solar panel is fixedly installed at the upper end of the placing plate.

Preferably, the fixing base includes cavity and telescopic cylinder B, and the cavity is seted up in the inside of fixing base, and telescopic cylinder B sets up in the inside of cavity, and has the backup pad at telescopic cylinder B's upper end fixed mounting.

Preferably, the lamp assembly comprises a mounting seat and a lamp body, the mounting seat is fixedly mounted at the upper end of the supporting plate, and the lamp body is arranged at the upper end of the mounting seat.

Preferably, the lamp body includes lamp shade, lamp pearl and protective layer, and the lamp shade setting is in the upper end of mount pad, and the lamp pearl sets up the inside at the lamp shade, and the protective layer setting is at the inner wall of lamp shade.

Preferably, the placing plate comprises a connecting plate, an elastic piece and a clamping block, the connecting plate is arranged on one side of the placing plate, the elastic piece is arranged at the upper end of the connecting plate, and the clamping block is arranged at the upper end of the elastic piece.

Preferably, the upper surface of the solar panel is provided with two groups of clamping grooves which are matched with the clamping blocks.

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

1. the utility model provides a pair of durable solar energy aviation lamp of rotation has seted up the cavity in the inside of fixing base, and telescopic cylinder B fixed mounting can make telescopic cylinder B drive backup pad and lamps and lanterns subassembly carry out the adjustment of vertical direction through utilizing the switch in the inside of cavity, is convenient for guide the flight direction in the direction of co-altitude not, and is provided with the protective layer at the inner wall of lamp shade, can protect the lamp shade, improves the durability of lamp shade.

2. The utility model provides a pair of durable solar energy aviation lamp of rotation has the structure of raising one's voice at one side fixed mounting of fixing base, and operating personnel can make the structure of raising one's voice through utilizing the switch to carry out the sound production, utilizes sound to be convenient for drive flight birds, avoids birds mistake to hit lamp subassembly and makes lamp subassembly impaired, and the work is guided in the influence, and has the protection casing in the upper end fixed mounting of the structure of raising one's voice, can hide rain etc. to the structure of raising one's voice, avoids the rainwater infiltration to influence the normal use of the structure of raising.

3. The utility model provides a pair of durable solar energy aviation lamp of rotation, one side of placing the board is provided with the connecting plate, the fixture block sets up the upper end at the elastic component, and fixture block and draw-in groove phase-match, elasticity through utilizing the elastic component, can make the fixture block fix the inside of placing at the draw-in groove, thereby fix solar panel, the lower extreme of placing the board is provided with support column and telescopic cylinder A simultaneously, utilize the switch to make telescopic cylinder A stretch out and draw back, thereby can adjust the angle of placing the board slope, solar panel of being convenient for absorbs solar energy, excellent in use effect.

Drawings

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

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

fig. 3 is a front view of the overall structure of the present invention;

fig. 4 is a schematic structural view of a solar panel according to the present invention;

fig. 5 is an enlarged view of a portion a in fig. 4 according to the present invention.

In the figure: 1. a base; 11. a fixed seat; 111. a cavity; 112. a telescopic cylinder B; 12. a support plate; 13. a lamp assembly; 131. a mounting seat; 132. a lamp body; 1321. a lamp shade; 1322. a lamp bead; 1323. a protective layer; 14. a speaker structure; 15. a protective cover; 2. adjusting the structure; 21. a support pillar; 22. a telescopic cylinder A; 23. placing the plate; 231. a connecting plate; 232. an elastic member; 233. a clamping block; 24. a solar panel; 241. a clamping groove.

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, a rotary durable solar aircraft lamp comprises a base 1 and an adjusting structure 2, wherein the adjusting structure 2 is arranged at the upper end of the base 1, the base 1 comprises a fixed seat 11, a supporting plate 12, a lamp assembly 13, a speaker structure 14 and a protective cover 15, the fixed seat 11 is arranged at the upper end of the base 1, the supporting plate 12 is arranged at the upper end of the fixed seat 11, the lamp assembly 13 is fixedly arranged at the upper end of the supporting plate 12, the speaker structure 14 is arranged at one side of the fixed seat 11, and the protective cover 15 is fixedly arranged at the upper end of the speaker structure 14; an operator can enable the loudspeaking structure 14 to produce sound by using the switch, flying birds can be driven by using the sound, the situation that the lamp assembly 13 is damaged due to the fact that the birds accidentally hit the lamp assembly 13 to influence guiding work is avoided, a protective cover 15 is fixedly installed at the upper end of the loudspeaking structure 14, rain shielding and the like can be carried out on the loudspeaking structure 14, and the situation that rainwater infiltrates to influence normal use of the loudspeaking structure 14 is avoided; the adjusting structure 2 comprises a supporting column 21, a telescopic cylinder A22, a placing plate 23 and a solar panel 24, wherein the supporting column 21 is fixedly installed at the upper end of the base 1, the telescopic cylinder A22 is arranged at one side of the supporting column 21, the placing plate 23 is arranged at the upper ends of the supporting column 21 and the telescopic cylinder A22, and the solar panel 24 is fixedly installed at the upper end of the placing plate 23.

Referring to fig. 2 and 3, the fixing base 11 includes a cavity 111 and a telescopic cylinder B112, the cavity 111 is disposed inside the fixing base 11, the telescopic cylinder B112 is disposed inside the cavity 111, and a supporting plate 12 is fixedly mounted at an upper end of the telescopic cylinder B112; the lamp assembly 13 comprises a mounting seat 131 and a lamp body 132, the mounting seat 131 is fixedly mounted at the upper end of the support plate 12, and the lamp body 132 is arranged at the upper end of the mounting seat 131; the lamp body 132 comprises a lampshade 1321, lamp beads 1322 and a protective layer 1323, the lampshade 1321 is arranged at the upper end of the mounting seat 131, the lamp beads 1322 are arranged inside the lampshade 1321, and the protective layer 1323 is arranged on the inner wall of the lampshade 1321; cavity 111 has been seted up in the inside of fixing base 11, telescopic cylinder B112 fixed mounting is in the inside of cavity 111, and operating personnel can make telescopic cylinder B112 drive backup pad 12 and lamp subassembly 13 carry out the adjustment of vertical direction through utilizing the switch, is convenient for guide the flight direction in the direction of co-altitude not, and is provided with protective layer 1323 at the inner wall of lamp shade 1321, can protect lamp shade 1321, improves lamp shade 1321's durability.

Referring to fig. 4 and 5, the placing plate 23 includes a connecting plate 231, an elastic member 232 and a latch 233, the connecting plate 231 is disposed at one side of the placing plate 23, the elastic member 232 is disposed at an upper end of the connecting plate 231, and the latch 233 is disposed at an upper end of the elastic member 232; the upper surface of the solar panel 24 is provided with two groups of clamping grooves 241, and the clamping grooves 241 are matched with the clamping blocks 233; be provided with connecting plate 231 in the one side of placing board 23, fixture block 233 sets up the upper end at elastic component 232, and fixture block 233 and draw-in groove 241 phase-match, through utilizing the elasticity of elastic component 232, can make the fixed inside of placing at draw-in groove 241 of fixture block 233, thereby fix solar panel 24, be provided with support column 21 and telescopic cylinder A22 at the lower extreme of placing board 23 simultaneously, utilize the switch to make telescopic cylinder A22 stretch out and draw back, thereby can adjust the angle of placing board 23 slope, solar panel 24 absorbs the solar energy of the sun of being convenient for, excellent in use effect.

In summary, the following steps: the rotary durable solar aviation lamp is characterized in that a cavity 111 is formed in a fixed seat 11, a telescopic cylinder B112 is fixedly installed in the cavity 111, an operator can drive a support plate 12 and a lamp component 13 to adjust the vertical direction by using a switch, so that the flight direction can be guided in the directions of different heights, a protective layer 1323 is arranged on the inner wall of a lampshade 1321, the lampshade 1321 can be protected, the durability of the lampshade 1321 is improved, a loudspeaker structure 14 is fixedly installed on one side of the fixed seat 11, the loudspeaker structure 14 can sound by using the switch, flying birds can be driven by using sound, the situation that the lamp component 13 is damaged due to the fact that the birds collide with the lamp component 13 by mistake and the guiding work is influenced is avoided, a protective cover 15 is fixedly installed at the upper end of the loudspeaker structure 14, and the loudspeaker structure 14 can be shielded from rain and the like, avoid rainwater infiltration to influence the normal use of structure 14 of raising one's voice, one side of placing board 23 is provided with connecting plate 231, fixture block 233 sets up the upper end at elastic component 232, and fixture block 233 and draw-in groove 241 phase-match, elasticity through utilizing elastic component 232, can make fixture block 233 fix the inside of placing at draw-in groove 241, thereby fix solar panel 24, the lower extreme of placing board 23 is provided with support column 21 and telescopic cylinder A22 simultaneously, utilize the switch can make telescopic cylinder A22 stretch out and draw back, thereby can adjust the angle of placing board 23 slope, solar panel 24 of being convenient for absorbs solar energy, excellent in use effect.

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. The utility model provides a durable solar energy aviation lamp of rotation, includes base (1) and adjustment structure (2), and adjustment structure (2) set up the upper end at base (1), its characterized in that: the base (1) comprises a fixed seat (11), a supporting plate (12), a lamp assembly (13), a loudspeaking structure (14) and a protective cover (15), wherein the fixed seat (11) is arranged at the upper end of the base (1), the supporting plate (12) is arranged at the upper end of the fixed seat (11), the lamp assembly (13) is fixedly arranged at the upper end of the supporting plate (12), the loudspeaking structure (14) is arranged on one side of the fixed seat (11), and the protective cover (15) is fixedly arranged at the upper end of the loudspeaking structure (14);

the adjusting structure (2) comprises a supporting column (21), a telescopic cylinder A (22), a placing plate (23) and a solar panel (24), wherein the supporting column (21) is fixedly installed at the upper end of the base (1), the telescopic cylinder A (22) is arranged on one side of the supporting column (21), the placing plate (23) is arranged at the upper ends of the supporting column (21) and the telescopic cylinder A (22), and the solar panel (24) is fixedly installed at the upper end of the placing plate (23).

2. The revolving durable solar aircraft light of claim 1, wherein: fixing base (11) include cavity (111) and telescopic cylinder B (112), and the inside at fixing base (11) is seted up in cavity (111), and telescopic cylinder B (112) set up in the inside of cavity (111), and have backup pad (12) in telescopic cylinder B's (112) upper end fixed mounting.

3. The revolving durable solar aircraft light of claim 1, wherein: the lamp component (13) comprises a mounting seat (131) and a lamp body (132), the mounting seat (131) is fixedly mounted at the upper end of the supporting plate (12), and the lamp body (132) is arranged at the upper end of the mounting seat (131).

4. The revolving durable solar aircraft lamp as claimed in claim 3, wherein: the lamp body (132) comprises a lampshade (1321), lamp beads (1322) and a protective layer (1323), the lampshade (1321) is arranged at the upper end of the mounting seat (131), the lamp beads (1322) are arranged inside the lampshade (1321), and the protective layer (1323) is arranged on the inner wall of the lampshade (1321).

5. The revolving durable solar aircraft light of claim 1, wherein: the placing plate (23) comprises a connecting plate (231), an elastic piece (232) and a clamping block (233), the connecting plate (231) is arranged on one side of the placing plate (23), the elastic piece (232) is arranged at the upper end of the connecting plate (231), and the clamping block (233) is arranged at the upper end of the elastic piece (232).

6. The revolving durable solar aircraft light of claim 1, wherein: the upper surface of the solar panel (24) is provided with two groups of clamping grooves (241), and the clamping grooves (241) are matched with the clamping blocks (233).