CN216047365U - Solar LED aviation warning lamp for high-altitude conducting wire - Google Patents
Solar LED aviation warning lamp for high-altitude conducting wire Download PDFInfo
- Publication number
- CN216047365U CN216047365U CN202122636490.2U CN202122636490U CN216047365U CN 216047365 U CN216047365 U CN 216047365U CN 202122636490 U CN202122636490 U CN 202122636490U CN 216047365 U CN216047365 U CN 216047365U
- Authority
- CN
- China
- Prior art keywords
- base
- clamping
- power transmission
- transmission line
- sides
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Non-Portable Lighting Devices Or Systems Thereof (AREA)
Abstract
The utility model discloses a solar energy LED aviation warning lamp for a high-altitude wire, which belongs to the technical field of aviation warning lamps and comprises a base and a lamp shade arranged on the top side of the base, wherein clamping components are connected to two sides of the lower end surface of the base in a sliding manner, the clamping components are fixed outside a power transmission line, pressing pieces for fixing the clamping components are arranged on two sides of the base, a mounting plate is arranged on the top side of the base through a supporting frame and is positioned inside the lamp shade, LED warning lamps and light-sensitive controllers distributed along the periphery are arranged on the top side of the mounting plate, and a solar panel is arranged between the mounting plate and the base.
Description
Technical Field
The utility model relates to the technical field of aviation warning lamps, in particular to a solar LED aviation warning lamp for a high-altitude wire.
Background
As is well known, in a power transmission system, a high-voltage wire is a very common power auxiliary device, and in order to avoid external damage during use, many high-voltage wires are generally erected at high altitude by using telegraph poles, but at night, because the high-voltage wire is dark in color, the high-voltage wire is easily dissolved in the night color and is not easily found by people, and great risk exists for aviation and related industries.
The aviation warning light that uses at present, the volume is great, meets under the influence of bad weather, and rocking of production can drive the electric wire and rock, and the security performance remains to be improved.
SUMMERY OF THE UTILITY MODEL
In order to overcome the defects of the prior art, the utility model aims to provide the solar aviation warning lamp which reduces the aviation potential safety hazard and has good stability and strong safety performance.
In order to achieve the purpose, the utility model adopts the following technical scheme:
the utility model provides a solar LED aviation warning lamp for a high-altitude wire, which comprises a base and a lamp shade arranged on the top side of the base, wherein clamping components are connected to two sides of the lower end surface of the base in a sliding manner, the clamping components are fixed outside a power transmission line, and pressing pieces for fixing the clamping components are arranged on two sides of the base;
the base top side is provided with the mounting panel through the supporting rack, the mounting panel is located inside the lamp shade, the top side of mounting panel is provided with along LED warning light and the light sense controller that distributes all around, the mounting panel with be provided with solar panel between the base.
The utility model has the preferable technical scheme that the clamping assembly comprises clamping parts which are in sliding connection with two sides of the lower end surface of the base, one side of each clamping part, which is close to the power transmission line, is provided with a clamping groove, and the inner wall of each clamping groove is provided with a plurality of groups of tooth parts which are mutually meshed with the outer part of the power transmission line.
The clamping assembly comprises a clamping component and a pressing component, wherein the clamping component is arranged on the clamping component, the pressing component comprises a movable part and a clamping rod piece, the movable part is rotatably connected with two sides of the base, the clamping rod piece is clamped on one side of the clamping component, a spring is connected to the outer wall of the movable part, and the other end of the spring is wound on the outer wall of the clamping rod piece and extends downwards.
The clamping rod piece is preferably provided with compression plates on the upper side and the lower side, and a locking bolt is arranged between the compression plates and the clamping assembly.
The utility model preferably adopts the technical scheme that the extending end of the other end of the spring is abutted against one side of the clamping part.
The utility model has the preferable technical scheme that an elastic connecting piece is arranged on the groove part of the base, and the other end of the elastic connecting piece is connected with a pressing part adaptive to the outer part of the power transmission line.
Compared with the prior art, the utility model has the beneficial effects that: according to the utility model, the clamping part is clamped at two sides of the power transmission line, the pressing part is pressed at one side of the power transmission line under the action of the elastic connecting piece, the clamping rod pieces at two sides are clamped at two sides of the clamping part under the action of the elastic force of the spring by rotating the clamping rod pieces at two sides, and meanwhile, pressure is applied to the clamping part, so that the clamping part firmly acts on the power transmission line, the clamping force of the clamping part on the power transmission line is improved, the stability of the clamping part is improved by the pressing force of the locking bolt and the pressing plate, the warning lamp is prevented from shaking under severe conditions in the process of high-altitude operation, and unnecessary potential safety hazards are reduced.
The solar aviation warning lamp provided by the utility model has the advantages of reduction of aviation potential safety hazards, good stability and strong safety performance.
Drawings
FIG. 1 is a schematic view of a solar aviation warning light of the present invention;
FIG. 2 is a schematic view of the mounting plate construction of the present invention;
FIG. 3 is a structural side view of the solar aviation warning light of the utility model.
In the drawings, the components represented by the respective reference numerals are listed below:
1. a base; 11. mounting a plate; 12. an LED warning light; 13. a light sensing controller; 14. a solar panel; 15. a groove part; 16. an elastic connecting member; 17. a pressing part; 2. a lamp shade; 3. a clamping assembly; 31. a clamping portion; 32. a clamping groove; 4. a compression member; 41. a movable portion; 42. clamping the rod piece; 43. a spring; 44. a compression plate; 45. locking the bolt; 5. and (4) a power transmission line.
Detailed Description
The technical scheme of the utility model is further explained by the specific implementation mode in combination with the attached drawings.
A solar LED aviation warning lamp for high-altitude wires comprises a base 1 and a lamp shade 2 installed on the top side of the base 1, wherein two sides of the lower end face of the base 1 are slidably connected with clamping components 3, the clamping components 3 are fixed outside a power transmission line 5, two sides of the base 1 are provided with pressing pieces 4 for fixing the clamping components 3, the top side of the base 1 is provided with a mounting plate 11 through a support frame, the mounting plate 11 is positioned inside the lamp shade 2, the top side of the mounting plate 11 is provided with LED warning lamps 12 and light sensing controllers 13 which are distributed along the periphery, a solar panel 14 is arranged between the mounting plate 11 and the base 1, the solar panel 14 absorbs light energy and stores the light energy in a storage battery on the bottom side of the mounting plate 11 so as to be used by the LED warning lamps 12, the clamping components 3 on two sides are installed on the power transmission line 5 and are pressed and fixed through the pressing pieces 4 on the two sides, under the cooperation of centre gripping subassembly 3 and pressing member 4, be fixed in the aviation warning light on power transmission line 5, small has, the swift advantage of installation, when encountering adverse weather, because the effect that two sides pressed member 4, make centre gripping subassembly 3 firmly hold power transmission line 5's outer wall all the time, guarantee the stability of aviation warning light, reduce the production of unnecessary potential safety hazard, the security of use improves, under the effect of light-sensitive controller 13, daytime LED warning light 12 does not take effect, when dark, through the work of light-sensitive controller 13 control LED warning light 12, prevent to cause the wasting of resources.
As a possible embodiment of the present disclosure, preferably, the clamping assembly 3 includes a clamping portion 31 slidably connected to two sides of the lower end surface of the base 1, a clamping groove 32 is disposed on one side of the clamping portion 31 close to the power transmission line 5, a plurality of sets of tooth portions mutually engaged with the outside of the power transmission line 5 are disposed on an inner wall of the clamping groove 32, and the tooth portions on the inner wall of the clamping groove 32 are engaged with the power transmission line 5, so that the clamping force and the clamping fixing effect of the clamping portion 31 on the power transmission line 5 can be better improved, the safety of high-altitude operation can be ensured, and the severe weather can be resisted.
As a possible implementation manner of this scheme, it is preferable, compress tightly piece 4 include with base 1 both sides rotate the movable part 41 of being connected and the joint in the joint member 42 of centre gripping subassembly 3 one side, the outer wall connection of movable part 41 has spring 43, the other end of spring 43 twine in the outer wall of joint member 42 to downwardly extending, through the spring action of spring 43, make joint member 42 act on clamping part 31 from both sides, make clamping part 31 exert pressure to power transmission line 5, firmly the centre gripping on power transmission line 5 to this makes solar energy aviation warning light install on power transmission line 5 steadily, avoids taking place to rock when suffering adverse conditions, influences the use and the safety of warning light.
As a possible implementation manner of this scheme, preferably, the upper and lower both sides of joint member 42 are provided with pressure strip 44, pressure strip 44 with install locking bolt 45 between clamping component 3, pressure strip 44 compresses tightly in clamping part 31 both sides under the spring action of spring 43 to strengthen the stability of clamping part 31 through locking bolt 45, further improve the fastness of clamping component 3 to the centre gripping of power transmission line 5, guarantee the safety and the stability of warning light installation.
As a possible embodiment of this solution, it is preferable that an extending end of the other end of the spring 43 abuts against one side of the clamping portion 31, so that the clamping rod 42 is clamped on one side of the clamping portion 31 under the action of elastic force and acts on the clamping portion 31, thereby increasing the clamping force of the clamping portion 31 on the power transmission line 5 to ensure the safety of the warning light.
As a possible implementation manner of the present solution, it is preferable that the groove portion 15 of the base 1 is installed with an elastic connection member 16, the other end of the elastic connection member 16 is connected with a pressing portion 17 adapted to the outside of the power transmission line 5, during installation, the power transmission line 5 presses the pressing portion 17 to move upwards, so that the elastic connection member 16 is pressed, after the installation is completed, the elastic connection member 16 presses the pressing portion 17 to the power transmission line 5 according to the working principle that the force is applied to each other, and the warning light is stabilized from the vertical direction and the horizontal direction in cooperation with the clamping assemblies 3 on both sides.
While the utility model has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the spirit and scope of the utility model. The present invention is not to be limited by the specific embodiments disclosed herein, and other embodiments that fall within the scope of the claims of the present application are intended to be within the scope of the present invention.
Claims (6)
1. The utility model provides a solar energy LED aviation warning light for high altitude wire which characterized in that: the device comprises a base (1) and a lampshade (2) arranged on the top side of the base (1), wherein clamping assemblies (3) are connected to two sides of the lower end face of the base (1) in a sliding mode, the clamping assemblies (3) are fixed outside a power transmission line (5), and pressing pieces (4) used for fixing the clamping assemblies (3) are arranged on two sides of the base (1);
base (1) top side is provided with mounting panel (11) through the supporting rack, mounting panel (11) are located inside lamp shade (2), the top side of mounting panel (11) is provided with along LED warning light (12) and light sense controller (13) that distribute all around, mounting panel (11) with be provided with solar panel (14) between base (1).
2. The solar LED aviation warning lamp for the overhead conductor of claim 1, which is characterized in that:
the clamping assembly (3) comprises clamping portions (31) which are in sliding connection with two sides of the lower end face of the base (1), a clamping groove (32) is formed in one side, close to the power transmission line (5), of each clamping portion (31), and a plurality of groups of tooth portions meshed with the outer portion of the power transmission line (5) are arranged on the inner wall of each clamping groove (32).
3. The solar LED aviation warning lamp for the overhead conductor of claim 1, which is characterized in that:
compress tightly piece (4) include with base (1) both sides rotate movable part (41) and the joint of connecting in joint member piece (42) of centre gripping subassembly (3) one side, the outer wall connection of movable part (41) has spring (43), the other end of spring (43) twine in the outer wall of joint member piece (42) to downwardly extending.
4. The solar LED aviation warning lamp for the overhead conductor of claim 3, wherein:
the upper side and the lower side of the clamping rod piece (42) are provided with pressing plates (44), and locking bolts (45) are installed between the pressing plates (44) and the clamping assemblies (3).
5. The solar LED aviation warning lamp for the overhead conductor of claim 3, wherein:
the extending end of the other end of the spring (43) is abutted against one side of the clamping part (31).
6. The solar LED aviation warning lamp for the overhead conductor of claim 1, which is characterized in that:
an elastic connecting piece (16) is installed on the groove portion (15) of the base (1), and the other end of the elastic connecting piece (16) is connected with a pressing portion (17) matched with the outside of the power transmission line (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122636490.2U CN216047365U (en) | 2021-10-29 | 2021-10-29 | Solar LED aviation warning lamp for high-altitude conducting wire |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122636490.2U CN216047365U (en) | 2021-10-29 | 2021-10-29 | Solar LED aviation warning lamp for high-altitude conducting wire |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216047365U true CN216047365U (en) | 2022-03-15 |
Family
ID=80612755
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122636490.2U Active CN216047365U (en) | 2021-10-29 | 2021-10-29 | Solar LED aviation warning lamp for high-altitude conducting wire |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216047365U (en) |
-
2021
- 2021-10-29 CN CN202122636490.2U patent/CN216047365U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108075718B (en) | Solar cell aluminum alloy frame convenient to installation | |
| CN218274213U (en) | Dry-type transformer with coil compact structure | |
| CN216047365U (en) | Solar LED aviation warning lamp for high-altitude conducting wire | |
| CN102881742B (en) | A kind of press-loading apparatus of solar energy photovoltaic panel | |
| CN211509152U (en) | Automatic climbing device for monitoring camera | |
| CN210838879U (en) | Mountain region circuit environment-friendly suspension clamp | |
| CN210157117U (en) | Installation interlock anchor clamps for various steel tile roof photovoltaic support are exclusively used in | |
| CN209071828U (en) | A kind of power distribution cabinet rain-proof equipment for outdoor | |
| CN208548853U (en) | A kind of photovoltaic module briquetting mounting structure | |
| CN108599690B (en) | Photovoltaic power generation device | |
| CN211579407U (en) | Aerial transmission line jumper wire and hook wire clamp mounting tool | |
| CN206650624U (en) | Double glass photovoltaic module erecting devices | |
| CN208469683U (en) | A kind of new-energy automobile intelligence favour management system terminal being easily installed | |
| CN201825167U (en) | Motorcycle relay device | |
| CN213402395U (en) | Cable adapter for electric power engineering | |
| CN112103680A (en) | Protector for power line worker | |
| CN219553645U (en) | Integrated circuit board for photovoltaic cell assembly | |
| CN221227346U (en) | Clamping structure of inverter | |
| CN218386386U (en) | Transformer substation support earthing device | |
| CN208025066U (en) | A kind of television set electric up-down mounting bracket | |
| CN203032543U (en) | Connecting structure component of automobile rearview mirror body and installation arms | |
| CN212258862U (en) | Wall ladder type solar photovoltaic power generation device | |
| CN208527870U (en) | A kind of stamping die producing stud | |
| CN204441506U (en) | Earth connection automatic clamping device | |
| CN219874195U (en) | Novel waterproof power connecting wire |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |