CN212456667U - Embedded novel environmental protection aviation lamp - Google Patents
Embedded novel environmental protection aviation lamp Download PDFInfo
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- CN212456667U CN212456667U CN202021583872.2U CN202021583872U CN212456667U CN 212456667 U CN212456667 U CN 212456667U CN 202021583872 U CN202021583872 U CN 202021583872U CN 212456667 U CN212456667 U CN 212456667U
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Abstract
The utility model discloses an embedded novel environment-friendly aviation lamp, which comprises a power supply mechanism, a connecting mechanism and an illuminating mechanism, wherein the connecting mechanism is arranged on the upper surface of the power supply mechanism, the illuminating mechanism is arranged inside the upper end of the connecting mechanism, an electrode groove is arranged at the bottom of a connecting pipe, a lamp body is electrically connected with a storage battery through pins and the electrode groove, an embedded structure is arranged between the lamp body and the connecting pipe, the lamp body can be conveniently replaced, an annular inclined structure is arranged at the upper end of a sealing layer, the lamp body can be conveniently calibrated and embedded, the lamp body is tightly attached to the sealing layer, the rainwater is prevented from invading, when the embedded installation is carried out, the gas inside the connecting pipe is discharged from a through hole, after the installation is finished, the through hole is blocked through the sealing bolt, the stability between the lamp body and the connecting pipe is enhanced by utilizing the vacuum pressure difference, and, the connecting block of being convenient for blocks up the through-hole, need not carry out calibration work.
Description
Technical Field
The utility model relates to an aviation lamp technical field specifically is an embedded novel environmental protection aviation lamp.
Background
The traditional light guiding system mainly depends on a related control system, and guides a target or a path through light, and the aviation light is an application of the light guiding system, and is mainly used for guiding the flight track of an air aircraft or guiding the flight direction.
Present aviation lamp generally sets up in the high altitude, and maintainer need regularly carry out troubleshooting and change to the aviation lamp, but present aviation lamp is generally that lamp body and base be integral structure now, through the bolt fastening and carry out electric connection to and the problem of the lamp body change operation that the troubleshooting of maintainer and be not convenient for.
To solve the above problems. Therefore, an embedded novel environment-friendly aviation lamp is provided.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an embedded novel environmental protection aviation lamp to having solved among the prior art aviation lamp and generally having set up in the high altitude, maintainer need regularly carry out troubleshooting and change to the aviation lamp, but present aviation lamp generally is lamp body and base structure as an organic whole, carries out electric connection through the bolt fastening, and the problem of the lamp body change operation that the troubleshooting of maintainer and be not convenient for reached is carried out to it.
In order to achieve the above object, the utility model provides a following technical scheme: an embedded novel environment-friendly aviation lamp comprises a power supply mechanism, a connecting mechanism and a lighting mechanism, wherein the connecting mechanism is arranged on the upper surface of the power supply mechanism, the lighting mechanism is arranged inside the upper end of the connecting mechanism, the power supply mechanism comprises a solar panel and a storage battery, and the solar panel is arranged on one side of the storage battery;
the connecting mechanism comprises a fixing plate, a bolt, a fixing piece, a connecting pipe and a sealing layer, wherein the fixing plate is arranged on the upper surface of the storage battery through the bolt, the connecting pipe is arranged on the upper surface of the fixing plate, the fixing piece is arranged on the periphery of the connecting pipe, and the sealing layer is bonded on the inner wall of the connecting pipe;
the lighting mechanism comprises a lamp body and pins, the pins are arranged at the lower end of the lamp body, and the lower end of the lamp body is arranged in the connecting pipe.
Preferably, the solar panel is electrically connected with the storage battery.
Preferably, the fixing part comprises a connecting block and a sealing bolt, the connecting block is arranged on the periphery of the connecting pipe, and the sealing bolt is arranged on the upper surface of the connecting block.
Preferably, a dovetail groove is formed in the inner portion of the upper surface of the connecting block, a dovetail block is arranged on the lower surface of the sealing bolt, and the connecting block and the sealing bolt are in sliding connection.
Preferably, the inner wall of the connecting pipe is provided with a through hole, and the through hole is matched with the sealing bolt.
Preferably, the bottom of the connecting pipe is provided with an electrode groove, the lamp body is electrically connected with the storage battery through the pins and the electrode groove, and an embedded structure is arranged between the lamp body and the connecting pipe.
Preferably, the upper end of the sealing layer is an annular inclined structure, and the sealing layer is a member made of rubber.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model provides a pair of embedded novel environmental protection aviation lamp, be electric connection through between solar panel and the battery, the electrode tank has been seted up to the bottom of connecting pipe, the lamp body passes through and constitutes electric connection between pin and electrode tank and the battery, and be embedded structure between lamp body and the connecting pipe, be convenient for change the operation to the lamp body, upper end through the sealing layer is an annular slope column structure, and the sealing layer is the component that a rubber material was made, be convenient for calibrate the embedding installation to the lamp body, and make lamp body and sealing layer closely laminate, avoid the rainwater to invade.
2. The utility model provides an embedded novel environmental protection aviation lamp sets up the periphery at the connecting pipe through the connecting block, and the upper surface sets up sealed bolt, and the through-hole has been seted up to the inner wall of connecting pipe, and through-hole and sealed bolt phase-match, when embedding the installation, because of lamp body and the inseparable laminating of sealing layer, make the inside gas of connecting pipe discharge from the through-hole, the back of finishing is installed, blocks up the through-hole through sealed bolt, utilizes the difference of vacuum pressure to strengthen the steadiness between lamp body and the connecting pipe.
3. The utility model provides a pair of embedded novel environmental protection aviation lamp has seted up the dovetail through the upper surface inside of connecting block, and the lower surface of sealed bolt sets up the dovetail piece, constitutes sliding connection between connecting block and the sealed bolt, and the connecting block of being convenient for blocks up the through-hole, need not carry out calibration work to accelerate the change speed of lamp body, set up the connecting block and be connected with sealed bolt, also avoid appearing the phenomenon that sealed bolt landing was lost.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic perspective view of the connection mechanism and the illumination mechanism of the present invention;
FIG. 3 is a schematic view of the internal three-dimensional structure of the connection mechanism of the present invention;
fig. 4 is a schematic view of the enlarged three-dimensional structure at a position a of the present invention.
In the figure: 1. a power supply mechanism; 11. a solar panel; 12. a storage battery; 2. a connecting mechanism; 21. a fixing plate; 22. a bolt; 23. a fixing member; 231. connecting blocks; 2311. a dovetail groove; 232. sealing the bolt; 2321. a dovetail block; 24. a connecting pipe; 241. a through hole; 242. an electrode tank; 25. a sealing layer; 3. an illumination mechanism; 31. a lamp body; 32. and (7) a pin.
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, an embedded novel environment-friendly aviation lamp includes a power supply mechanism 1, a connection mechanism 2 and a lighting mechanism 3, the connection mechanism 2 is installed on the upper surface of the power supply mechanism 1, the lighting mechanism 3 is installed inside the upper end of the connection mechanism 2, the power supply mechanism 1 includes a solar panel 11 and a storage battery 12, the solar panel 11 is installed on one side of the storage battery 12, the connection mechanism 2 includes a fixing plate 21, a bolt 22, a fixing member 23, a connection pipe 24 and a sealing layer 25, the fixing plate 21 is installed on the upper surface of the storage battery 12 through the bolt 22, the connection pipe 24 is installed on the upper surface of the fixing plate 21, the fixing member 23 is arranged on the periphery of the connection pipe 24, the sealing layer 25 is adhered on the inner wall of the connection pipe 24, the lighting mechanism 3 includes a lamp body 31 and a pin 32, the pin, the solar panel 11 is electrically connected with the storage battery 12, the bottom of the connecting pipe 24 is provided with an electrode groove 242, the lamp body 31 is electrically connected with the storage battery 12 through the pin 32 and the electrode groove 242, the lamp body 31 and the connecting pipe 24 are of an embedded structure, the upper end of the sealing layer 25 is of an annular inclined structure, the sealing layer 25 is a member made of rubber material, so that the replacement operation of the lamp body 31 is convenient, the lamp body 31 is conveniently calibrated and embedded and installed through the upper end of the sealing layer 25, the lamp body 31 is tightly attached to the sealing layer 25, the invasion of rainwater is avoided, the inner wall of the connecting pipe 24 is provided with a through hole 241, the through hole 241 is matched with the sealing bolt 232, when the embedded installation is carried out, the gas in the connecting pipe 24 is discharged from the through hole 241 due to the tight attachment of the lamp body 31 and the sealing layer 25, after the, the through hole 241 is blocked by the sealing plug 232, the stability between the lamp body 31 and the connecting pipe 24 is enhanced by the vacuum pressure difference,
please refer to fig. 4, an embedded novel environment-friendly aviation lamp, the fixing member 23 includes a connecting block 231 and a sealing plug 232, the connecting block 231 is disposed at the periphery of the connecting pipe 24, and the upper surface is provided with the sealing plug 232, a dovetail groove 2311 is disposed inside the upper surface of the connecting block 231, a dovetail block 2321 is disposed on the lower surface of the sealing plug 232, a sliding connection is formed between the connecting block 231 and the sealing plug 232, the connecting block 231 is convenient to block the through hole 241, calibration work is not needed, thereby increasing the replacement rate of the lamp body 31, the connecting block 231 is connected with the sealing plug 232, and the phenomenon that the sealing plug 232 is lost due to sliding is avoided.
In summary, the following steps: the utility model provides an embedded novel environmental protection aviation lamp, including power supply mechanism 1, coupling mechanism 2 and lighting mechanism 3, coupling mechanism 2 installs the upper surface at power supply mechanism 1, lighting mechanism 3 installs inside the upper end of coupling mechanism 2, through being the electric connection between solar panel 11 and battery 12, electrode slot 242 has been seted up to the bottom of connecting pipe 24, lamp body 31 constitutes the electric connection through pin 32 and electrode slot 242 and battery 12, and be the embedded structure between lamp body 31 and the connecting pipe 24, be convenient for change the operation to lamp body 31, through the upper end of sealing layer 25 be an annular slope form structure, and sealing layer 25 is the component that a rubber material made, be convenient for calibrate the embedding installation to lamp body 31, and make lamp body 31 and sealing layer 25 closely laminate, avoid the rainwater to invade, set up in the periphery of connecting pipe 24 through connecting block 231, and the upper surface sets up the sealing bolt 232, the through-hole 241 has been seted up to the inner wall of connecting pipe 24, and through-hole 241 and sealing bolt 232 phase-match, when embedding installation, because of lamp body 31 and sealing layer 25 closely laminate, make the inside gas of connecting pipe 24 discharge from through-hole 241, after the installation, block up through-hole 241 through sealing bolt 232, utilize the vacuum pressure difference to strengthen the steadiness between lamp body 31 and the connecting pipe 24, dovetail 2311 has been seted up through the upper surface inside of connecting block 231, the lower surface of sealing bolt 232 sets up forked tail piece 2321, constitute sliding connection between connecting block 231 and the sealing bolt 232, be convenient for connecting block 231 blocks up through-hole 241, need not carry out calibration work, thereby accelerate the change rate of lamp body 31, set up connecting block 231 and sealing bolt 232 and be connected, also avoid appearing the phenomenon that sealing bolt 232 landing is lost.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
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 (7)
1. The utility model provides an embedded novel environmental protection aviation lamp, includes power supply mechanism (1), coupling mechanism (2) and lighting mechanism (3), the upper surface at power supply mechanism (1) is installed in coupling mechanism (2), and inside the upper end of coupling mechanism (2), its characterized in that were installed in lighting mechanism (3): the power supply mechanism (1) comprises a solar panel (11) and a storage battery (12), wherein the solar panel (11) is arranged on one side of the storage battery (12);
the connecting mechanism (2) comprises a fixing plate (21), a bolt (22), a fixing piece (23), a connecting pipe (24) and a sealing layer (25), the fixing plate (21) is installed on the upper surface of the storage battery (12) through the bolt (22), the connecting pipe (24) is installed on the upper surface of the fixing plate (21), the fixing piece (23) is arranged on the periphery of the connecting pipe (24), and the sealing layer (25) is bonded on the inner wall of the connecting pipe (24);
the lighting mechanism (3) comprises a lamp body (31) and pins (32), the pins (32) are arranged at the lower end of the lamp body (31), and the lower end of the lamp body (31) is arranged in the connecting pipe (24).
2. The embedded novel environment-friendly aviation lamp as claimed in claim 1, wherein: the solar panel (11) is electrically connected with the storage battery (12).
3. The embedded novel environment-friendly aviation lamp as claimed in claim 1, wherein: the fixing piece (23) comprises a connecting block (231) and a sealing bolt (232), the connecting block (231) is arranged on the periphery of the connecting pipe (24), and the sealing bolt (232) is arranged on the upper surface of the connecting block.
4. The embedded novel environment-friendly aviation lamp as claimed in claim 3, wherein: the inner part of the upper surface of the connecting block (231) is provided with a dovetail groove (2311), the lower surface of the sealing bolt (232) is provided with a dovetail block (2321), and the connecting block (231) and the sealing bolt (232) are in sliding connection.
5. The embedded novel environment-friendly aviation lamp as claimed in claim 1, wherein: the inner wall of the connecting pipe (24) is provided with a through hole (241), and the through hole (241) is matched with the sealing bolt (232).
6. The embedded novel environment-friendly aviation lamp as claimed in claim 1, wherein: an electrode groove (242) is formed in the bottom of the connecting pipe (24), the lamp body (31) is electrically connected with the storage battery (12) through the pins (32) and the electrode groove (242), and an embedded structure is formed between the lamp body (31) and the connecting pipe (24).
7. The embedded novel environment-friendly aviation lamp as claimed in claim 1, wherein: the upper end of the sealing layer (25) is of an annular inclined structure, and the sealing layer (25) is a component made of rubber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021583872.2U CN212456667U (en) | 2020-08-03 | 2020-08-03 | Embedded novel environmental protection aviation lamp |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021583872.2U CN212456667U (en) | 2020-08-03 | 2020-08-03 | Embedded novel environmental protection aviation lamp |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212456667U true CN212456667U (en) | 2021-02-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021583872.2U Active CN212456667U (en) | 2020-08-03 | 2020-08-03 | Embedded novel environmental protection aviation lamp |
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| Country | Link |
|---|---|
| CN (1) | CN212456667U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117588728A (en) * | 2024-01-19 | 2024-02-23 | 保定天杉电子科技开发有限公司 | Combined type aviation lamp convenient to replace |
-
2020
- 2020-08-03 CN CN202021583872.2U patent/CN212456667U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117588728A (en) * | 2024-01-19 | 2024-02-23 | 保定天杉电子科技开发有限公司 | Combined type aviation lamp convenient to replace |
| CN117588728B (en) * | 2024-01-19 | 2024-04-09 | 保定天杉电子科技开发有限公司 | Combined type aviation lamp convenient to replace |
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