CN212584830U - Aviation lamp with early warning mechanism - Google Patents

Aviation lamp with early warning mechanism Download PDF

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Publication number
CN212584830U
CN212584830U CN202021572238.9U CN202021572238U CN212584830U CN 212584830 U CN212584830 U CN 212584830U CN 202021572238 U CN202021572238 U CN 202021572238U CN 212584830 U CN212584830 U CN 212584830U
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China
Prior art keywords
early warning
lamp
module
protection casing
warning mechanism
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CN202021572238.9U
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Chinese (zh)
Inventor
宋红雨
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Baoding Tianshan Electric Technology Dev Co ltd
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Baoding Tianshan Electric Technology Dev Co ltd
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Abstract

The utility model discloses an aviation lamp with an early warning mechanism, when the aviation lamp is arranged on an airport runway for use, the upper end of the supporting rod is provided with a playing component which consists of a microprocessor module, a timer module, a memory module, a digital signal processor module and a music playing unit, the music playing unit can play sound according to the set playing time so as to play the effect of early warning and repelling birds, the outer surface of the lamp is provided with the protective cover, the protective cover with the net-shaped hollow structure can protect the lamp to prevent birds or overlarge objects from damaging the lamp, the limiting block arranged at the lower end of the outer surface of the protective cover is put in from the rotating groove, and after the protection casing is rotated, the lifter plate of protection casing bottom surface can make the stopper card inside the U-shaped structure under the elastic force effect of first spring, and the effectual protection casing that prevents drops after the installation.

Description

Aviation lamp with early warning mechanism
Technical Field
The utility model relates to an aviation lamp technical field specifically is an aviation lamp with early warning mechanism.
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.
However, the prior aviation lamp cannot perform early warning and driving when being used in an airport, and the bird crowd near the aviation lamp is too much, so that the airplane is easy to have accidents.
In order to solve the problems, the aviation lamp with the early warning mechanism is provided.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aviation lamp with early warning mechanism, when aviation lamp is installed and is used on the airport runway, install the broadcast subassembly in the upper end of bracing piece, the broadcast subassembly comprises microprocessor module, timer module, memory module, digital signal processor module and music play unit, the music play unit can carry out the sound according to the broadcast time of settlement and broadcast to play the effect that the birds were driven in the early warning, thereby solved the problem 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 an aviation lamp with early warning mechanism, the aviation lamp includes base, bracing piece, broadcast subassembly, waterproof board, mounting groove, protection casing and lamps and lanterns, and the bracing piece is installed to the upper end of base, and the broadcast subassembly is installed to the upper end of bracing piece, and the waterproof board is installed in the surface upper end four corners of broadcast subassembly, and the mounting groove has been seted up to the upper end of broadcast subassembly, and the protection casing is installed to the inner chamber of mounting groove, and lamps and lanterns are installed to the inner chamber of protection.
Preferably, the playing assembly comprises a microprocessor module, a timer module, a memory module, a digital signal processor module and a music playing unit, and the microprocessor module, the timer module, the memory module, the digital signal processor module and the music playing unit are sequentially installed in an inner cavity of the playing assembly.
Preferably, the mounting groove includes swivelling chute, first spring and lifter plate, and the swivelling chute has been seted up to the inner chamber lateral wall of mounting groove, and first spring is installed to the inner chamber bottom surface of mounting groove, and the lifter plate is installed to the upper end of first spring.
Preferably, the rotating groove comprises an arc ball, a check ring and a second spring, the arc ball is mounted on the side wall of the inner cavity of the rotating groove, the check ring is mounted on the side surface of the arc ball, the second spring is mounted on the side surface of the check ring, and the rotating groove is of a U-shaped structure.
Preferably, the protective cover comprises a limiting block and a fastening hole, the limiting block is mounted on two sides of the lower end of the protective cover, and the fastening hole is formed in the side face of the limiting block.
Preferably, the protective cover is in a mesh hollow structure.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model provides a pair of aviation lamp with early warning mechanism, when aviation lamp installs and uses on the airport runway, install the broadcast subassembly in the upper end of bracing piece, the broadcast subassembly comprises microprocessor module, timer module, memory module, digital signal processor module and music broadcast unit, and the music broadcast unit can carry out the sound according to the broadcast time of settlement and broadcast to play the effect that birds were driven in the early warning.
2. The utility model provides a pair of aviation lamp with early warning mechanism, there is the protection casing at the surface mounting of lamps and lanterns, netted hollow out construction's protection casing can protect lamps and lanterns, prevents that birds or too big thing piece from damaging lamps and lanterns, and the stopper of protection casing surface lower extreme installation is put into from the swivelling chute to behind the rotation protection casing, the lifter plate of protection casing bottom surface can make the stopper card inside the U-shaped structure under the spring action of first spring, effectually prevents that the protection casing from dropping after the installation.
3. The utility model provides a pair of aviation lamp with early warning mechanism installs the arc ball at the inner chamber lateral wall of swivelling chute, and the arc ball can carry out the block with the fastening hole under the spring action of second spring, and further fastens the protection casing, prevents that the phenomenon that the protection casing dropped from appearing.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of the detachable structure of the aviation lamp of the present invention;
fig. 3 is a schematic diagram of the internal structure of the playing component of the present invention;
fig. 4 is an enlarged schematic structural view of the utility model at the position B in fig. 3;
fig. 5 is an enlarged schematic structural view of a point a in fig. 2 according to the present invention;
fig. 6 is a schematic diagram of the playing component according to the present invention.
In the figure: 1. an aviation light; 11. a base; 12. a support bar; 13. a play component; 131. a microprocessor module; 132. a timer module; 133. a memory module; 134. a digital signal processor module; 135. a music playing unit; 14. a waterproof sheet; 15. mounting grooves; 151. a rotating tank; 1511. a circular arc ball; 1512. a retainer ring; 1513. a second spring; 152. a first spring; 153. a lifting plate; 16. a protective cover; 161. a limiting block; 162. a fastening hole; 17. a luminaire.
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 aviation lamp with an early warning mechanism, the aviation lamp 1 includes a base 11, a support rod 12, a playing component 13, a waterproof board 14, and a mounting groove 15, the mounting groove 15 includes a rotating groove 151, a first spring 152 and a lifting board 153, the rotating groove 151 is disposed on the side wall of the inner cavity of the mounting groove 15, the first spring 152 is disposed on the bottom surface of the inner cavity of the mounting groove 15, the lifting board 153 is disposed on the upper end of the first spring 152, a protective cover 16 is disposed on the outer surface of the lamp 17, the protective cover 16 with a mesh-type hollow structure can protect the lamp 17 to prevent birds or oversized objects from damaging the lamp 17, a limit block 161 disposed on the lower end of the outer surface of the protective cover 16 is put in from the rotating groove 151, and after the protective cover 16 is rotated, the lifting board 153 on the bottom surface of the protective cover 16 can enable the, effectual protection casing 16 that prevents drops after the installation, protection casing 16 and lamps and lanterns 17, bracing piece 12 is installed to the upper end of base 11, and broadcast subassembly 13 is installed to the upper end of bracing piece 12, and waterproof board 14 is installed at the surface upper end four corners of broadcast subassembly 13, and mounting groove 15 has been seted up to the upper end of broadcast subassembly 13, and protection casing 16 is installed to the inner chamber of mounting groove 15, and lamps and lanterns 17 are installed to the inner chamber of protection casing 16.
Referring to fig. 4-5, an aircraft lamp with an early warning mechanism includes a rotating groove 151 including an arc ball 1511, a retainer ring 1512 and a second spring 1513, the arc ball 1511 is installed on a sidewall of an inner cavity of the rotating groove 151, the retainer ring 1512 is installed on a side surface of the arc ball 1511, the second spring 1513 is installed on a side surface of the retainer ring 1512, the rotating groove 151 is in a U-shaped structure, the shield 16 includes a stopper 161 and a fastening hole 162, the stoppers 161 are installed on two sides of a lower end of the shield 16, the fastening hole 162 is opened on a side surface of the stopper 161, the shield 16 is in a mesh-like hollow structure, the arc ball 1511 is installed on a sidewall of the inner cavity of the rotating groove 151, the arc ball 1511 can be engaged with the fastening hole 162 under an elastic force of the second spring 1513, so as to further fasten the.
Referring to fig. 6, a navigation light with an early warning mechanism, a playing component 13 includes a microprocessor module 131, a timer module 132, a memory module 133, a digital signal processor module 134 and a music playing unit 135, the microprocessor module 131, the timer module 132, the memory module 133, the digital signal processor module 134 and the music playing unit 135 are sequentially installed in an inner cavity of the playing component 13, when the navigation light 1 is installed on an airport runway for use, the playing component 13 is installed at the upper end of the supporting rod 12, the playing component 13 is composed of the microprocessor module 131, the timer module 132, the memory module 133, the digital signal processor module 134 and the music playing unit 135, and the music playing unit 135 can play sound according to a set playing time, thereby playing an early warning effect of repelling birds.
In summary, the following steps: the utility model provides an aviation lamp with early warning mechanism, when aviation lamp 1 is installed on the airport runway for use, install broadcast subassembly 13 at the upper end of bracing piece 12, broadcast subassembly 13 comprises microprocessor module 131, timer module 132, memory module 133, digital signal processor module 134 and music play unit 135, music play unit 135 can carry out the sound broadcast according to the broadcast time of settlement, thereby play the effect that the birds are driven in the early warning, there is the protection casing 16 at the surface of lamps and lanterns 17, the protection casing 16 of netted hollow out construction can protect lamps and lanterns 17, prevent birds or too big thing piece from damaging lamps and lanterns 17, and stopper 161 of the installation of protection casing 16 surface lower extreme is put into from the rotating slot 151, and after rotating protection casing 16, the lifter plate 153 of protection casing 16 bottom surface can make stopper 161 inside the U-shaped structure under the elastic force effect of first spring 152, the effectual protection casing 16 that prevents drops after the installation, installs circular arc ball 1511 at the inner chamber lateral wall of swivelling chute 151, and circular arc ball 1511 can carry out the block with fastening hole 162 under the spring action of second spring 1513, and further fastens protection casing 16, prevents that the phenomenon that protection casing 16 appears dropping.
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 (6)

1. The utility model provides an aviation lamp with early warning mechanism which characterized in that: aviation lamp (1) is including base (11), bracing piece (12), broadcast subassembly (13), waterproof board (14), mounting groove (15), protection casing (16) and lamps and lanterns (17), bracing piece (12) are installed to the upper end of base (11), broadcast subassembly (13) are installed to the upper end of bracing piece (12), waterproof board (14) are installed in the surface upper end four corners of broadcast subassembly (13), mounting groove (15) have been seted up to the upper end of broadcast subassembly (13), protection casing (16) are installed to the inner chamber of mounting groove (15), lamps and lanterns (17) are installed to the inner chamber of protection casing (16).
2. An aviation lamp with an early warning mechanism as claimed in claim 1, wherein: the playing assembly (13) comprises a microprocessor module (131), a timer module (132), a memory module (133), a digital signal processor module (134) and a music playing unit (135), wherein the microprocessor module (131), the timer module (132), the memory module (133), the digital signal processor module (134) and the music playing unit (135) are sequentially installed in an inner cavity of the playing assembly (13).
3. An aviation lamp with an early warning mechanism as claimed in claim 1, wherein: mounting groove (15) have been seted up swivelling chute (151) including swivelling chute (151), first spring (152) and lifter plate (153), swivelling chute (151) have been installed to the inner chamber lateral wall of mounting groove (15), and first spring (152) are installed to the inner chamber bottom surface of mounting groove (15), and lifter plate (153) are installed to the upper end of first spring (152).
4. An aviation lamp with an early warning mechanism as claimed in claim 3, wherein: the rotating groove (151) comprises an arc ball (1511), a retainer ring (1512) and a second spring (1513), the arc ball (1511) is installed on the side wall of the inner cavity of the rotating groove (151), the retainer ring (1512) is installed on the side surface of the arc ball (1511), the second spring (1513) is installed on the side surface of the retainer ring (1512), and the rotating groove (151) is of a U-shaped structure.
5. An aviation lamp with an early warning mechanism as claimed in claim 1, wherein: the protective cover (16) comprises a limiting block (161) and a fastening hole (162), the limiting block (161) is installed on two sides of the lower end of the protective cover (16), and the fastening hole (162) is formed in the side face of the limiting block (161).
6. An aviation lamp with an early warning mechanism as claimed in claim 1, wherein: the protective cover (16) is of a net-shaped hollow structure.
CN202021572238.9U 2020-08-02 2020-08-02 Aviation lamp with early warning mechanism Active CN212584830U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202021572238.9U CN212584830U (en) 2020-08-02 2020-08-02 Aviation lamp with early warning mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202021572238.9U CN212584830U (en) 2020-08-02 2020-08-02 Aviation lamp with early warning mechanism

Publications (1)

Publication Number Publication Date
CN212584830U true CN212584830U (en) 2021-02-23

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN202021572238.9U Active CN212584830U (en) 2020-08-02 2020-08-02 Aviation lamp with early warning mechanism

Country Status (1)

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CN (1) CN212584830U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113412830A (en) * 2021-06-29 2021-09-21 无棣泰祥电力器材有限责任公司 Remote control's high adaptability drives bird equipment

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113412830A (en) * 2021-06-29 2021-09-21 无棣泰祥电力器材有限责任公司 Remote control's high adaptability drives bird equipment

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