Aviation obstruction beacon with temperature detection function
By introducing temperature sensors and remote control modules into the aviation obstacle lights, real-time monitoring and automatic control of the internal temperature of the protective cover is achieved, and equipment damage caused by excessive temperature in the prior art is solved, and the service life of the equipment is extended.
Patent Information
- Application Number
- CN202422327666.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-09-24
- Publication Date
- 2025-06-27
- Estimated Expiration
- 2034-09-24
AI Technical Summary
During the long-term operation of existing aviation obstacle lights, the internal temperature may be too high, causing damage to the lines and light bulbs, but they cannot be detected and processed in real time.
An aviation barrier light with temperature detection function is designed. By setting a temperature sensor on the control circuit board and connecting it with a remote control module, the temperature inside the protective cover is monitored in real time. When the temperature exceeds the set range, the light bulb will be automatically turned off or subsequent processing is performed.
It effectively avoids the continuous high temperature inside the protective cover, protects the control circuit board and light bulb, and extends its service life.
Smart Images
Figure CN223036350U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of aviation obstruction lights, in particular to an aviation obstruction light with a temperature detection function. Background Art
[0002] An aviation obstruction light is an indicator light used for aircraft operators to identify the outlines of ground buildings and obstacles, and plays an important role in the field of aviation safety.
[0003] During the use of existing aviation obstruction lights, the internal bulbs generate heat. During long-term operation, it is easy to cause the internal temperature of the obstruction lights to be too high, resulting in damage to the circuits and bulbs. It is impossible to detect the internal temperature in real time, and thus it is impossible to perform subsequent processing in a timely manner. For this reason, the utility model proposes an aviation obstruction light with a temperature detection function. Summary of the Utility Model
[0004] Aiming at the deficiencies of the prior art, the utility model provides an aviation obstruction light with a temperature detection function, which solves the problems raised in the above background art.
[0005] To achieve the above purposes, the utility model is realized through the following technical solutions: an aviation obstruction light with a temperature detection function, including a lamp base, a fastening bolt is arranged on the outside of the lamp base, a protective cover is arranged at the upper end of the lamp base, a fastening ring is arranged at the connection between the protective cover and the lamp base, and a buckle and a clamping block are arranged on the outside of the fastening ring;
[0006] A bulb and a control circuit board are arranged at the upper end of the lamp base, a temperature sensor is arranged at the upper end of the control circuit board, an auxiliary seat is connected to the bottom of the temperature sensor, an installation bolt is arranged between the auxiliary seat and the control circuit board, a solar panel is arranged at the upper end of the protective cover, and a battery is arranged inside the lamp base.
[0007] As a further technical solution of the utility model, a threaded hole is arranged between the lamp base and the fastening bolt, the lamp base and the protective cover are connected through a fastening ring, the protective cover is of a transparent structure, the fastening ring is of an open circular ring structure, and a number of limiting blocks are installed at the top of the fastening ring.
[0008] As a further technical solution of the utility model, the buckle is connected to the fastening ring, the clamping block is an integral structure with the fastening ring, and the clamping block is adapted to the buckle.
[0009] As a further technical solution of the utility model, the bulb is electrically connected to the control circuit board, the control circuit board is electrically connected to the battery, and a remote control module and a communication module are arranged inside the control circuit board.
[0010] As a further technical solution of the present utility model, the number of the temperature sensors is several groups and is distributed in an array. The temperature sensors are fixedly connected to the auxiliary seat, electrically connected to the control circuit board, and the auxiliary seat and the control circuit board are connected by mounting bolts.
[0011] As a further technical solution of the present utility model, the solar power generation panel is of a flexible structure, wraps the top of the protective cover, and is electrically connected to the control circuit board.
[0012] The present utility model provides an aviation obstruction lamp with a temperature detection function. Compared with the prior art, it has the following beneficial effects:
[0013] The designed aviation obstruction lamp with a temperature detection function, through the settings of the control circuit board, temperature sensors, auxiliary seat and mounting bolts, when the bulb is lit for a long time and with the installation of the auxiliary seat and mounting bolts, enables the temperature sensors to monitor the temperature inside the protective cover in real time. When the temperature exceeds the set interval value, it is connected to the background PC through the remote control module inside the control circuit board, so as to timely turn off the bulb or perform subsequent processing, avoiding the continuous occurrence of high temperature inside the protective cover, thereby protecting the control circuit board and the bulb and improving their service life. Description of the Drawings
[0014] Figure 1 It is a schematic diagram of the overall structure of an aviation obstruction lamp with a temperature detection function;
[0015] Figure 2 It is a top view of an aviation obstruction lamp with a temperature detection function;
[0016] Figure 3 It is an aviation obstruction lamp with a temperature detection function Figure 2 Side sectional view of A-A in.
[0017] In the figure: 1, lamp base; 2, fastening bolt; 3, protective cover; 4, fastening ring; 5, buckle; 6, clamping block; 7, bulb; 8, control circuit board; 9, temperature sensor; 10, auxiliary seat; 11, mounting bolt; 12, solar power generation panel; 13, battery. Detailed Embodiment
[0018] Next, the technical solutions in the embodiments of the present invention will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
[0019] Please refer to Figures 1-3 , the present invention provides a technical solution for an aviation obstruction light with a temperature detection function: an aviation obstruction light with a temperature detection function, including a lamp base 1, a fastening bolt 2 is arranged on the outer side of the lamp base 1, a protective cover 3 is arranged at the upper end of the lamp base 1, a fastening ring 4 is arranged at the connection between the protective cover 3 and the lamp base 1, and a buckle 5 and a clamping block 6 are arranged on the outer side of the fastening ring 4;
[0020] Among them, a light bulb 7 and a control circuit board 8 are arranged at the upper end of the lamp base 1, a temperature sensor 9 is arranged at the upper end of the control circuit board 8, the bottom of the temperature sensor 9 is connected to an auxiliary seat 10, an installation bolt 11 is arranged between the auxiliary seat 10 and the control circuit board 8, a solar panel 12 is arranged at the upper end of the protective cover 3, and a battery 13 is arranged inside the lamp base 1.
[0021] As Figures 1-3 shown, a threaded hole is arranged between the lamp base 1 and the fastening bolt 2, the lamp base 1 and the protective cover 3 are connected through the fastening ring 4, the protective cover 3 is of a transparent structure, the fastening ring 4 is of an open circular ring structure, and a number of limiting blocks are installed at the top of the fastening ring 4. The buckle 5 is connected to the fastening ring 4, the clamping block 6 is an integral structure with the fastening ring 4, and the clamping block 6 is adapted to the buckle 5, which is beneficial to the installation and fixation between the protective cover 3 and the lamp base 1.
[0022] As Figures 1-3 shown, the light bulb 7 is electrically connected to the control circuit board 8, the control circuit board 8 is electrically connected to the battery 13, and a remote control module and a communication module are arranged inside the control circuit board 8, which is beneficial to the communication connection with the background PC.
[0023] As Figures 1-3 shown, the number of the temperature sensors 9 is several groups and is distributed in an array. The temperature sensors 9 are fixedly connected to the auxiliary seat 10, the temperature sensors 9 are electrically connected to the control circuit board 8, and the auxiliary seat 10 and the control circuit board 8 are connected through the installation bolt 11, which is beneficial to the installation of the temperature sensors 9, facilitating the real-time monitoring of the temperature inside the protective cover 3 and avoiding the phenomenon of damage to the circuit and the light bulb 7 due to too high temperature.
[0024] As Figures 1-3As shown, the solar panel 12 is of a flexible structure. The solar panel 12 wraps the top of the protective cover 3. The solar panel 12 is electrically connected to the control circuit board 8, which is conducive to power generation. The electric energy is stored inside the battery 13. When the building power supply is cut off, the bulb 7 can continue to be lit and the temperature of the control circuit board 8 can be detected.
[0025] The working principle of the present utility model is as follows: During the use of the aviation obstruction lamp, the protective cover 3 is installed and fixed to the lamp base 1 through the fastening ring 4, the buckle 5 and the clamping block 6. The bulb 7 is lit. At the same time, with the installation of the auxiliary seat 10 and the installation bolt 11, the temperature sensor 9 monitors the temperature inside the protective cover 3 in real time. When the temperature exceeds the set range value, the remote control module inside the control circuit board 8 is connected to the background PC terminal, so as to timely turn off the bulb 7 or perform subsequent processing, avoiding the continuous high temperature phenomenon inside the protective cover 3, thereby protecting the control circuit board 8 and the bulb 7 and improving their service life.
[0026] The above is only the preferred embodiment of the present utility model. It should be noted that for those of ordinary skill in the art in this technical field, without departing from the principle of the present utility model, several improvements and retouches can be made, and these improvements and retouches should also be regarded as the protection scope of the present utility model. The structures, devices and operation methods not specifically described and explained in the present utility model, without special instructions and limitations, are implemented according to the conventional means in this field.
Claims
1. An aviation obstruction light with a temperature detection function, comprising a light base (1), characterized in that: A fastening bolt (2) is arranged on the outside of the lamp base (1), a protective cover (3) is arranged on the upper end of the lamp base (1), a fastening ring (4) is arranged at the connection between the protective cover (3) and the lamp base (1), and a buckle (5) and a clamping block (6) are arranged on the outside of the fastening ring (4); A light bulb (7) and a control circuit board (8) are arranged at the upper end of the lamp base (1); a temperature sensor (9) is arranged at the upper end of the control circuit board (8); an auxiliary seat (10) is connected to the bottom of the temperature sensor (9); mounting bolts (11) are arranged between the auxiliary seat (10) and the control circuit board (8); a solar power generation panel (12) is arranged at the upper end of the protective cover (3); and a battery (13) is arranged inside the lamp base (1).
2. The aviation obstruction light with temperature detection function according to claim 1, characterized in that: A threaded hole is provided between the lamp base (1) and the fastening bolt (2); the lamp base (1) and the protective cover (3) are connected via a fastening ring (4); the protective cover (3) is a transparent structure; the fastening ring (4) is an open circular ring structure; and a plurality of groups of limit blocks are installed on the top of the fastening ring (4).
3. The aviation obstruction light with temperature detection function according to claim 1, characterized in that: The buckle (5) is connected to the fastening ring (4), the clamping block (6) and the fastening ring (4) are an integrated structure, and the clamping block (6) and the buckle (5) are adapted to each other.
4. The aviation obstruction light with temperature detection function according to claim 1, characterized in that: The light bulb (7) is electrically connected to the control circuit board (8), the control circuit board (8) is electrically connected to the battery (13), and a remote control module and a communication module are arranged inside the control circuit board (8).
5. The aviation obstruction light with temperature detection function according to claim 1, characterized in that: The temperature sensors (9) are arranged in a plurality of groups and are distributed in an array; the temperature sensors (9) are fixedly connected to the auxiliary seat (10); the temperature sensors (9) are electrically connected to the control circuit board (8); and the auxiliary seat (10) and the control circuit board (8) are connected via mounting bolts (11).
6. The aviation obstruction light with temperature detection function according to claim 1, characterized in that: The solar power generation panel (12) is a flexible structure, the solar power generation panel (12) wraps the top of the protective cover (3), and the solar power generation panel (12) is electrically connected to the control circuit board (8).