Emergency intelligent induction lighting device for civil air defense engineering

Abstract

The emergency intelligent induction lighting device comprises a mounting frame and a connecting frame, the connecting frame is located on one side of the mounting frame, transversely-arranged supporting columns are symmetrically arranged on the other side of the connecting frame, a lamp holder is arranged at the end of each supporting column, and a full-spectrum lighting lamp is arranged at the bottom of each lamp holder. The full-spectrum illuminating lamp is sleeved with a protective cover connected with the lamp holder, and the connecting frame is provided with an adjusting mechanism used for adjusting the angle of the full-spectrum illuminating lamp. Through cooperative arrangement of the induction assembly and the signal receiving and transmitting module, the induction assembly is used for monitoring whether a person passes by or not and sending a monitoring result to the microcontroller and the signal receiving and transmitting module, and when the person passes by, the microcontroller controls the full-spectrum illuminating lamp to work; and therefore, the position angle of the full-spectrum illuminating lamp can be adjusted, the height of the illuminating device at a high position can be reduced, the illuminating device can be conveniently overhauled, and the illuminating device can be overhauled very conveniently.

Description

Technical Field

[0001] The present invention relates to the technical field of lighting devices, and in particular to an emergency intelligent induction lighting device for civil air defense projects. Background Art

[0002] The clear height of the space inside the civil air defense project is relatively high, and the height at which its lighting devices are installed and used is also relatively high. At the same time, the lighting devices are fixed structures. When the lighting devices need to be inspected and maintained, climbing tools are required to perform the inspection and maintenance operations. Therefore, the inspection and maintenance operations of the lighting devices in the civil air defense project are relatively inconvenient.

[0003] Currently, no effective solutions have been proposed for the problems in related technologies. Summary of the Invention

[0004] In response to the problems in the related art, the present invention proposes an emergency intelligent sensing lighting device for civil air defense projects to overcome the above-mentioned technical problems existing in the existing related art.

[0005] To this end, the specific technical solutions adopted in the present invention are as follows:

[0006] An emergency intelligent induction lighting device for civil air defense projects, comprising a mounting frame and a connecting frame, the connecting frame being located on one side of the mounting frame, the connecting frame being symmetrically provided with laterally arranged pillars on the other side, the ends of the pillars being provided with lamp holders, the bottom of the lamp holders being provided with a full-spectrum lighting lamp, the full-spectrum lighting lamp being provided with a protective cover connected to the lamp holder, and the connecting frame being provided with an adjustment mechanism for adjusting the angle of the full-spectrum lighting lamp;

[0007] A sensing component is provided on one side of the lamp holder. The sensing component includes a thermal energy sensor, an electronic eye and a photoelectric sensor. The thermal energy sensor, the electronic eye and the photoelectric sensor are electrically connected to the microcontroller in the lamp holder.

[0008] Preferably, the adjustment mechanism includes a shell located on one side of the connecting frame, a side plate is provided in the shell, a gear disc is provided on one side of the side plate, a horizontally arranged bearing seat is provided on one side of the gear disc, the bearing seat is movably connected to a rotating shaft, and the end of the rotating shaft is provided with a connecting column extending outside the shell and connected to the pillar.

[0009] Preferably, a transmission gear meshing with the gear disc is provided on one side of the side plate, and the axis of the transmission gear is connected to an output shaft of the servo motor of the housing.

[0010] Preferably, a limiting member is provided on one side of the gear disc and located between the bearing seat 1 and the transmission gear, and a limiting column matching the limiting member is symmetrically provided on one side of the side plate.

[0011] Preferably, a vertically arranged bearing seat 2 is provided on one side of the side plate and above the gear disc, a rotating shaft 2 is movably connected to the bearing seat 2, and the bottom end of the rotating shaft 2 is provided with a shaft rod 1 and a shaft rod 2 which are symmetrically arranged in pairs.

[0012] Preferably, the end of the rotating shaft 1 away from the connecting column is provided with shaft rods 3 and 4 symmetrically arranged in pairs, two groups of shaft rods 3 are movably connected to the shaft rods 1 in pairs, and two groups of shaft rods 4 are movably connected to the shaft rods 2 in pairs.

[0013] Preferably, the shaft one and the shaft two are movably connected to the shaft three and the shaft four via universal joints, and a servo motor two for driving the rotating shaft two is provided on the side panel.

[0014] Preferably, a travel hole for the movement of the connecting column is provided on the shell, and the shell is connected to the connecting frame by bolts.

[0015] Preferably, the length of the shaft rod one is smaller than the length of the shaft rod two, and the length of the shaft rod three is smaller than the length of the shaft rod four.

[0016] Preferably, the thermal energy sensor is an infrared sensor, the connecting frame is provided with a signal transceiver module electrically connected to the sensing component, and one side of the signal transceiver module is provided with an antenna for connecting signals.

[0017] The beneficial effects of the present invention are as follows: through the cooperative setting of the sensing component and the signal transceiver module, the sensing component is used to detect whether someone passes by and sends the monitoring results to the microcontroller and the signal transceiver module. When someone passes by, the microcontroller controls the full-spectrum lighting to work;

[0018] Through the setting of the adjustment mechanism, the transmission gear and the toothed disc are meshed and transmitted, so that the toothed disc drives the bearing seat 1 to perform forward and reverse rotation adjustment, so that the bearing seat 1 drives the pillar to rotate the angle through the connecting column; and the rotating shaft 2 drives the rotating shaft 1 to rotate through the rotation of the shaft rods 1 and 2 and the shaft rods 3 and 4 and through the movable parts, so that the rotating shaft 1 drives the pillar to rotate and adjust through the connecting column, thereby adjusting the position angle of the full-spectrum lighting lamp, and can lower the height of the lighting device at a high place to facilitate its maintenance operation, thereby greatly facilitating the maintenance of the lighting device. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0020] Figure 1 2 is a schematic structural diagram of an emergency intelligent induction lighting device for civil air defense projects according to an embodiment of the present invention;

[0021] Figure 2 This is a structural diagram of an adjustment mechanism in an emergency intelligent induction lighting device for civil air defense projects according to an embodiment of the present invention;

[0022] Figure 3 is a side view of a side panel of an emergency intelligent induction lighting device for civil air defense projects according to an embodiment of the present invention;

[0023] Figure 4 The figure is a structural schematic diagram of a universal joint in an emergency intelligent induction lighting device for civil air defense projects according to an embodiment of the present invention.

[0024] In the picture:

[0025] 1. Mounting frame; 2. Connecting frame; 3. Pillar; 4. Lamp holder; 5. Full-spectrum lighting; 6. Protective cover; 7. Sensing component; 8. Thermal sensor; 9. Electronic eye; 10. Photoelectric sensor; 11. Housing; 12. Side panel; 13. Spur; 14. Bearing seat 1; 15. Rotating shaft 1; 16. Connecting column; 17. Transmission gear; 18. Servo motor 1; 19. Limiting piece; 20. Limiting column; 21. Bearing seat 2; 22. Rotating shaft 2; 23. Shaft 1; 24. Shaft 2; 25. Universal joint; 26. Shaft 3; 27. Shaft 4; 28. Servo motor 2; 29. Travel hole; 30. Signal transceiver module; 31. Antenna. DETAILED DESCRIPTION

[0026] To further illustrate each embodiment, the present invention provides drawings, which are part of the disclosure of the present invention. They are mainly used to illustrate the embodiments and can be used in conjunction with the relevant descriptions in the specification to explain the operating principles of the embodiments. By referring to these contents, ordinary technicians in this field should be able to understand other possible implementation methods and advantages of the present invention. The components in the figures are not drawn to scale, and similar component symbols are generally used to represent similar components.

[0027] According to an embodiment of the present invention, an emergency intelligent induction lighting device for civil air defense projects is provided.

[0028] Example 1:

[0029] like Figure 1-4 As shown, the emergency intelligent induction lighting device for civil air defense projects according to an embodiment of the present invention includes a mounting frame 1 and a connecting frame 2. The connecting frame 2 is located on one side of the mounting frame 1, and the other side of the connecting frame 2 is symmetrically provided with a laterally arranged pillar 3. The end of the pillar 3 is provided with a lamp holder 4. The bottom of the lamp holder 4 is provided with a full-spectrum lighting lamp 5. The full-spectrum lighting lamp 5 is provided with a protective cover 6 connected to the lamp holder 4. The connecting frame 2 is provided with an adjustment mechanism for adjusting the angle of the full-spectrum lighting lamp 5.

[0030] A sensing component 7 is provided on one side of the lamp holder 4. The sensing component 7 includes a thermal energy sensor 8, an electronic eye 9 and a photoelectric sensor 10. The thermal energy sensor 8, the electronic eye 9 and the photoelectric sensor 10 are electrically connected to the microcontroller in the lamp holder 4.

[0031] Example 2:

[0032] like Figure 1-4 As shown, the adjustment mechanism includes a shell 11 located on one side of the connecting frame 2, a side plate 12 is provided in the shell 11, a gear plate 13 is provided on one side of the side plate 12, a horizontally arranged bearing seat 14 is provided on one side of the gear plate 13, the bearing seat 14 is movably connected to a rotating shaft 15, and the end of the rotating shaft 15 is provided with a connecting column 16 extending to the outside of the shell 11 and connected to the pillar 3.

[0033] A transmission gear 17 meshing with the gear plate 13 is provided on one side of the side plate 12 , and the axis of the transmission gear 17 is connected to the output shaft of the servo motor 18 of the housing 11 .

[0034] A limiting member 19 is provided on one side of the gear disc 13 and between the bearing seat 14 and the transmission gear 17 , and a limiting column 20 matching the limiting member 19 is symmetrically provided on one side of the side plate 12 .

[0035] Example 3:

[0036] like Figure 1-4 As shown, a vertically arranged bearing seat 21 is provided on one side of the side plate 12 and above the gear disc 13, and a rotating shaft 22 is movably connected to the bearing seat 21. The bottom end of the rotating shaft 22 is provided with a shaft rod 1 23 and a shaft rod 24 symmetrically arranged in pairs.

[0037] The end of the rotating shaft 15 away from the connecting column 16 is provided with axle rods 3 26 and axle rods 4 27 arranged symmetrically in pairs, two groups of the axle rods 3 26 are movably connected to the axle rods 1 23 in pairs, and two groups of the axle rods 4 27 are movably connected to the axle rods 24 in pairs.

[0038] The shaft 1 23 and the shaft 2 24 are movably connected to the shaft 3 26 and the shaft 4 27 via a universal joint 25 . A servo motor 2 28 for driving the rotating shaft 2 22 is provided on the side plate 12 .

[0039] Example 4:

[0040] like Figure 1-4 As shown, a travel hole 29 is provided on the housing 11 for the movement of the connecting column 16 , and the housing 11 is connected to the connecting frame 2 by bolts.

[0041] The length of the shaft 1 23 is smaller than the length of the shaft 2 24 , and the length of the shaft 3 26 is smaller than the length of the shaft 4 27 .

[0042] The thermal energy sensor 8 is an infrared sensor. The connecting frame 2 is provided with a signal transceiver module 30 electrically connected to the sensing component 7. An antenna 31 for connecting signals is provided on one side of the signal transceiver module 30.

[0043] In order to facilitate understanding of the above technical solutions of the present invention, the working principle or operation mode of the present invention in actual process is described in detail below.

[0044] In actual application, the thermal energy sensor 8, the electronic eye 9 and the photoelectric sensor 10 monitor whether someone passes by, and send the monitoring results to the microcontroller and the signal transceiver module 30. The signal transceiver module 30 can receive the signal and send instructions to the microcontroller, and the microcontroller controls the operation of the full-spectrum lighting lamp 5;

[0045] When the angle of the full-spectrum lighting lamp 5 needs to be adjusted, the servo motor 18 is started to drive the transmission gear 17 to rotate forward and reverse. The transmission gear 17 engages with the toothed disc 13 for transmission, so that the toothed disc 13 drives the bearing seat 14 to move in a circle. The bearing seat 14 drives the connecting column 16 to rotate in the stroke hole 29 through the rotating shaft 15, so that the connecting column 16 drives the lamp holder 4 and its full-spectrum lighting lamp 5 to rotate in the left and right directions through the pillar 3, and the servo motor 2 28 drives the rotating shaft 2 22 to rotate in the bearing seat 2 21, so that the rotating shaft 2 22 drives the shaft 1 23 and the shaft 2 24 to rotate, and the shaft 1 23 and the shaft 2 24 drive the shaft 3 26 and the shaft 4 27 to rotate through the universal joint 25, so that the shaft 3 26 and the shaft 4 27 drive the rotating shaft 15 to rotate, so that the rotating shaft 15 drives the pillar 3 to rotate through the connecting column 16, and the pillar 3 drives the lamp holder 4 and its full-spectrum lighting lamp 5 to rotate and adjust.

[0046] In summary, with the help of the above technical solution of the present invention, through the cooperative arrangement of the sensing component 7 and the signal transceiver module 30, the sensing component 7 is used to detect whether a person passes by and sends the monitoring result to the microcontroller and the signal transceiver module 30. When a person passes by, the microcontroller controls the full-spectrum lighting 5 to work;

[0047] Through the setting of the adjustment mechanism, the transmission gear 17 is meshed with the toothed disc 13 for transmission, so that the toothed disc 13 drives the bearing seat 14 to perform forward and reverse rotation adjustment, so that the bearing seat 14 drives the pillar 3 to rotate the angle through the connecting column 16; and the rotating shaft 2 22 drives the rotating shaft 15 to rotate through the rotation of the shaft rod 1 23 and the shaft rod 2 24 and the shaft rod 3 26 and the shaft rod 4 27 and through the movable parts, so that the rotating shaft 15 drives the pillar 3 to rotate and adjust through the connecting column 16, thereby adjusting the position angle of the full-spectrum lighting lamp 5, and can lower the height of the lighting device at a high place to facilitate the maintenance operation, thereby greatly facilitating the maintenance of the lighting device.

[0048] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of protection of the present invention.

Claims

1. An emergency intelligent induction lighting device for civil air defense projects, characterized in that: The invention comprises a mounting frame (1) and a connecting frame (2), wherein the connecting frame (2) is located on one side of the mounting frame (1), and a laterally arranged pillar (3) is symmetrically provided on the other side of the connecting frame (2), and a lamp holder (4) is provided at the end of the pillar (3), and a full-spectrum lighting lamp (5) is provided at the bottom of the lamp holder (4), and a protective cover (6) connected to the lamp holder (4) is provided on the full-spectrum lighting lamp (5), and an adjustment mechanism for adjusting the angle of the full-spectrum lighting lamp (5) is provided on the connecting frame (2); A sensing component (7) is provided on one side of the lamp holder (4), and the sensing component (7) includes a thermal energy sensor (8), an electronic eye (9), and a photoelectric sensor (10). The thermal energy sensor (8), the electronic eye (9), and the photoelectric sensor (10) are electrically connected to a microcontroller in the lamp holder (4).

2. The emergency intelligent induction lighting device for civil air defense engineering according to claim 1, characterized in that: The adjustment mechanism includes a shell (11) located on one side of the connecting frame (2), a side plate (12) is provided in the shell (11), a gear disc (13) is provided on one side of the side plate (12), a bearing seat (14) is provided on one side of the gear disc (13), the bearing seat (14) is movably connected to a rotating shaft (15), and the end of the rotating shaft (15) is provided with a connecting column (16) extending outside the shell (11) and connected to the pillar (3).

3. The intelligent emergency induction lighting device for civil air defense projects according to claim 2, characterized in that: A transmission gear (17) meshing with the toothed disc (13) is provided on one side of the side plate (12), and the axis of the transmission gear (17) is connected to an output shaft of a servo motor (18) of the housing (11).

4. The intelligent emergency induction lighting device for civil air defense projects according to claim 3, characterized in that: A limiting member (19) is provided on one side of the toothed disc (13) and located between the bearing seat 1 (14) and the transmission gear (17), and a limiting column (20) matching the limiting member (19) is symmetrically provided on one side of the side plate (12).

5. The intelligent induction lighting device for emergency use in civil air defense projects according to claim 4, characterized in that: A vertically arranged bearing seat 2 (21) is provided on one side of the side plate (12) and above the gear disc (13); a rotating shaft 2 (22) is movably connected to the bearing seat 2 (21); and a bottom end of the rotating shaft 2 (22) is provided with a shaft rod 1 (23) and a shaft rod 2 (24) symmetrically arranged in pairs.

6. The intelligent induction lighting device for emergency use in civil air defense projects according to claim 5, characterized in that: The end of the rotating shaft 1 (15) away from the connecting column (16) is provided with two symmetrically arranged shaft rods 3 (26) and shaft rods 4 (27), two groups of the shaft rods 3 (26) are movably connected to the two shaft rods 1 (23) respectively, and two groups of the shaft rods 4 (27) are movably connected to the two shaft rods 2 (24) respectively.

7. The intelligent emergency induction lighting device for civil air defense projects according to claim 6, characterized in that: The shaft rod 1 (23) and the shaft rod 2 (24) are movably connected to the shaft rod 3 (26) and the shaft rod 4 (27) via a universal joint (25), and a servo motor 2 (28) for driving the rotating shaft 2 (22) is provided on the side plate (12).

8. The intelligent emergency induction lighting device for civil air defense projects according to claim 7, characterized in that: The housing (11) is provided with a travel hole (29) for the connection column (16) to move, and the housing (11) is connected to the connection frame (2) via bolts.

9. The intelligent induction lighting device for emergency use in civil air defense projects according to claim 8, characterized in that: The length of the shaft rod one (23) is smaller than the length of the shaft rod two (24), and the length of the shaft rod three (26) is smaller than the length of the shaft rod four (27).

10. The intelligent emergency induction lighting device for civil air defense projects according to claim 1, characterized in that: The thermal energy sensor (8) is an infrared sensor. A signal transceiver module (30) electrically connected to the sensing component (7) is provided on the connecting frame (2). An antenna (31) for connecting signals is provided on one side of the signal transceiver module (30).

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