CN216684880U - Aviation obstruction beacon for helicopter - Google Patents
Aviation obstruction beacon for helicopter Download PDFInfo
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- CN216684880U CN216684880U CN202122282658.4U CN202122282658U CN216684880U CN 216684880 U CN216684880 U CN 216684880U CN 202122282658 U CN202122282658 U CN 202122282658U CN 216684880 U CN216684880 U CN 216684880U
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Abstract
The utility model discloses an aviation obstruction light for a helicopter, which comprises a flash light component, a lamp shade component, an aviation lamp base, an aviation lamp box body and a control component, wherein the aviation lamp box body comprises two box body positioning frames which correspond up and down, a stand column is arranged between four corners of the two box body positioning frames, a solar panel is arranged between the two box body positioning frames, the solar panel is provided with the control component, the control component is connected with the solar panel through a lead, the lower surface of the lower box body positioning frame is connected with the aviation lamp base through a bolt, the aviation lamp base is connected with the control component through a lead, the upper surface of the upper box body positioning frame is connected with the lamp shade component through a bolt, and the device can be controlled through a control panel box and a liquid crystal screen. The receiving angle is wide, and the requirements of people can be met.
Description
Technical Field
The utility model relates to the technical field of aviation obstruction lamps for helicopters, in particular to an aviation obstruction lamp for helicopters.
Background
The aviation obstruction light can help a helicopter operator to judge the height and the outline of an obstacle, plays a role in warning, can meet the obstacle avoidance requirements of the helicopter in the flying and taking off and landing processes, but the existing aviation obstruction light is powered through the outside, has poor sensitivity, small receiving angle and can not meet the requirements of people.
SUMMERY OF THE UTILITY MODEL
The technical problem to be solved by the utility model is to overcome the existing defects, and provide the aviation obstruction light for the helicopter, which is simple in structure, convenient to install, capable of being powered by solar energy, high in sensitivity and wide in receiving angle, capable of meeting the requirements of people, and capable of effectively solving the problems in the background art.
In order to achieve the purpose, the utility model provides the following technical scheme: an aviation obstruction light for a helicopter comprises a flash light component, a lamp shade component, a navigation aid lamp base, a navigation aid lamp box body and a control component, wherein the navigation aid lamp box body comprises two box body positioning frames which vertically correspond to each other, a stand column is arranged between four corners of the two box body positioning frames, a solar panel is arranged between the two box body positioning frames, the solar panel is provided with the control component, the control component is connected with the solar panel through a lead, the lower surface of the lower box body positioning frame is connected with the navigation aid lamp base through a bolt, the navigation aid lamp base is connected with the control component through a lead, the upper surface of the upper box body positioning frame is connected with the lamp shade component through a bolt, the lower surface of the lamp shade component is provided with the flash light component, the flash light component is positioned in the navigation aid lamp box body and is connected with the navigation aid lamp base through a lead, and the flash light component comprises a supporting frame connected with the lamp shade component through a threaded connection mode, the lower extreme of support frame is equipped with solar control assembly, and solar control assembly passes through the wire and is connected with solar panel, the centre of support frame is equipped with master control circuit subassembly, and the upper end of support frame is equipped with the flash light, and the flash light passes through master control circuit subassembly to be connected with solar control assembly through the wire, can be to throwing light on through the flash light.
Furthermore, the control assembly comprises a liquid crystal screen and a control panel box, the liquid crystal screen is connected with the control panel box through a wire, and the device can be controlled through the control panel box and the liquid crystal screen.
Further, the aid to navigation lamp base includes lower extreme flange, and lower extreme flange's upper surface is equipped with circuit mounting panel and battery, and the battery passes through the battery buckle to be connected with lower extreme flange upper surface, can provide the electric energy for the device through the battery.
Further, the lamp shade subassembly includes the upper end flange of being connected with box location frame, and upper end flange's upper surface center is equipped with fresnel lampshade, and is equipped with two antennas on the upper end flange, and two antennas are location antenna and communication antenna respectively, can protect through fresnel lampshade, and make the light source disperse the angle wider through fresnel lampshade, and can fix a position and communicate through location antenna and communication antenna.
Furthermore, a sealing ring is arranged between the Fresnel lamp cover and the upper end connecting flange, a lifting handle is arranged on one side of the upper end connecting flange, and the device is more convenient to carry through the lifting handle.
Compared with the prior art, the utility model has the beneficial effects that: this aviation obstruction lamp for helicopter can protect through fresnel lampshade, and makes the light source divergence angle wider through fresnel lampshade, and can fix a position and the communication through location antenna and communication antenna, can control the device through control panel box and LCD screen, this aviation obstruction lamp for helicopter, simple structure, simple to operate not only can supply power through solar energy, current aviation obstruction lamp sensitivity is high moreover, receiving angle is wide, can satisfy people's demand.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic cross-sectional view of the present invention;
FIG. 3 is a schematic view of a lampshade assembly according to the present invention;
FIG. 4 is a schematic structural diagram of a navigation aid lamp base according to the present invention;
FIG. 5 is a schematic structural diagram of a navigation light box according to the present invention.
In the figure: the solar energy control system comprises a flash lamp assembly 1, a support frame 11, a main control circuit assembly 12, a solar control assembly 13, a flash lamp 14, a lampshade assembly 2, an antenna 21, a Fresnel lampshade 22, an upper end connecting flange 23, a handle 24, a navigation aid lamp base 3, a circuit mounting plate 31, a battery buckle 32, a battery 33, a lower end connecting flange 34, a navigation aid lamp box 4, a box positioning frame 41, a solar panel 42, a stand column 43, a control assembly 5, a liquid crystal display 51 and a control panel box 52.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides a technical solution: an aviation obstruction light for a helicopter comprises a flash light component 1, a lampshade component 2, a navigation light base 3, a navigation light box body 4 and a control component 5, wherein the navigation light box body 4 comprises two box body positioning frames 41 which correspond up and down, a stand column 43 is arranged between four corners of the two box body positioning frames 41, a solar panel 42 is arranged between the two box body positioning frames 41, the solar panel 42 is provided with the control component 5, the control component 5 is connected with the solar panel 42 through a lead, the lower surface of the lower box body positioning frame 41 is connected with the navigation light base 3 through a bolt, the navigation light base 3 is connected with the control component 5 through a lead, the upper surface of the upper box body positioning frame 41 is connected with the lampshade component 2 through a bolt, the lower surface of the lampshade component 2 is provided with a flash light component 1, the flash light component 1 is positioned inside the navigation light box body 4, and the flash light component 1 is connected with the navigation light base 3 through a lead, the flash lamp assembly 1 comprises a support frame 11 connected with a lampshade assembly 2 in a threaded connection mode, a solar control assembly 13 is arranged at the lower end of the support frame 11, the solar control assembly 13 is connected with a solar panel 42 through a lead, a main control circuit assembly 12 is arranged in the middle of the support frame 11, a flash lamp 14 is arranged at the upper end of the support frame 11, red light and white light are emitted by the flash lamp 14, the flash lamp 14 is connected with the solar control assembly 13 through the main control circuit assembly 12 through a lead, illumination can be performed through the flash lamp 14, a control assembly 5 comprises a liquid crystal screen 51 and a control panel box 52, the liquid crystal screen 51 is connected with the control panel box 52 through a lead, the device can be controlled through the control panel box 52 and the liquid crystal screen 51, a navigation aid lamp base 3 comprises a lower end connecting flange 34, and a circuit mounting plate 31 and a battery 33 are arranged on the upper surface of the lower end connecting flange 34, battery 33 passes through battery buckle 32 and 34 upper surface connections of lower extreme flange, can provide the electric energy for the device through battery 33, lamp shade subassembly 2 includes the upper end flange 23 of being connected with box location frame 41, the upper surface center of upper end flange 23 is equipped with fresnel lampshade 22, and be equipped with two antennas 21 on the upper end flange 23, two antennas 21 are location antenna and communication antenna respectively, can protect through fresnel lampshade 22, and can fix a position and the communication through location antenna and communication antenna, be equipped with the sealing washer between fresnel lampshade 22 and the upper end flange 23, one side of upper end flange 23 is equipped with handle 24, it is more convenient to make to carry the device through handle 24.
When in use: can control the switch to flash light 14 through master control circuit module 12 and solar control module 13, send red light and white light by flash light 14, can generate electricity through solar panel 42, can protect through fresnel lampshade 22, and make the light source diverge the angle wider through fresnel lampshade 22, and can fix a position and communicate through location antenna and communication antenna, can control the device through control panel box 52 and LCD screen 51, it is more convenient to make to carry the device through handle 24.
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 utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides an aviation obstruction beacon for helicopter, includes flash of light subassembly (1), lamp shade subassembly (2), navigation aid lamp base (3), navigation aid lamp box (4) and control assembly (5), its characterized in that: the navigation aid lamp box body (4) comprises two box body positioning frames (41) which vertically correspond, a stand column (43) is arranged between four corners of the two box body positioning frames (41), a solar panel (42) is arranged between the two box body positioning frames (41), the solar panel (42) is provided with a control component (5), the control component (5) is connected with the solar panel (42) through a lead, the lower surface of the lower box body positioning frame (41) is connected with a navigation aid lamp base (3) through a bolt, the navigation aid lamp base (3) is connected with the control component (5) through a lead, the upper surface of the upper box body positioning frame (41) is connected with a lampshade component (2) through a bolt, the lower surface of the lampshade component (2) is provided with a flash lamp component (1), the flash component (1) is positioned in the navigation aid lamp box body (4), and the flash component (1) is connected with the navigation aid lamp base (3) through a lead, flash light subassembly (1) include with support frame (11) of being connected through threaded connection's mode and lamp shade subassembly (2), the lower extreme of support frame (11) is equipped with solar control module (13), and solar control module (13) are connected with solar panel (42) through the wire, the centre of support frame (11) is equipped with master control circuit subassembly (12), and the upper end of support frame (11) is equipped with flash light (14), and flash light (14) are connected with solar control module (13) through wire through master control circuit subassembly (12).
2. An aircraft obstruction beacon for a helicopter according to claim 1, wherein: the control assembly (5) comprises a liquid crystal screen (51) and a control panel box (52), and the liquid crystal screen (51) is connected with the control panel box (52) through a lead.
3. An aircraft obstruction beacon for a helicopter according to claim 1, wherein: the navigation aid lamp base (3) comprises a lower end connecting flange (34), the upper surface of the lower end connecting flange (34) is provided with a circuit mounting plate (31) and a battery (33), and the battery (33) is connected with the upper surface of the lower end connecting flange (34) through a battery buckle (32).
4. An aircraft obstruction beacon for a helicopter according to claim 1, wherein: the lamp shade component (2) comprises an upper end connecting flange (23) connected with the box body positioning frame (41), a Fresnel lamp shade (22) is arranged at the center of the upper surface of the upper end connecting flange (23), two antennas (21) are arranged on the upper end connecting flange (23), and the two antennas (21) are respectively a positioning antenna and a communication antenna.
5. An aircraft obstruction light for a helicopter according to claim 4, wherein: a sealing ring is arranged between the Fresnel lamp shade (22) and the upper end connecting flange (23), and a handle (24) is arranged on one side of the upper end connecting flange (23).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122282658.4U CN216684880U (en) | 2021-09-22 | 2021-09-22 | Aviation obstruction beacon for helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122282658.4U CN216684880U (en) | 2021-09-22 | 2021-09-22 | Aviation obstruction beacon for helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216684880U true CN216684880U (en) | 2022-06-07 |
Family
ID=81813834
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122282658.4U Active CN216684880U (en) | 2021-09-22 | 2021-09-22 | Aviation obstruction beacon for helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216684880U (en) |
-
2021
- 2021-09-22 CN CN202122282658.4U patent/CN216684880U/en active Active
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