CN202581107U - Red medium-light-intensity aviation obstruction lamp - Google Patents
Red medium-light-intensity aviation obstruction lamp Download PDFInfo
- Publication number
- CN202581107U CN202581107U CN 201220260613 CN201220260613U CN202581107U CN 202581107 U CN202581107 U CN 202581107U CN 201220260613 CN201220260613 CN 201220260613 CN 201220260613 U CN201220260613 U CN 201220260613U CN 202581107 U CN202581107 U CN 202581107U
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- power supply
- light
- holder
- aviation obstruction
- chamber
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- Expired - Lifetime
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Abstract
The utility model discloses a red medium-light-intensity aviation obstruction lamp which comprises a luminous chamber, a power supply chamber and a fixing seat, wherein the luminous chamber consists of a lamp shade; the power supply chamber consists of a lamp body; the fixing seat is arranged between the luminous chamber and the power supply chamber; a luminous device and a power supply device are respectively arranged on an upper surface and a lower surface of the fixing seat; the luminous device is positioned in the luminous chamber; the power supply device is positioned in the power supply chamber; and the luminous device is electrically connected with the power supply device. The red medium-light-intensity aviation obstruction lamp disclosed by the utility model has the advantages of low power, easiness in control, extremely-low use cost and safety in use; and all optical parts can be machined or subjected to injection molding by adopting cold stamping, belong to general machine parts and are convenient for machining.
Description
Technical field
The utility model relates to a kind of aviation obstruction beacon, the red aviation obstruction beacon of light intensity in specifically being meant.
Background technology
The peak value efficient intensity of the red flash lamp of middle light intensity reaches 2000～2500cd/m
2, the high-power bulb that present method in common is 150W-1000W satisfies light intensity requirement.Bulb power is big, need control with high-power control system, and the control difficulty is big; Simultaneously, power is big, and heat is big during operation, and cold-resistant heat shocks of lampshade and degree are high, is difficult to realize, high simultaneously heat operation, and potential safety hazard is outstanding; Energy consumption is big in addition, and operating cost is high, and use cost is big.
The utility model content
The purpose of utility model is to provide a kind of middle light intensity red aviation obstruction beacon, and it is simple in structure, and light intensity is very high, and light is evenly distributed.
The implementation of the utility model is following: the red aviation obstruction beacon of middle light intensity; Comprise luminous chamber that constitutes by lampshade and the power supply chamber that constitutes by lamp body; Also comprise the holder that is arranged between luminous chamber and the power supply chamber, the upper surface of holder and lower surface are separately installed with light-emitting device and electric supply installation, and light-emitting device is positioned at luminous chamber; Electric supply installation is positioned at the power supply chamber, and light-emitting device is electrically connected with electric supply installation.
Lampshade is socketed on the outer wall of lamp body through adapter ring.
Mainly endless tube carries out the light source that circumference arranges and constitutes said light-emitting device by the location endless tube that is arranged on the holder upper surface and around the location; Light source is electrically connected with electric supply installation.
The location endless tube also is connected with cover plate away from an end of holder; The annular parabolic trough that is set in the locating ring tube outer surface is installed between cover plate and the holder; Concavees lens also are installed between cover plate and the holder; Wherein light source is positioned at the along of annular parabolic trough, and the opening direction of annular parabolic trough points to concavees lens by the location endless tube, and the opening direction of its concavees lens is relative with the opening direction of annular parabolic trough.
The cross section projection of said annular parabolic trough is free curve shape or is parabola shaped or possesses the oval linear of opening.
Said light source is the red LED light source.
Mainly by at the bottom of the spiral that is arranged on the holder lower surface and be set in that the propeller cap of outer surface constitutes at the bottom of the spiral, propeller cap is connected with installing plate away from the lower surface of holder to said electric supply installation, and installing plate is equipped with the driving box away from the lower surface of propeller cap; Wherein driving box is electrically connected with installing plate and propeller cap.
Also comprise the lamp socket that is connected with lamp body, lamp socket is positioned at the end of lamp body away from lampshade, is provided with the terminal interface plate in the lamp socket, and the terminal interface plate is provided with the power supply terminal of power supply in succession, and wherein power supply terminal is electrically connected with the driving box.
Based on the description of said structure, the utility model is divided into opticator and power pack.
Opticator: the optical system in the utility model mainly is made up of light source, annular parabolic trough, concavees lens that location endless tube, circumference are arranged; Wherein light source is positioned at the along of annular parabolic trough, and the opening direction of annular parabolic trough points to concavees lens by the location endless tube, and the opening direction of its concavees lens is relative with the opening direction of annular parabolic trough.Like this, after the light source luminescent on the focus, a part of light directly is injected on the concavees lens of luminous intensity distribution, and another part is directive annular parabolic trough then, is totally reflected to by annular parabolic trough on the concavees lens of luminous intensity distribution.Originally small, four light penetrated are incident upon on the concavees lens by the whole orientations of annular parabolic trough.After this carries out the distribution of light, penetrate with 360 ° of directed annular again, make the distribution of light intensity and light all meet aviation and use the lamp requirement.
Power pack: through being arranged on the power supply terminal on the terminal interface plate, power supply is introduced in this device, power supply is given current delivery through power supply terminal and is driven box then; Through driving the allocation process of box; Will be through electrical connection, give propeller cap and installing plate with power delivery, the positive and negative electrode at the bottom of the spiral respectively with propeller cap with after installing plate is connected; Energising at the bottom of the spiral is at last through distributing to light source with electric current at the bottom of the spiral.
Lamp socket is by aluminium alloy compression casting, and except being used for installing the lamp body, also electric interfaces has been installed in the chamber within it, is convenient to user installation and uses.The inner chamber of lamp body is an electric panel room, in order to adapt to field work, adopts the secret room structure, and aluminium alloy compression casting housing and the external world good by thermal conductivity carry out heat exchange, improve the working environment of electric device.Lampshade is pressed by Merlon and is formed shape, has designed embedded screw and has been connected with lamp body, is convenient to protect screw not to be soaked with rain.With the optical technology is that the light source design of relying on has been selected general E27 lamp holder interface for use, user-friendly and maintenance.
The design's main points are to be the opticator that relies on the optical technology.All optical elements have all designed locating surface, positioning table, locating hole etc.After accomplishing installation, the luminous point of light source is positioned on the focus by annular parabolic trough just.Obviously, endless tube carries out the LED combined annular light source that formation that circumference arranges carries 12 ° of reflectors to light source around the location, after LED combined annular light source is lighted, sends ring light.A part wherein direct projection forward arrives concavees lens; Another part annular parabolic reflector rooved face that goes directly is totally reflected on the concavees lens by it.The light that penetrates at last forms 360 ° of ring-shaped light spots.
Each optical element can adopt cold punching technology processing, also can adopt the injection mould injection moulding, and on light intensity measuring instrument, carry out light intensity test, repairs mould again, till light intensity and light distribution are qualified.
The advantage of the utility model is: power is very little, and control is easy, and use cost is quite low, and is safe in utilization, and all optical elements can adopt cold stamping processing or injection moulding, belong to general parts, also is convenient to processing.
Description of drawings
Fig. 1 is the overall structure sketch map of the utility model.
Mark and corresponding parts title in the accompanying drawing: 1, lamp socket; 2, terminal interface plate; 3, lamp body; 4, drive box; 5, installing plate; 6, at the bottom of the spiral; 7, adapter ring; 8, lampshade; 9, propeller cap; 10, holder; 11, concavees lens; 12, annular parabolic trough; 13, location endless tube; 14, cover plate; 15, light source.
The specific embodiment
Embodiment one
As shown in Figure 1.
The red aviation obstruction beacon of middle light intensity; Comprise luminous chamber that constitutes by lampshade 8 and the power supply chamber that constitutes by lamp body 3; Also comprise the holder 10 that is arranged between luminous chamber and the power supply chamber, the upper surface of holder 10 and lower surface are separately installed with light-emitting device and electric supply installation, and light-emitting device is positioned at luminous chamber; Electric supply installation is positioned at the power supply chamber, and light-emitting device is electrically connected with electric supply installation.Lampshade 8 is socketed on the outer wall of lamp body 3 through adapter ring 7.Mainly endless tube 13 carries out the light source 15 that circumference arranges and constitutes said light-emitting device by the location endless tube 13 that is arranged on holder 10 upper surfaces and around the location; Light source 15 is electrically connected with electric supply installation.Location endless tube 13 also is connected with cover plate 14 away from an end of holder 10; The annular parabolic trough 12 that is set in location endless tube 13 outer surfaces is installed between cover plate 14 and the holder 10; Between cover plate 14 and the holder 10 concavees lens 11 are installed also; Wherein light source 15 is positioned at the along of annular parabolic trough 12, and the opening direction of annular parabolic trough 12 points to concavees lens 11 by location endless tube 13, and the opening direction of the opening direction of its concavees lens 11 and annular parabolic trough 12 is relative.Said light source 15 is the red LED light source.The cross section projection of said annular parabolic trough 12 is free curve shape or is parabola shaped or possesses the oval linear of opening.
Said electric supply installation is mainly by at the bottom of the spiral that is arranged on holder 10 lower surfaces 6 and be set in that the propeller cap 9 of 6 outer surfaces constitutes at the bottom of the spiral; Propeller cap 9 is connected with installing plate 5 away from the lower surface of holder 10, and installing plate 5 is equipped with driving box 4 away from the lower surface of propeller cap 9; Wherein driving box 4 is electrically connected with installing plate 5 and propeller cap 9.Also comprise the lamp socket 1 that is connected with lamp body 3, lamp socket 1 is positioned at the end of lamp body 3 away from lampshade 8, is provided with terminal interface plate 2 in the lamp socket 1, and terminal interface plate 2 is provided with the power supply terminal of power supply in succession, and wherein power supply terminal is electrically connected with driving box 4.
The utility model is divided into opticator and power pack.
Opticator: the optical system in the utility model mainly is made up of light source 15, annular parabolic trough 12, concavees lens 11 that location endless tube 13, circumference are arranged; Wherein light source 15 is positioned at the along of annular parabolic trough 12, and the opening direction of annular parabolic trough 12 points to concavees lens 11 by location endless tube 13, and the opening direction of the opening direction of its concavees lens 11 and annular parabolic trough 12 is relative.Like this, after the light source luminescent on the focus, a part of light directly is injected on the concavees lens of luminous intensity distribution, and another part is directive annular parabolic trough then, is totally reflected to by annular parabolic trough on the concavees lens of luminous intensity distribution.Originally small, four light penetrated are incident upon on the concavees lens by the whole orientations of annular parabolic trough.After this carries out the distribution of light, penetrate with 360 ° of directed annular again, make the distribution of light intensity and light all meet aviation and use the lamp requirement.
Power pack: through being arranged on the power supply terminal on the terminal interface plate 2, power supply is introduced in this device, power supply is given current delivery through power supply terminal and is driven box 4 then; Through driving the allocation process of box 4; Will be through electrical connection, give propeller cap 9 and installing plate 5 with power delivery, at the bottom of the spiral 6 positive and negative electrode respectively with propeller cap 9 with after installing plate 5 is connected; 6 energisings at the bottom of the spiral are at last through 6 distributing to light source with electric current at the bottom of the spiral.
Lamp socket 1 is by aluminium alloy compression casting, and except being used for installing the lamp body 4, also electric interfaces has been installed in the chamber within it, is convenient to user installation and uses.The inner chamber of lamp body 3 is an electric panel room, in order to adapt to field work, adopts the secret room structure, and aluminium alloy compression casting housing and the external world good by thermal conductivity carry out heat exchange, improve the working environment of electric device.Lampshade 8 is pressed by Merlon and is formed shape, has designed embedded screw and has been connected with lamp body 3, is convenient to protect screw not to be soaked with rain.The general E27 lamp holder interface that has been the led light source design Selection of relying on the optical technology, user-friendly and safeguard.
The design's key is to be the opticator that relies on the optical technology.All optical elements have all designed locating surface, positioning table, locating hole etc.After accomplishing installation, the luminous point of light source is positioned on the focus by annular parabolic trough just.Obviously, endless tube 13 carries out the LED combined annular light source that formation that circumference arranges carries 12 ° of reflectors to light source 15 around the location, after LED combined annular light source is lighted, sends ring light.A part wherein direct projection forward arrives concavees lens; Another part annular parabolic reflector rooved face that goes directly is totally reflected on the concavees lens by it.The light that penetrates at last forms 360 ° of ring-shaped light spots.
Each optical element can adopt cold punching technology processing, also can adopt the injection mould injection moulding, and on light intensity measuring instrument, carry out light intensity test, repairs mould again, till light intensity and light distribution are qualified.
As stated, then can well realize the utility model.
Claims (8)
1. the red aviation obstruction beacon of middle light intensity; It is characterized in that: comprise luminous chamber that constitutes by lampshade (8) and the power supply chamber that constitutes by lamp body (3); Also comprise the holder (10) that is arranged between luminous chamber and the power supply chamber, the upper surface and the lower surface of holder (10) are separately installed with light-emitting device and electric supply installation, and light-emitting device is positioned at luminous chamber; Electric supply installation is positioned at the power supply chamber, and light-emitting device is electrically connected with electric supply installation.
2. the red aviation obstruction beacon of light intensity in according to claim 1, it is characterized in that: lampshade (8) is socketed on the outer wall of lamp body (3) through adapter ring (7).
3. the red aviation obstruction beacon of light intensity in according to claim 1 is characterized in that: said light-emitting device mainly carries out light source (15) formation that circumference is arranged by the location endless tube (13) that is arranged on holder (10) upper surface and around location endless tube (13); Light source (15) is electrically connected with electric supply installation.
4. the red aviation obstruction beacon of light intensity in according to claim 3, it is characterized in that: location endless tube (13) also is connected with cover plate (14) away from an end of holder (10); The annular parabolic trough (12) that is set in location endless tube (13) outer surface is installed between cover plate (14) and the holder (10); Between cover plate (14) and the holder (10) concavees lens (11) are installed also; Wherein light source (15) is positioned at the along of annular parabolic trough (12); And the opening direction of annular parabolic trough (12) points to concavees lens (11) by location endless tube (13), and the opening direction of opening direction of its concavees lens (11) and annular parabolic trough (12) is relative.
5. the red aviation obstruction beacon of light intensity in according to claim 4, it is characterized in that: the cross section projection of said annular parabolic trough (12) is free curve shape or is parabola shaped or possesses the oval linear of opening.
6. the red aviation obstruction beacon of light intensity in according to claim 3, it is characterized in that: said light source (15) is the red LED light source.
7. according to any red aviation obstruction beacon of described middle light intensity among the claim 1-6; It is characterized in that: said electric supply installation mainly by (6) at the bottom of the spiral that is arranged on holder (10) lower surface and at the bottom of being set in spiral the propeller cap (9) of (6) outer surface constitute; Propeller cap (9) is connected with installing plate (5) away from the lower surface of holder (10), and installing plate (5) is equipped with driving box (4) away from the lower surface of propeller cap (9); Wherein driving box (4) is electrically connected with installing plate (5) and propeller cap (9).
8. the red aviation obstruction beacon of light intensity in according to claim 7; It is characterized in that: also comprise the lamp socket (1) that is connected with lamp body (3); Lamp socket (1) is positioned at the end of lamp body (3) away from lampshade (8); Be provided with terminal interface plate (2) in the lamp socket (1), terminal interface plate (2) is provided with the power supply terminal of power supply in succession, and wherein power supply terminal is electrically connected with driving box (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220260613 CN202581107U (en) | 2012-06-05 | 2012-06-05 | Red medium-light-intensity aviation obstruction lamp |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220260613 CN202581107U (en) | 2012-06-05 | 2012-06-05 | Red medium-light-intensity aviation obstruction lamp |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202581107U true CN202581107U (en) | 2012-12-05 |
Family
ID=47250514
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220260613 Expired - Lifetime CN202581107U (en) | 2012-06-05 | 2012-06-05 | Red medium-light-intensity aviation obstruction lamp |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202581107U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110131626A (en) * | 2019-06-13 | 2019-08-16 | 吉林省全星航空技术有限公司 | Multilayer obstruction light |
-
2012
- 2012-06-05 CN CN 201220260613 patent/CN202581107U/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110131626A (en) * | 2019-06-13 | 2019-08-16 | 吉林省全星航空技术有限公司 | Multilayer obstruction light |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20121205 |