CN201351839Y - Aviation obstruction lamp with high light intensity - Google Patents
Aviation obstruction lamp with high light intensity Download PDFInfo
- Publication number
- CN201351839Y CN201351839Y CNU2009200500416U CN200920050041U CN201351839Y CN 201351839 Y CN201351839 Y CN 201351839Y CN U2009200500416 U CNU2009200500416 U CN U2009200500416U CN 200920050041 U CN200920050041 U CN 200920050041U CN 201351839 Y CN201351839 Y CN 201351839Y
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- CN
- China
- Prior art keywords
- lamp
- light intensity
- aviation obstruction
- high light
- fluorescent tube
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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- Non-Portable Lighting Devices Or Systems Thereof (AREA)
Abstract
The utility model discloses an aviation obstruction lamp with high light intensity. The aviation obstruction lamp comprises an electric box and a lamp structure which are mutually connected. The lamp structure comprises a lamp shell, a lamp tube, a lamp tube clip, a paraboloid reflector and a reflector bracket. The lamp tube is fixedly arranged on the lamp tube clip, the lamp tube and the lamp tube clip are located in the paraboloid reflector, the lamp tube clip and the paraboloid reflector are fixedly connected with the reflector bracket, and the paraboloid reflector is arranged in the lamp shell. A lens is arranged at the front end of the lamp shell, and the lamp shell is connected with the lens by a lens focal length adjusting rod. The aviation obstruction lamp with high light intensity can effectively control emergence angles of vertical light rays within 3 to 7 DEG (the standard requirements of the aviation obstruction lamp). The aviation obstruction lamp with high light intensity can well concentrate light rays, leads high illumination, and meets the national standards.
Description
Technical field
The utility model relates to the equipment of superelevation obstruction marker effect, is specifically related to a kind of high light intensity aviation obstruction beacon.
Background technology
The light of existing aviation obstruction beacon is that omnidirectional is luminous or use common floodlight transformation, and the weak and light of light intensity disperses very much, can not satisfy high light intensity obstruction light alignment request.
Summary of the invention
The utility model is in order to overcome the deficiency that above prior art exists, provide a kind of rational in infrastructure, light is concentrated, the high high light intensity aviation obstruction beacon of brightness.
The purpose of this utility model realizes by following technical scheme: this high light intensity aviation obstruction beacon, comprise interconnective electric box and modulated structure, it is characterized in that: described modulated structure comprises lamp housing, fluorescent tube, fluorescent tube card, parabolic reflector and reflector bracket, fluorescent tube is fixed on the fluorescent tube card, fluorescent tube and fluorescent tube are positioned in the parabolic reflector, the fluorescent tube card is fixedlyed connected with reflector bracket with parabolic reflector, and parabolic reflector is positioned at lamp housing.
The front end of described lamp housing is provided with lens.
Scioptics focus adjustment bar connects between described lamp housing and the lens.
Described lamp housing is provided with the face glass that is used to seal lamp housing and printing opacity effect.
Described lamp housing side is provided with the lock screw that is used for fixing parabolic reflector.
Connect by connecting steel pipe between described electric box and the modulated structure.
Described fluorescent tube card is fixedlyed connected with reflector bracket by screw with parabolic reflector.
The utility model has following advantage with respect to prior art:
One, this high light intensity aviation obstruction beacon improves the structure of existing aviation obstruction beacon, and the light of fluorescent tube has become and decided the direction ejaculation, and then penetrated through lens refraction back through the parabolic reflector reflection.And scioptics focus adjustment bar connects between lamp housing and the lens, can regulate the focal length of lens by regulating focal length of lens adjusting rod, and then regulate the vertical shooting angle of light.
Two, this high light intensity aviation obstruction beacon can make the vertical light line angle of emergence effectively be controlled in 3～7 degree of aviation obstruction beacon standard-required.
Three, this high light intensity aviation obstruction beacon concentrates light better, and the brightness height satisfies national standard.
Description of drawings
Fig. 1 is the longitudinal sectional view of a kind of high light intensity aviation obstruction beacon of the utility model.
Fig. 2 is the side view of high light intensity aviation obstruction beacon.
Fig. 3 is the front view of high light intensity aviation obstruction beacon.
Fig. 4 is the stereogram of high light intensity aviation obstruction beacon.
The specific embodiment
The utility model is described in further detail below in conjunction with drawings and Examples.
A kind of high light intensity aviation obstruction beacon as shown in Figure 1, comprise by connecting steel pipe 1 interconnective electric box 2 and modulated structure 3, modulated structure 3 comprises lamp housing 4, fluorescent tube 5, fluorescent tube card 6, parabolic reflector 7 and reflector bracket 8, fluorescent tube 5 is fixed on the fluorescent tube card 6, fluorescent tube 5 and fluorescent tube card 6 are positioned at parabolic reflector 7, fluorescent tube card 6 is fixedlyed connected with reflector bracket 8 by screw 14 with parabolic reflector 7, and parabolic reflector 7 is positioned at lamp housing 4.
The front end of lamp housing 4 is provided with lens 9.Scioptics focus adjustment bar 11 connects between lamp housing 4 and the lens 9.Lamp housing 4 is provided with the face glass 12 that is used to seal lamp housing 4 and printing opacity effect.Lamp housing 4 sides are provided with the lock screw 13 that is used for fixing parabolic reflector 7.
This high light intensity aviation obstruction beacon, the light of fluorescent tube 5 have become and have decided the direction ejaculation through parabolic reflector 7 reflections, and then penetrate through lens 9 refraction backs.And scioptics focus adjustment bar 11 connects between lamp housing 4 and the lens 9, can regulate the focal length of lens 9 by regulating focal length of lens adjusting rod 11, and then regulate the vertical shooting angle of light.This high light intensity aviation obstruction beacon can make the vertical light line angle of emergence effectively be controlled in 3～7 degree of aviation obstruction beacon standard-required.
The above-mentioned specific embodiment is a preferred embodiment of the present utility model; can not limit claim of the present utility model; other any change that does not deviate from the technical solution of the utility model and made or other equivalent substitute mode are included within the protection domain of the present utility model.
Claims (7)
1, high light intensity aviation obstruction beacon, comprise interconnective electric box and modulated structure, it is characterized in that: described modulated structure comprises lamp housing, fluorescent tube, fluorescent tube card, parabolic reflector and reflector bracket, fluorescent tube is fixed on the fluorescent tube card, fluorescent tube and fluorescent tube are positioned in the parabolic reflector, the fluorescent tube card is fixedlyed connected with reflector bracket with parabolic reflector, and parabolic reflector is positioned at lamp housing.
2, high light intensity aviation obstruction beacon according to claim 1, it is characterized in that: the front end of described lamp housing is provided with lens.
3, high light intensity aviation obstruction beacon according to claim 2 is characterized in that: scioptics focus adjustment bar connects between described lamp housing and the lens.
4, high light intensity aviation obstruction beacon according to claim 1, it is characterized in that: described lamp housing is provided with the face glass that is used to seal lamp housing and printing opacity effect.
5, high light intensity aviation obstruction beacon according to claim 1, it is characterized in that: described lamp housing side is provided with the lock screw that is used for fixing parabolic reflector.
6, high light intensity aviation obstruction beacon according to claim 1 is characterized in that: connect by connecting steel pipe between described electric box and the modulated structure.
7, high light intensity aviation obstruction beacon according to claim 1, it is characterized in that: described fluorescent tube card is fixedlyed connected with reflector bracket by screw with parabolic reflector.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2009200500416U CN201351839Y (en) | 2009-01-13 | 2009-01-13 | Aviation obstruction lamp with high light intensity |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2009200500416U CN201351839Y (en) | 2009-01-13 | 2009-01-13 | Aviation obstruction lamp with high light intensity |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201351839Y true CN201351839Y (en) | 2009-11-25 |
Family
ID=41375226
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2009200500416U Expired - Lifetime CN201351839Y (en) | 2009-01-13 | 2009-01-13 | Aviation obstruction lamp with high light intensity |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201351839Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108966454A (en) * | 2018-06-13 | 2018-12-07 | 苏州创存数字科技有限公司 | A kind of aviation obstruction light system based on optical path prompt |
| CN113551202A (en) * | 2020-04-26 | 2021-10-26 | 湖南辰东科技有限公司 | Combined optical device of full-concave parabolic reflector |
-
2009
- 2009-01-13 CN CNU2009200500416U patent/CN201351839Y/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108966454A (en) * | 2018-06-13 | 2018-12-07 | 苏州创存数字科技有限公司 | A kind of aviation obstruction light system based on optical path prompt |
| CN108966454B (en) * | 2018-06-13 | 2019-12-06 | 滁州善树商贸有限公司 | Aviation obstruction light system based on light path suggestion |
| CN113551202A (en) * | 2020-04-26 | 2021-10-26 | 湖南辰东科技有限公司 | Combined optical device of full-concave parabolic reflector |
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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: 20091125 |
|
| DD01 | Delivery of document by public notice | ||
| DD01 | Delivery of document by public notice |
Addressee: Wang Yalong Document name: Notification of Expiration of Patent Right Duration |