CN108966454A - A kind of aviation obstruction light system based on optical path prompt - Google Patents
A kind of aviation obstruction light system based on optical path prompt Download PDFInfo
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- CN108966454A CN108966454A CN201810605412.6A CN201810605412A CN108966454A CN 108966454 A CN108966454 A CN 108966454A CN 201810605412 A CN201810605412 A CN 201810605412A CN 108966454 A CN108966454 A CN 108966454A
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- 230000003287 optical effect Effects 0.000 title claims abstract description 63
- 238000004891 communication Methods 0.000 claims abstract description 38
- 230000004888 barrier function Effects 0.000 claims abstract description 36
- 238000012806 monitoring device Methods 0.000 claims description 17
- 238000002347 injection Methods 0.000 claims 1
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- 238000010586 diagram Methods 0.000 description 6
- 230000000007 visual effect Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
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Classifications
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B47/00—Circuit arrangements for operating light sources in general, i.e. where the type of light source is not relevant
- H05B47/10—Controlling the light source
- H05B47/105—Controlling the light source in response to determined parameters
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Abstract
The present invention relates to a kind of aviation obstruction light systems based on optical path prompt, comprising: several are installed on the first lamp body on barrier, further includes: the second lamp body, optical path mirror, communication device, control processor；First lamp body is installed on the edge of barrier, barrier same seamed edge at least there are two the first lamp body；Second lamp body is set to the first lamp body side, and optical path mirror is set to the other side of the first lamp body, and optical path mirror and the second lamp body are on same straight line；Communication device is connect with control processor, and control processor is in communication with each other by communication device and ground control centre；Control processor is connect with the first lamp body, the second lamp body；If having aircraft i.e. will be close to barrier overhead, ground control centre exports the first standby signal to communication device, and communication device exports the first standby signal to control processor, and control processor exports open signal to the second lamp body according to the first standby signal.
Description
Technical field
The present invention relates to airline security device field, in particular to a kind of aviation obstruction light system based on optical path prompt.
Background technique
People's Republic of China's civil aviation professional standard " aviation obstruction beacon (MH/T6012-1999) ", there is obstruction light
Following regulation: the aviation obstruction beacon of barrier setting is necessary for glistening, and has obviously to overlook in the sky with ground constant light source
It distinguishes and can reach and provide remote visual range, aviation obstruction beacon is divided into low light intensity obstruction light, middle light intensity obstruction light and high light intensity
Obstruction light, wherein high light intensity obstruction light is divided into high light intensity A type obstruction light and two kinds of light intensity Type B obstruction light high by lighting requirements.
With the fast development of urban construction, high-rise is also more and more, is limited by land resource, and high level is built
Object is built also increasingly to higher challenge.This brings many advantages to urban construction, but brings certain be stranded to aircraft industry
It disturbs.In the case where the visual field is bad, aviation obstruction beacon is easily ignored to cause tragedy.
Summary of the invention
Goal of the invention:
It is difficult to provide the clear prompt in the bad situation in the visual field for the prior art mentioned in background technique, the present invention provides one
The aviation obstruction light system that kind is prompted based on optical path.
Technical solution:
A kind of aviation obstruction light system based on optical path prompt, comprising: several are installed on the first lamp body on barrier, also wrap
It includes: the second lamp body, optical path mirror, communication device, control processor；
First lamp body is installed on the edge of barrier, barrier same seamed edge at least there are two the first lamp body；
Second lamp body is set to the first lamp body side, and optical path mirror is set to the other side of the first lamp body, optical path mirror and the second lamp body
On same straight line；
Communication device is connect with control processor, and control processor is in communication with each other by communication device and ground control centre；
Control processor is connect with the first lamp body, the second lamp body, and control processor opens letter to the first lamp body/the second lamp body output
Number/shutdown signal, the first lamp body/second lamp body is according to signal execution unlatching/closing；
If having aircraft i.e. will be close to barrier overhead, ground control centre exports the first standby signal, communication to communication device
Device exports the first standby signal to control processor, and control processor is exported to the second lamp body according to the first standby signal and opened
Signal, the second lamp body are opened and form the reflection of optical path by opposite optical path mirror；
If aircraft leaves barrier overhead, ground control centre exports the second standby signal to communication device, communication device to
Control processor exports the second standby signal, and control processor opens shutdown signal to the output of the second lamp body according to standby signal, the
Two lamp bodies are closed.
As a kind of preferred embodiment of the invention, the light that the second lamp body projects is vertical with the mirror surface of optical path mirror.
As a kind of preferred embodiment of the invention, control processor is by communication device control centre's request institute to the ground
The plan schedule in the course line at place, control processor feed back the plan schedule in locating course line to control processor.
As a kind of preferred embodiment of the invention, control processor passes through according to the plan schedule in the course line at place in aircraft
At the time of to the second lamp body export open signal.
It further include weather monitoring device, weather monitoring device and control processor as a kind of preferred embodiment of the invention
Connection；Weather monitoring device is used to monitor the weather condition near barrier, meteorological if meteorological optical range is lower than preset threshold
Monitoring device exports the first standby signal to control processor.
As a kind of preferred embodiment of the invention, if meteorological optical range is lower than preset threshold, and current time is when default
Between in threshold value, then control processor is always on after receiving the first standby signal of weather monitoring device output to the output of the second lamp body
Signal, the second lamp body are opened and are always on.
As a kind of preferred embodiment of the invention, the first lamp body is provided with spare lamp body, spare if the second lamp body is opened
Lamp body is opened.
As a kind of preferred embodiment of the invention, between two adjacent the first lamp bodies, several independent second lamps are set
Body and optical path mirror corresponding with the second lamp body.
As a kind of preferred embodiment of the invention, the light of the second lamp body is pencil.
The present invention realize it is following the utility model has the advantages that
1. becoming linear light source from traditional point light source, optical path, the clearer shape for showing barrier are constituted；
2. only the second lamp body just lights when aircraft passes through, light pollution is reduced；
3. being actively always on the second lamp body when sight is bad.
Detailed description of the invention
The drawings herein are incorporated into the specification and forms part of this specification, and shows the implementation for meeting the disclosure
Example, and consistent with the instructions for explaining the principles of this disclosure.
Fig. 1 is a kind of system block diagram of aviation obstruction light system based on optical path prompt provided by the invention；
Fig. 2 is the system block diagram of the second provided by the invention aviation obstruction light system based on optical path prompt；
Fig. 3 is the system block diagram of the third aviation obstruction light system based on optical path prompt provided by the invention.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.
Embodiment one
With reference to Fig. 1-3, Fig. 1 is a kind of system block diagram of aviation obstruction light system based on optical path prompt provided by the invention；
Fig. 2 is the system block diagram of the second provided by the invention aviation obstruction light system based on optical path prompt；
Fig. 3 is the system block diagram of the third aviation obstruction light system based on optical path prompt provided by the invention.
A kind of aviation obstruction light system based on optical path prompt, comprising: several are installed on the first lamp body on barrier
1, further includes: the second lamp body 2, optical path mirror, communication device 3, control processor.
First lamp body 1 is installed on the edge of barrier, barrier same seamed edge at least there are two the first lamp body 1.
Barrier often has a plurality of seamed edge, and two the first lamp bodies 1 are at least arranged in same seamed edge.In the present embodiment, the rib of barrier
The both ends on side are provided with the first lamp body 1.
Second lamp body 2 is set to 1 side of the first lamp body, and optical path mirror is set to the other side of the first lamp body 1, optical path mirror and
Two lamp bodies 2 are on same straight line.Optical path mirror is reflecting mirror, for the second lamp body 2 to be irradiated light thereon to the second lamp
Body 2 reflects, to constitute optical path.Second lamp body 2 is respectively arranged at the two sides of the first lamp body 1, in the present embodiment, barrier with optical path mirror
The optical path mirror for the first lamp body 1 for hindering the both ends of the seamed edge of object to be arranged on the outside, avoids the light of the second lamp body 2 from overflowing outward.
Communication device 3 is connect with control processor, and control processor is mutual by communication device 3 and ground control centre 5
Communication.
Control processor is connect with the first lamp body 1, the second lamp body 2, and control processor is defeated to 1/ second lamp body 2 of the first lamp body
Open signal/shutdown signal out, 1/ second lamp body 2 of the first lamp body execute unlatching/closing according to signal.
If having aircraft i.e. will be close to barrier overhead, ground control centre 5 is believed to first prompt of the output of communication device 3
Number, communication device 3 exports the first standby signal to control processor, and control processor is according to the first standby signal to the second lamp body
2 output open signals, the second lamp body 2 are opened and form the reflection of optical path by opposite optical path mirror.Ground control centre 5 is in aircraft
When will arrive in barrier overhead by plane, the first standby signal, the control of the barrier are exported to the communication device 3 of corresponding barrier
Processor exports open signal to the second lamp body 2 of the barrier, and the second lamp body 2 is opened.
If aircraft leaves barrier overhead, ground control centre 5 exports the second standby signal, communication to communication device 3
Device 3 exports the second standby signal to control processor, and control processor is closed according to standby signal to the second lamp body 2 output switch
Signal, the second lamp body 2 are closed.When aircraft flies away from barrier overhead, communication device 3 of the ground control centre 5 to the barrier
The second standby signal is exported, the control processor of the barrier closes the second lamp body 2.
As an embodiment of the present embodiment, the first standby signal and the second standby signal can be from aircrafts directly to barrier
The communication device 3 of object is hindered to export.
As a kind of preferred embodiment of the invention, the light that the second lamp body 2 projects is vertical with the mirror surface of optical path mirror.Second lamp
The light and optical path mirror mirror surface of body 2 are vertically formed optical path between the two.
As a kind of preferred embodiment of the invention, control processor is by 5 request of control centre to the ground of communication device 3
The plan schedule in locating course line, control processor feed back the plan schedule in locating course line to control processor.Control
Processor processed exports open signal to the second lamp body 2 at the time of aircraft passes through according to the plan schedule in the course line at place.Bottom surface
Control centre receives and can transfer the plan schedule of standard after request signal and fed back to communication device 3.As to the boat
The supplement of the plan schedule of line, ground control centre 5 also export the first standby signal to communication device 3 and believe with the second prompt
Number.
It further include weather monitoring device 6 as a kind of preferred embodiment of the invention, weather monitoring device 6 and control are handled
Device connection.Weather monitoring device 6 is used to monitor the weather condition near barrier, if meteorological optical range is lower than preset threshold,
Weather monitoring device 6 exports the first standby signal to control processor.Preset threshold may be configured as 0.5-5km, in the present embodiment
In may be configured as 2.5km, if meteorological optical range be lower than 2.5km, weather monitoring device 6 to control processor output first prompt
Signal control processor exports open signal to the second lamp body 2 according to the first standby signal, and the second lamp body 2 is opened and by opposite direction
The reflection of optical path mirror formation optical path.
As a kind of preferred embodiment of the invention, if meteorological optical range is lower than preset threshold, and current time is when default
Between in threshold value, then control processor exports often after receiving the first standby signal of the output of weather monitoring device 6 to the second lamp body 2
Bright signal, the second lamp body 2 are opened and are always on.Preset threshold may be configured as 0.5-5km, may be configured as 2.5km in the present embodiment,
Preset time threshold may be configured as 18:00-6:00.That is, being controlled if meteorological optical range is lower than preset threshold and the time is in night
Processor receive weather monitoring device 6 output the first standby signal after to the second lamp body 2 output be always on signal, the second lamp body
2 open and are always on, and improve the prompt effect of aviation obstruction beacon.
As a kind of preferred embodiment of the invention, the first lamp body 1 is provided with spare lamp body 7, if the second lamp body 2 is opened,
Spare lamp body 7 is opened.Spare lamp body 7 is used to improve the brightness of the first lamp body 1, and when the second lamp body 2 is closed, spare lamp body 7 is closed
It closes.
As a kind of preferred embodiment of the invention, between two adjacent the first lamp bodies 1, several independent second lamps are set
Body 2 and optical path mirror corresponding with the second lamp body 2.Second lamp body 2 can be independently arranged with optical path mirror, when the seamed edge of barrier is longer
It can effectively show.
As a kind of preferred embodiment of the invention, the light of the second lamp body is pencil.The light of gathering of pencil avoids light
Scattering.
The above embodiments merely illustrate the technical concept and features of the present invention, and the purpose is to allow the skill for being familiar with the technical field
Art personnel can understand the content of the present invention and implement it accordingly, and can not be limited the scope of the invention with this.All bases
Equivalent changes or modifications made by spirit of the invention, should be covered by the protection scope of the present invention.
Claims (9)
1. a kind of aviation obstruction light system based on optical path prompt, comprising: several are installed on the first lamp body on barrier,
It is characterized in that, further includes: the second lamp body, optical path mirror, communication device, control processor；
First lamp body is installed on the edge of barrier, barrier same seamed edge at least there are two the first lamp body；
Second lamp body is set to the first lamp body side, and optical path mirror is set to the other side of the first lamp body, optical path mirror and the second lamp body
On same straight line；
Communication device is connect with control processor, and control processor is in communication with each other by communication device and ground control centre；
Control processor is connect with the first lamp body, the second lamp body, and control processor opens letter to the first lamp body/the second lamp body output
Number/shutdown signal, the first lamp body/second lamp body is according to signal execution unlatching/closing；
If having aircraft i.e. will be close to barrier overhead, ground control centre exports the first standby signal, communication to communication device
Device exports the first standby signal to control processor, and control processor is exported to the second lamp body according to the first standby signal and opened
Signal, the second lamp body are opened and form the reflection of optical path by opposite optical path mirror；
If aircraft leaves barrier overhead, ground control centre exports the second standby signal to communication device, communication device to
Control processor exports the second standby signal, and control processor opens shutdown signal to the output of the second lamp body according to standby signal, the
Two lamp bodies are closed.
2. a kind of aviation obstruction light system based on optical path prompt according to claim 1, which is characterized in that the second lamp body
The light of injection is vertical with the mirror surface of optical path mirror.
3. a kind of aviation obstruction light system based on optical path prompt according to claim 1, which is characterized in that control processing
The plan schedule in device course line as locating for communication device control centre's request to the ground, control processor is by locating boat
The plan schedule of line is fed back to control processor.
4. a kind of aviation obstruction light system based on optical path prompt according to claim 3, which is characterized in that control processing
Device exports open signal to the second lamp body at the time of aircraft passes through according to the plan schedule in the course line at place.
5. a kind of aviation obstruction light system based on optical path prompt according to claim 1, which is characterized in that further include gas
As monitoring device, weather monitoring device is connect with control processor；Weather monitoring device is used to monitor the meteorology near barrier
Situation, if meteorological optical range is lower than preset threshold, weather monitoring device exports the first standby signal to control processor.
6. a kind of aviation obstruction light system based on optical path prompt according to claim 5, which is characterized in that if meteorological energy
Degree of opinion is lower than preset threshold, and current time in preset time threshold, then it is defeated to receive weather monitoring device for control processor
It is always on signal to the output of the second lamp body after the first standby signal out, the second lamp body is opened and is always on.
7. a kind of aviation obstruction light system based on optical path prompt according to claim 1, which is characterized in that the first lamp body
It is provided with spare lamp body, if the second lamp body is opened, spare lamp body is opened.
8. a kind of aviation obstruction light system based on optical path prompt according to claim 1, which is characterized in that adjacent
Between two the first lamp bodies, several independent second lamp bodies and optical path mirror corresponding with the second lamp body are set.
9. a kind of aviation obstruction light system based on optical path prompt according to claim 1, which is characterized in that the second lamp body
Light be pencil.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810605412.6A CN108966454B (en) | 2018-06-13 | 2018-06-13 | Aviation obstruction light system based on light path suggestion |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810605412.6A CN108966454B (en) | 2018-06-13 | 2018-06-13 | Aviation obstruction light system based on light path suggestion |
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| Publication Number | Publication Date |
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| CN108966454A true CN108966454A (en) | 2018-12-07 |
| CN108966454B CN108966454B (en) | 2019-12-06 |
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| CN201810605412.6A Expired - Fee Related CN108966454B (en) | 2018-06-13 | 2018-06-13 | Aviation obstruction light system based on light path suggestion |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110568858A (en) * | 2019-08-16 | 2019-12-13 | 天津大学 | method for adjusting safety distance of unmanned aerial vehicle based on LED aviation obstruction light |
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| US8591073B2 (en) * | 2005-03-03 | 2013-11-26 | Dialight Corporation | Beacon light with reflector and light emitting diodes |
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| US20110305014A1 (en) * | 2010-06-15 | 2011-12-15 | John Patrick Peck | Highly collimating reflector lens optic and light emitting diodes |
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| CN110568858B (en) * | 2019-08-16 | 2022-07-08 | 天津大学 | Method for adjusting safety distance of unmanned aerial vehicle based on LED aviation obstruction light |
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| CN108966454B (en) | 2019-12-06 |
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Effective date of registration: 20221223 Address after: 276000 No. 95, Huaxia Road, economic and Technological Development Zone, Linyi City, Shandong Province Patentee after: SHANDONG TIANCHENG STEEL STRUCTURE Co.,Ltd. Address before: Room 712, 7th floor, community entrepreneurship Park, Langya Economic Development Zone, Langya District, Chuzhou City, Anhui Province Patentee before: Chuzhou Shanshu Trading Co.,Ltd. |
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