CN203554765U - Novel aviation obstruction light - Google Patents
Novel aviation obstruction light Download PDFInfo
- Publication number
- CN203554765U CN203554765U CN201320715647.3U CN201320715647U CN203554765U CN 203554765 U CN203554765 U CN 203554765U CN 201320715647 U CN201320715647 U CN 201320715647U CN 203554765 U CN203554765 U CN 203554765U
- Authority
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- China
- Prior art keywords
- module
- aviation obstruction
- electrically connected
- obstruction beacon
- control module
- 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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- 238000004891 communication Methods 0.000 claims abstract description 9
- 238000012544 monitoring process Methods 0.000 claims abstract description 8
- 230000003321 amplification Effects 0.000 claims abstract description 6
- 238000003199 nucleic acid amplification method Methods 0.000 claims abstract description 6
- 238000005286 illumination Methods 0.000 abstract 1
- 238000012423 maintenance Methods 0.000 description 5
- 230000002159 abnormal effect Effects 0.000 description 3
- 239000004744 fabric Substances 0.000 description 3
- 230000001360 synchronised effect Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B20/00—Energy efficient lighting technologies, e.g. halogen lamps or gas discharge lamps
- Y02B20/40—Control techniques providing energy savings, e.g. smart controller or presence detection
Abstract
The utility model provides a novel aviation obstruction light. The novel aviation obstruction light comprises a programmable module, a GPS receiving module electrically connected with the programmable module, a light control module electrically connected with the programmable module, a wireless communication module electrically connected with the programmable module, and a light fixture electrically connected with the light control module. The programmable module comprises a single-chip microcomputer and an EEPROM unit. The light control module comprises a signal amplification unit, a photosensitive unit and a light state monitoring unit. The novel aviation obstruction light realizes synchronization states among multiple aviation obstruction lights without wiring connection, and can automatically turn on or turn off the aviation obstruction lights according to illumination environment, and can also remotely monitor the positions of the aviation obstruction lights and the real-time working states of the aviation obstruction lights through a short message mode.
Description
Technical field
The utility model relates to a kind of light fixture, particularly relates to a kind of novel aviation obstruction beacon.
Background technology
The control mode of traditional aviation obstruction beacon is by the mode of wiring, each aviation obstruction beacon to be connected on a master controller to realize the synchronous regime of each aviation obstruction beacon; this method needs cloth payout at the scene; on-the-spot cloth payout not only expends a large amount of manpower and materials but also needs follow-up a large amount of maintenance work of carrying out; in the more severe situation of environment, also need with pvc pipe, laid circuit to be protected at the scene the maintenance difficulties in can further increase input so again cost and later stage.In whole aviation obstruction beacon system, usually can cannot normally work because the fault of a lamp causes whole system, this greatly reduces the reliability of aviation obstruction beacon.Many times, aviation obstruction beacon must be placed on the area that the people such as high mountain area are difficult to maintenance by cloth simultaneously, and traditional aviation obstruction beacon cannot meet the instructions for use of such kind of area.Need now a kind of needs connecting up and can realize the aviation obstruction beacon that it can have synchronous regime between multiple aviation obstruction beacons badly, simultaneously remote monitoring aviation obstruction beacon state very easily again.
Utility model content
The utility model wants technical solution problem to be, a kind of novel aviation obstruction beacon is provided.
For solving above technical problem, the technical solution of the utility model is: a kind of novel aviation obstruction beacon, its key is: comprise programmable module, the GPS receiver module body being electrically connected with described programmable module and the lighting control module being electrically connected with described programmable module, also comprise the light fixture being electrically connected with described lighting control module.
As improvement one of the present utility model, described programmable module comprises single-chip microcomputer.
As the utility model, further improve, described programmable module also comprises EEPROM unit.
As improvement two of the present utility model, described lighting control module comprises signal amplification unit and photosensitive unit.
As the utility model, further improve, described lighting control module also comprises light Condition Monitoring Unit.
As the utility model, further improve, also comprise the wireless communication module being electrically connected with described programmable module, described wireless communication module is gsm module.
As the utility model, further improve, also comprise the power module to described programmable module, GPS receiver module, lighting control module and gsm module power supply.
By implement the utility model desirable following beneficial effect:
A kind of novel aviation obstruction beacon, comprises programmable module, the GPS receiver module body being electrically connected with described programmable module and the lighting control module being electrically connected with described programmable module, also comprises the light fixture being electrically connected with described lighting control module.GPS receiver module can utilize the split-second precision standard that gps satellite provides to carry out time service, and wherein time signal is taken out, programmable module be the time signal of taking out be frequency and the pulsewidth that benchmark programming output expection is wanted, the in the situation that of so just can connecting up between not needing many aviation obstruction beacons, realize its state synchronously.Described programmable module comprises single-chip microcomputer and EEPROM unit, wherein EEPROM unit is used for storing frequencies and pulse width information, first the frequency requiring and pulse width information are write in EEPROM unit, after receiving time signal, GPS receiver module delivers to single-chip microcomputer, the starting point of single-chip microcomputer take this time signal as flick of lamp, the frequency and the pulsewidth that according to the data output being pre-written in EEPROM unit, need again, because output signal starting point is identical, therefore the flash of light of each lamp is synchronous, dodging light frequency and pulsewidth is to realize according to the data in EEPROM unit.Described lighting control module comprises signal amplification unit, photosensitive unit and light Condition Monitoring Unit, signal amplification unit can amplify to promote light fixture work by the small-signal of output, photosensitive unit can detect photoenvironment around in real time, according to photoenvironment aviation obstruction beacon around, can automatically close or open, single-chip microcomputer timing judges the operating state of lamp by light Condition Monitoring Unit feedack, once detect that unusual condition appears in lamp, single-chip microcomputer can read positional information corresponding to GPS receiver module in the abnormal aviation obstruction beacon of current generation, so just can understand in real time each aviation obstruction beacon and whether extremely also can carry out in time maintenance process.Described novel aviation obstruction beacon also comprises the wireless communication module being electrically connected with described programmable module, described wireless communication module is gsm module, when certain lamp is abnormal, gsm module can send to corresponding main frame number by the positional information that abnormal lamp occurs in the mode of note, this main frame number is stored in advance in gsm module, make like this maintenance in later stage become more simple, this wireless monitor mode is specially adapted to safeguard monitoring to being operated in the aviation obstruction beacon in area that the people such as high mountain are difficult to safeguard.
Described novel aviation obstruction beacon also comprises the power module to described programmable module, GPS receiver module, lighting control module and gsm module power supply, power module can provide for whole lamp system the electric energy of continuous operation, has guaranteed that novel aviation obstruction beacon can work reliable and stablely.The utility model is skillfully constructed, and this function is very practical, is with a wide range of applications.
Accompanying drawing explanation
Below in conjunction with Figure of description, the utility model is described in more detail, wherein:
Fig. 1 is structural representation of the present utility model.
Embodiment
As shown in Figure 1, a kind of novel aviation obstruction beacon,, comprise programmable module, the GPS receiver module body that is electrically connected with described programmable module, the lighting control module being electrically connected with described programmable module, the light fixture being electrically connected with described lighting control module and the wireless communication module being electrically connected with described programmable module.Described programmable module comprises single-chip microcomputer and EEPROM unit, and described lighting control module comprises signal amplification unit, photosensitive unit and light Condition Monitoring Unit, and described wireless communication module is gsm module.Described novel aviation obstruction beacon also comprises the power module to described programmable module, GPS receiver module, lighting control module and gsm module power supply.
Must be pointed out, some indefinitenesses that above-mentioned embodiment is just made the utility model illustrate.But person of skill in the art will appreciate that, do not departing under aim of the present utility model and scope, can the utility model be made modification, replaces and be changed, these be revised, replace and change and still belong to protection range of the present utility model.
Claims (9)
1. a novel aviation obstruction beacon, it is characterized in that: comprise programmable module, the GPS receiver module body being electrically connected with described programmable module and the lighting control module being electrically connected with described programmable module, also comprise the light fixture being electrically connected with described lighting control module.
2. the novel aviation obstruction beacon of one according to claim 1, is characterized in that: described programmable module comprises single-chip microcomputer.
3. the novel aviation obstruction beacon of one according to claim 2, is characterized in that: described programmable module also comprises EEPROM unit.
4. according to the novel aviation obstruction beacon of one described in any one in claims 1 to 3, it is characterized in that: described lighting control module comprises signal amplification unit.
5. the novel aviation obstruction beacon of one according to claim 4, is characterized in that: described lighting control module also comprises photosensitive unit.
6. the novel aviation obstruction beacon of one according to claim 5, is characterized in that: described lighting control module also comprises light Condition Monitoring Unit.
7. the novel aviation obstruction beacon of one according to claim 6, is characterized in that: also comprise the wireless communication module being electrically connected with described programmable module.
8. the novel aviation obstruction beacon of one according to claim 7, is characterized in that: described wireless communication module is gsm module.
9. the novel aviation obstruction beacon of one according to claim 8, is characterized in that: also comprise the power module to described programmable module, GPS receiver module, lighting control module and gsm module power supply.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320715647.3U CN203554765U (en) | 2013-11-14 | 2013-11-14 | Novel aviation obstruction light |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320715647.3U CN203554765U (en) | 2013-11-14 | 2013-11-14 | Novel aviation obstruction light |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203554765U true CN203554765U (en) | 2014-04-16 |
Family
ID=50472822
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320715647.3U Expired - Lifetime CN203554765U (en) | 2013-11-14 | 2013-11-14 | Novel aviation obstruction light |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203554765U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109413821A (en) * | 2018-10-26 | 2019-03-01 | 北京首航艾启威节能技术股份有限公司 | Novel aviation obstruction light controller and control method |
-
2013
- 2013-11-14 CN CN201320715647.3U patent/CN203554765U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109413821A (en) * | 2018-10-26 | 2019-03-01 | 北京首航艾启威节能技术股份有限公司 | Novel aviation obstruction light controller and control method |
| CN109413821B (en) * | 2018-10-26 | 2024-02-23 | 首航高科能源技术股份有限公司 | Aviation obstruction light controller and control method |
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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 |
Granted publication date: 20140416 |
|
| CX01 | Expiry of patent term |