CN201733492U - Omni-directional aviation obstruction light synchronous control system - Google Patents
Omni-directional aviation obstruction light synchronous control system Download PDFInfo
- Publication number
- CN201733492U CN201733492U CN2010202483422U CN201020248342U CN201733492U CN 201733492 U CN201733492 U CN 201733492U CN 2010202483422 U CN2010202483422 U CN 2010202483422U CN 201020248342 U CN201020248342 U CN 201020248342U CN 201733492 U CN201733492 U CN 201733492U
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- obstruction
- obstruction light
- processing unit
- central processing
- control system
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Abstract
The utility model discloses an obstruction light control system, in particular to a wind turbine omni-directional aviation obstruction light synchronous control system, the structure is that a central processing unit is arranged on a low pressure unit bottom plate, the central processing unit is connected with obstruction light terminal boxes, the obstruction light and the obstruction light terminal boxes are connected through shielded cables, various photographic sensors are connected with the central processing unit, and the central processing unit is connected with a GPS module. The wind turbine omni-directional aviation obstruction light synchronous control system can adjust the brightness of the obstruction light in daytime and at night, simultaneously guarantees all obstruction lights of a total obstruction system to synchronously operate, greatly increases the safety of an aviation obstruction system, can supply aviation risk alarm in maximum limit, and reduces the effect of ground environment.
Description
Technical field
The utility model relates to the obstruction light control system, particularly relates to the comprehensive aviation obstruction beacon synchronous control system of a kind of wind-driven generator.
Background technology
Along with fast development of social economy, energy problem is stranded is always scratching countries in the world, and tapping a new source of energy is an effective means.The therefore fast development at home of wind power generation industry, and along with the rising of single-machine capacity, the wind-driven generator machine volume increases gradually, thereby causes the height of tower tube constantly to raise.This just gives the civil aviaton field, and National Space Administration's aviation auxiliary facility brings corresponding problem.Aeronautical beacon is the critical facility of aircraft navigation, at present, domestic traditional aviation obstruction beacon control system is separate, though low price, circuit is simple, but useful life is shorter relatively, and the system maintenance cost is very high, and poor for the aviation Risk-warning of huge barricade system, for aircraft industry is brought very big potential safety hazard.
The utility model content
Technical problem to be solved in the utility model provides a kind of long service life, accurate fault-free, comprehensive aviation obstruction beacon synchronous control system.
In order to solve the problems of the technologies described above, the utility model is achieved by the following technical solution: comprehensive aviation obstruction beacon synchronous control system, structure is as follows: central processing unit is installed on the low voltage unit base plate, central processing unit is connected with each obstruction light terminal box by communication cable, obstruction light is connected by shielded type cable with the obstruction light terminal box, each photosensitive sensor is connected with central processing unit, and central processing unit is connected with the GPS module.
Described obstruction light is installed on the support of both sides, rear portion, top, cabin.
Described photosensitive sensor is installed in side, obstruction light support two ends.
Described GPS module is installed in the side of obstruction light support.
Described central processing unit is connected with Surge Protector.
Advantage of the present utility model and effect are as follows: the utility model adopts the two light intensity aviation obstruction beacon mark high-altitude obstacles of merely hitting, and obstruction light can be used for as signal lamp, and can with other obstruction light synchronous operation of whole barricade system.The utility model can provide the alarm of aviation risk to greatest extent, reduces the influence of ground environment.Can regulate daytime or night obstruction light brightness, change the color of control system obstruction light according to the ambient light state of strength.More reliable and stable, the efficient height, good uniformity, long service life is easy to installation and maintenance, and windproof and rain proof is fit to be installed in the rugged environment.Greatly improved the fail safe of air line.
Description of drawings
Fig. 1 is that the comprehensive aviation obstruction beacon synchronous control system of the utility model structure connects sketch.
Among the figure: 1, obstruction light, 2, photosensitive sensor, 3, the GPS module, 4, shielded type cable, 5, the obstruction light terminal box, 6, the obstruction light support, 7, communication cable, 8, central processing unit, 9, low voltage unit.
Embodiment
Below in conjunction with accompanying drawing the utility model is described in further details, but protection range of the present utility model is not limit by embodiment.
As shown in Figure 1; comprehensive aviation obstruction beacon synchronous control system; structure is as follows: the utility model is an example to control the two light intensity A type obstruction lights 1 of merely hitting; central processing unit 8 is installed on low voltage unit 9 base plates; central processing unit 8 is connected with obstruction light terminal box 5 by communication cable 7; two obstruction lights 1 are connected by shielded type cable 4 with obstruction light terminal box 5; each photosensitive sensor 2 is connected with central processing unit 8; central processing unit 8 is connected with GPS module 3; obstruction light 1 is installed on the support of both sides, rear portion, top, cabin; photosensitive sensor 2 is installed in side, obstruction light support 6 two ends; GPS module 3 is installed in the side of obstruction light support 6; central processing unit 8 is connected with Surge Protector, provides power supply by low voltage unit 9 for central processing unit.Obstruction light 1 is outer to be provided with lampshade, and lampshade is that macromolecular material has firm and anti-high-strength impact characteristic, in light weightly is easy to installation and maintenance, and windproof and rain proof is fit to be installed in the rugged environment, satisfies the relevant laws and regulations requirement of aviation obstacle marking.Central processing unit relies on photosensitive sensor to experience the Strength Changes of ambient light, carry out daytime or night mode of operation conversion.Whether normally the output signal of two photosensitive sensors of central processing unit comparison determines their operations, discerns and ignore the indication of photosensitive sensor mistake.If two photosensitive sensors all damage, central processing unit can write down this mistake, and obstruction light can continue to operate in day mode.GPS module 3 is installed in the next door of obstruction light support, provides the global synchronization real-time clock signal to central processing unit, controls the synchronous blinking characteristic of whole barricade system obstruction light.
Claims (5)
1. comprehensive aviation obstruction beacon synchronous control system, it is characterized in that structure is as follows: central processing unit is installed on the low voltage unit base plate, central processing unit is connected with each obstruction light terminal box by communication cable, obstruction light is connected by shielded type cable with the obstruction light terminal box, each photosensitive sensor is connected with central processing unit, and central processing unit is connected with the GPS module.
2. comprehensive aviation obstruction beacon synchronous control system according to claim 1 is characterized in that described obstruction light is installed on the support of both sides, rear portion, top, cabin.
3. comprehensive aviation obstruction beacon synchronous control system according to claim 1 is characterized in that described photosensitive sensor is installed in side, obstruction light support two ends.
4. comprehensive aviation obstruction beacon synchronous control system according to claim 1 is characterized in that described GPS module is installed in the side of obstruction light support.
5. comprehensive aviation obstruction beacon synchronous control system according to claim 1 is characterized in that described central processing unit is connected with Surge Protector.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010202483422U CN201733492U (en) | 2010-07-06 | 2010-07-06 | Omni-directional aviation obstruction light synchronous control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010202483422U CN201733492U (en) | 2010-07-06 | 2010-07-06 | Omni-directional aviation obstruction light synchronous control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201733492U true CN201733492U (en) | 2011-02-02 |
Family
ID=43524646
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010202483422U Expired - Fee Related CN201733492U (en) | 2010-07-06 | 2010-07-06 | Omni-directional aviation obstruction light synchronous control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201733492U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109268736A (en) * | 2018-09-14 | 2019-01-25 | 广东玖洲机场建设有限公司 | A kind of induction height aviation obstruction beacon |
| CN112235916A (en) * | 2020-09-25 | 2021-01-15 | 深圳星标科技股份有限公司 | Light intensity control method of visual navigation aid equipment and related device |
-
2010
- 2010-07-06 CN CN2010202483422U patent/CN201733492U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109268736A (en) * | 2018-09-14 | 2019-01-25 | 广东玖洲机场建设有限公司 | A kind of induction height aviation obstruction beacon |
| CN112235916A (en) * | 2020-09-25 | 2021-01-15 | 深圳星标科技股份有限公司 | Light intensity control method of visual navigation aid equipment and related device |
| CN112235916B (en) * | 2020-09-25 | 2023-03-31 | 深圳星标科技股份有限公司 | Light intensity control method of visual navigation aid equipment and related device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20110202 Termination date: 20150706 |
|
| EXPY | Termination of patent right or utility model |