Solar powered Tower Warning Light, 10cd, 32.5cd, steady-flashing, Red Aircraft Warning light
Compliance of Solar Aircraft Warning Light
ICAO Annex 14 Volume 1, Seventh edition, 2016, table 6.3 Low Intensity Type A / B / E Obstruction Light
FAA L-810
Features of Solar Aircraft Warning Light
Electrical
LED as light source, life experience >100,000hours
Physical
With bird needle to prevent bird drop
UV & vibrations protected polycarbonate lens for converging light
Powder coated die casting aluminum base, light fastness, resist snow and rain, salt atmosphere
Built-in mono crystalline silicon solar panel, conversion efficiency is better than poly crystalline silicon
System design
Built-in photocell (Photo diode) for day & night working mode (dusk to dawn mode)
ON/OFF button make local control easy
Optional
Infrared LED for pilot using NVG(Night Vision Goggles)
GPS sync flashing
Application of Solar Aircraft Warning Light
AH-LS-L Solar Aircraft Warning Light is specialized used on the top of the High Chimney, Telecommunication tower, Wind Turbine where there is no cable power supply and those facilities which have high requirements on lightning protection.
l Used alone on the top of obstacle which height is less than 45meter
SPECIFICATIONS | AH-LS-L LED Low-intensity L810 Solar Aircraft Warning Light |
Light Characteristics | |
Light Source | LED |
Emitting Color | Red |
Intensity(cd) |
>10cd(>32.5cd is optional) ) |
Horizontal Output(degrees) | 360 |
Vertical Divergence(degrees) | ≥10 |
Flash Characteristics | 20fpm(steady/other flashing rate is customized) |
Operation Mode | Dusk-to-Dawn operation |
LED Life Experience(hours) | >100,000 |
Electrical Characteristics | |
Operating Voltage | 3.7 |
Circuit Protection | Integrated |
Solar Characteristics | |
Solar Module Type | Mono crystalline Silicon |
Charging Regulation | Microprocessor controlled |
Battery Characteristics | |
Battery type | Lithium ion battery |
Nominal Voltage (V) | 3.7 |
Battery Service Life | Average 3 years |
Autonomy (hours) | Steady: ≥60, Flashing: ≥120 |
Physical Characteristics | |
Lamb Body Material | UV protected Polycarbonate |
Base Material | Powder-coated Die-casting aluminum |
Installation Size | 140×140×M6 |
Overall Size (mm) | 162×162×160 |
Weight(kg) | 1 |
Product Life Expectancy | Average 5 years |
Environmental Factors | |
Ambient Temperature(℃) -55℃~+70℃ |
-55~70 |
Humidity | 0~100% |
Wind Speed | 80m/s |
Waterproof | IP68 |
Compliance | |
ICAO | Annex 14 Volume 1,'Aerodrome Design and |
Operations’ Seventh edition July 2016, table 6.3 | |
Low-intensity Type A/B/E Obstacle Light | |
FAA | L-810 |
Optional | |
NVG - compatible infrared (IR) LED
|
|
GPS sync flashing |
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