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    • 26. 发明授权
    • 이착륙장을 조명하기 위한 조명 유닛
    • 用于照明着陆区域的照明单元
    • KR101771441B1
    • 2017-08-25
    • KR1020127011287
    • 2010-09-30
    • 아데베 베파우베아
    • 베우케마,마르티즌문스,루도
    • B64F1/20F21V31/00F21V15/01F21V31/03B64C27/82F21W111/06F21Y101/02F21Y113/00
    • F21V31/00B64D2203/00B64F1/20F21V15/01F21V31/03F21W2111/06F21Y2115/10
    • 본발명은특히항공기로신호를전달하기위해공항에서이착륙장을조명하기위한조명장치에관한것이다. 조명장치는방출되는광을발생하기위한하나이상의발광다이오드(4)를가지는광원, 광원을공급하고작동하기위한전기부품(5), 광원에의해발생된광에영향을미치기위한광학부품(7) 및광 배출개구(14)를가지는전기및 광학부품을포함하며, 광배출개구(14)를통하여광학부품에의해영향을받는광이배출된다. 본발명에따라, 광원은기밀방식으로폐쇄된카세트모듈(1) 내의전기및 광학부품(5, 7)과함께배치된다. 상기모듈은외측하우징에통합되며, 외측하우징은또한기밀방식으로폐쇄되어, 카세트모듈내에배치된부품은이중밀봉보호부를가진다.
    • 技术领域本发明涉及用于照明机场着陆区域的照明设备,特别是用于向飞机传送信号。 影响由电气部件5产生用于照明装置的光学部件,用于提供光源的光源,具有该光源的至少一个发光二极管(4)和工作用于产生光发射的光(7)的 并且具有光出射孔(14)的电和光学部件,被光学部件影响的光通过该出光孔射出。 根据本发明,光源布置成盒式模块1中的电气和光学组件5,7以气密方式关闭。 该模块被集成到外壳体,外壳体也被关闭以气密的方式,布置在盒模块中的部件具有双重部密封保护。
    • 29. 发明公开
    • 항공장애등 점검 장치 및 방법, 및 이를 이용한 항공장애등 점검 시스템
    • 检查用于飞行的障碍物的装置和方法,以及使用该系统的系统
    • KR1020140042421A
    • 2014-04-07
    • KR1020120109165
    • 2012-09-28
    • 한전케이디엔주식회사
    • 강대권서덕기유성재
    • G01R19/165H05B37/03
    • G01R19/165F21W2111/06H05B37/03
    • Disclosed are an apparatus and a method for inspecting an aviation obstruction light and a system for inspecting the aviation obstruction light using the same. The apparatus for inspecting the aviation obstruction light according to an embodiment of the present invention comprises: a power supply unit which supplies power to the aviation obstruction light; a shunt resistor which is inserted into a wire connecting the power supply unit to the aviation obstruction light; a shunt sensor which measures voltage and the number of flashes across both ends of the shunt resistor; and a failure detection unit which compares the measured data of the voltage and the number of flashes across both ends of the shunt resistor with a set reference value to determine whether the aviation obstruction light has any problem.
    • 公开了一种用于检查航空障碍物的装置和方法以及使用其的航空障碍物的检查系统。 根据本发明的实施例的用于检查航空障碍物的装置包括:向航空障碍灯供电的电源单元; 插入到将电源单元连接到航空障碍灯的线路中的分流电阻器; 分流传感器,其测量分流电阻器两端的电压和闪光数; 以及故障检测单元,其将分流电阻器的两端的电压和闪烁次数的测量数据与设定的参考值进行比较,以确定航空障碍物是否具有任何问题。
    • 30. 发明公开
    • 전 방향 투사 매립형 태양광 도로 표지병
    • OMNIDIRECTIONAL PROJECTION RECLAMATION TYPE SOLAR ROAD STUD
    • KR1020130024126A
    • 2013-03-08
    • KR1020110087375
    • 2011-08-30
    • 주식회사 지앤아이테크
    • 서창범
    • E01F9/06F21S9/03
    • F21V15/00E01F9/559F21S8/022F21S9/037F21V31/00F21W2111/02F21W2111/06F21Y2115/10Y02B20/72
    • PURPOSE: An embedded solar road marker for omnidirectional projection is provided to prevent shock or movement due to the weight of a vehicle or the frictional force with wheels and to suppress damage or breakdown due to the thermal expansion from temperature changes. CONSTITUTION: An embedded solar road marker for omnidirectional projection comprises a base(100), a marker body(200), and a fixing plate(300). The base is embedded in a road surface. The marker body includes a lower case, an upper case, a solar cell(211), an accumulator board(212), and an LED module(215). The lower case and the upper case are combined to form the marker body in the sealed state. The solar cell installed within the lower case receives solar light for converting solar energy into electric energy. The accumulator board stores the electric energy. The fixing plate is fixed to the base and presses down the marker body.
    • 目的:提供用于全向投影的嵌入式太阳能道路标志,以防止由于车辆重量或车轮摩擦力引起的冲击或运动,并抑制由温度变化引起的热膨胀引起的损坏或破坏。 构成:用于全向投影的嵌入式太阳能道路标志包括基座(100),标记体(200)和固定板(300)。 基座嵌入路面。 标记体包括下壳体,上壳体,太阳能电池(211),蓄电池板(212)和LED模块(215)。 组合下壳体和上壳体以形成处于密封状态的标记体。 安装在下壳体内的太阳能电池接收用于将太阳能转换为电能的太阳光。 蓄电池存储电能。 固定板固定在基座上并按压标记体。