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公开(公告)号:KR100374146B1
公开(公告)日:2003-03-03
申请号:KR1020000074569
申请日:2000-12-08
Applicant: 한국항공우주연구원
IPC: G01N31/00
Abstract: PURPOSE: An ozone-measuring sensor capable of measuring the amount of ozone using optical absorption characteristics of gas as ozone by being mounted on an ultra-high speed flying body containing a scientific rocket is provided. It is short in a measuring time and simple as compared to conventional sensors, thereby being applied to a balloon which flies at low speed, or other transporting devices as well as a rocket. CONSTITUTION: The sensor mounted on the outer skin of a frying body measures the amount of ozone by extremely short measurement, wherein it comprises: an interference type filter(10) for filtering a specified wavelength from light; an optical sensor part(20) for detecting the quantity of light having a specified wavelength filtered therein; a front amplification part(30) for amplifying the light intensity detected therein; an automatic gain control circuit part(40) for gain controlling the light intensity; and a power source control part(50) for supplying a drive power source.
Abstract translation: 目的:提供一种臭氧测量传感器,其能够通过安装在包含科学火箭的超高速飞行体上,利用气体的光学吸收特性作为臭氧来测量臭氧量。 与传统的传感器相比,其测量时间短且简单,因此应用于低速飞行的气球或其他运输装置以及火箭。 本发明的特征在于:安装在煎炸器外壳上的传感器通过极短的测量来测量臭氧的量,其中包括:用于从光中过滤特定波长的干涉型过滤器(10) 一个光学传感器部件(20),用于检测在其中过滤的具有特定波长的光量; 前置放大部分(30),用于放大其中检测到的光强度; 自动增益控制电路部分(40),用于增益控制光强度; 和用于供给驱动动力源的动力源控制部(50)。
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公开(公告)号:KR1020020045199A
公开(公告)日:2002-06-19
申请号:KR1020000074569
申请日:2000-12-08
Applicant: 한국항공우주연구원
IPC: G01N31/00
Abstract: PURPOSE: An ozone-measuring sensor capable of measuring the amount of ozone using optical absorption characteristics of gas as ozone by being mounted on an ultra-high speed flying body containing a scientific rocket is provided. It is short in a measuring time and simple as compared to conventional sensors, thereby being applied to a balloon which flies at low speed, or other transporting devices as well as a rocket. CONSTITUTION: The sensor mounted on the outer skin of a frying body measures the amount of ozone by extremely short measurement, wherein it comprises: an interference type filter(10) for filtering a specified wavelength from light; an optical sensor part(20) for detecting the quantity of light having a specified wavelength filtered therein; a front amplification part(30) for amplifying the light intensity detected therein; an automatic gain control circuit part(40) for gain controlling the light intensity; and a power source control part(50) for supplying a drive power source.
Abstract translation: 目的:提供一种臭氧测量传感器,其能够通过安装在包含科学火箭的超高速飞行体上,测量作为臭氧的气体的光吸收特性的臭氧量。 与常规传感器相比,测量时间短,简单,因此适用于以低速飞行的气球,或其他运输装置以及火箭。 构成:安装在油炸机外皮上的传感器通过非常短的测量来测量臭氧量,其中包括:用于从光中过滤指定波长的干涉型过滤器(10); 光传感器部件(20),用于检测在其中滤波的具有指定波长的光量; 用于放大其中检测到的光强度的前置放大部分(30); 用于增益控制光强度的自动增益控制电路部分(40); 以及用于提供驱动电源的电源控制部(50)。
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