公开(公告)号：KR101348956B1

公开(公告)日：2014-01-10

申请号：KR1020120085526

申请日：2012-08-06

Applicant: 한국항공우주연구원

Inventor： 정일형 ,  문경록 ,  라승호

IPC: G08C19/00

Abstract: A soundness monitoring system for an analog sensor in a measurement waiting state disclosed in the present invention includes: a data input unit (110) which is connected to an analog sensor (10) through a communication network (20) and receives a measurement waiting state sensing value (A) sensed at predetermined time intervals; a database (130) which stores a normal operation range (B) for the measurement waiting state sensing value and stores the current measurement waiting state sensing value obtained from the data input unit; a comparison control unit (120) which determines whether the current measurement waiting state sensing value obtained from the data input unit is within the normal operation range and outputs a control signal to selectively display the abnormal operation status (C) depending on the determination result; and a display unit (140) which displays the abnormal operation status to the outside according to the control signal. [Reference numerals] (10,AA,BB) Analog sensor; (110) Data input unit; (120) Comparison control unit; (130) Database; (140) Display unit; (141) Alarm display unit; (142) Display; (CC) Communication network

Abstract translation: 本发明公开的测量等待状态下的模拟传感器的健全性监视系统包括：通过通信网络（20）连接到模拟传感器（10）并接收测量等待状态的数据输入单元（110） 以预定时间间隔感测的感测值（A）; 数据库（130），其存储用于测量等待状态检测值的正常操作范围（B），并存储从数据输入单元获得的当前测量等待状态感测值; 比较控制单元，确定从数据输入单元获得的当前测量等待状态检测值是否在正常操作范围内，并输出控制信号，以根据确定结果选择性地显示异常运行状态（C）; 以及根据控制信号向外部显示异常操作状态的显示单元（140）。 （附图标记）（10，AA，BB）模拟传感器; （110）数据输入单元; （120）比较控制单元; （130）数据库; （140）显示单元; （141）报警显示单元; （142）显示; （CC）通信网络

公开(公告)号：KR1020110130085A

公开(公告)日：2011-12-05

申请号：KR1020100049546

申请日：2010-05-27

Applicant: 한국항공우주연구원

Inventor： 정일형 ,  이종웅 ,  문경록 ,  강선일 ,  안재철 ,  라승호

IPC: B64G5/00 ,  F42B35/00 ,  F41F3/052 ,  G01M99/00

CPC classification number: B64G5/00 ,  F02K9/96

Abstract: PURPOSE: A sensor fixing device for measuring the flame characteristic of a rocket is provided to facilitate the installation and maintenance by collectively installing a plurality of sensors and guarantee the convenience by applying various standard sensor. CONSTITUTION: A sensor fixing device for measuring the flame characteristic of a rocket comprises a plate-shaped sensor fixing unit(100) and one or more sensor fixing hole(110). The plate-shaped sensor fixing unit is fixed to the fixed position of launcher equipment. One or more sensor fixing hole is formed in the plate-shaped sensor fixing unit. The sensor fixing hole comprises one or more among a pressure sensor fixing hole, a gas temperature sensor fixing hole, a surface temperature fixing hole, an impact wave sensor fixing hole and a sound pressure sensor fixing hole.

Abstract translation: 目的：提供一种用于测量火箭火焰特性的传感器固定装置，通过集体安装多个传感器便于安装和维护，并通过应用各种标准传感器确保方便。 构成：用于测量火箭的火焰特性的传感器固定装置包括板状传感器固定单元（100）和一个或多个传感器固定孔（110）。 板状传感器固定单元固定在发射装置的固定位置。 一个或多个传感器固定孔形成在板状传感器固定单元中。 传感器固定孔包括压力传感器固定孔，气体温度传感器固定孔，表面温度固定孔，冲击波传感器固定孔和声压传感器固定孔中的一个或多个。