公开(公告)号：KR1020120074472A

公开(公告)日：2012-07-06

申请号：KR1020100136316

申请日：2010-12-28

Applicant: 한국항공우주연구원

Inventor： 문상만 ,  김경표 ,  송재훈 ,  최선우 ,  이장연

IPC: G01N3/08 ,  G01M5/00 ,  G01M99/00 ,  G05B9/02

CPC classification number: G01N3/08 ,  G01M5/00 ,  G01M99/007 ,  G01N2203/0204 ,  G05B9/02

Abstract: PURPOSE: A system for controlling a stop of an aircraft structure test and a method for controlling the stop of the aircraft structure test using the same are provided to predict accumulated properties based on signals of a sensor and a fractural moment of an testing object based on a preset value while testing an aircraft structure, thereby enhancing the stability of an aircraft structure testing body and the testing object. CONSTITUTION: A system for controlling a stop of an aircraft structure test comprises a testing object(101), a testing sensor unit(103), a sensor data acquisition unit(104), a monitoring and analyzing unit(105), and a commanding unit(106). The testing object is installed in an aircraft structure testing body. The testing sensor unit is mounted on the testing object and the aircraft structure testing body. The sensor data acquisition unit receives signals from the testing sensor unit, thereby obtaining data. The monitoring and analyzing unit monitors and analyzes the obtained data. The commanding unit commands a stop of an aircraft structure test by receiving signals from the monitoring and analyzing unit.

Abstract translation: 目的：提供一种用于控制飞机结构测试停止的系统和一种用于控制飞行器结构测试停止的方法，用于基于传感器的信号和基于测试对象的断裂力矩来预测累积特性 同时测试飞行器结构的预设值，从而提高飞行器结构测试体和测试对象的稳定性。 构成：用于控制飞机结构测试停止的系统包括测试对象（101），测试传感器单元（103），传感器数据获取单元（104），监视和分析单元（105）以及命令 单元（106）。 测试对象安装在飞机结构测试机构中。 测试传感器单元安装在测试对象和飞机结构测试体上。 传感器数据采集单元从测试传感器单元接收信号，从而获得数据。 监测和分析单元监测和分析获得的数据。 指挥单位通过接收来自监测分析单元的信号来指挥飞机结构试验的停止。