摘要
针对某民用飞机飞控系统MOC4适航符合性验证,给出MOC4试验验证的基本方法,并对验证方案进行了设计。通过方向舵舵面卡阻试验,详细说明了MOC4试验验证方法的实施过程。由所采集的实验数据与试验判据相比较,得到MOC4试验验证方法可行、有效。该验证方法可为同类机型的MOC4适航符合性验证提供有效途径,具有工程实践意义。
For a civil aircraft flight control system MOC4 airworthiness compliance verification, given MOC4 test validation, and the validation protocol was designed. By rudder jam test, the details of MOC4 test process was illustrated. The experimental data collected and test criterion comparison showed that, the method had feasibility and effectiveness. The authentication method can be in line with similar models MOC4 airworthiness validation to provide an effective way of engineering practice signiifcance.
出处
《航空科学技术》
2014年第1期46-50,共5页
Aeronautical Science & Technology
作者简介
通讯作者张大伟（1982-）男，硕士学位，工程师，主要研究方向：飞控系统设计。Tel：021．33226651E-mail：zdw20030612@126．com
