摘要
介绍了飞机水平安定面作动器功能及受载情况,利用有限元方法对作动器结构进行了强度分析。分析结果表明,飞机水平安定面作动器满足静强度要求,研究内容具有实际的工程意义。
This paper introduces the function and loading of aircraft horizontal stabilizer trim actuator,and conducts strength analysis of actuator structure by using finite element method.The analysis results show that the aircraft horizontal stabilizer trim actuator meets the static strength requirements,and the research has a practical engineering significance.
作者
孙滨
Sun Bin(Shenyang Aircraft Airworthiness Certification Center of CAAC,Shenyang Liaoning 110043,China)
出处
《工程与试验》
2019年第3期36-37,共2页
Engineering and Test
