民用飞机尾翼操纵面的特殊设计研究  

Special Design Research of EmpennageControl Surface in Civil Aircraft

作　　者：金晖[1] 

机构地区：[1]上海飞机设计研究院,上海201210

出　　处：《民用飞机设计与研究》2012年第B11期69-72,共4页Civil Aircraft Design & Research

摘　　要：尾翼操纵面是飞机结构中的重要组成部分,是飞机操纵性和稳定性的重要保证。国内民机研制中针对惯性载荷作用下的设计参考较少。本文从尾翼结构的强度分析角度出发,针对尾翼操纵面惯性载荷下的受力特点,分析研究了两种不同设计方法各自的特点,同时对一些新问题提出了展望和期待。Empennage control surface is an important part of aircraft structure and is also an important guarantee on aircraft operability and stability. There is little design references for inertial loads in civil aircraft research. The article, which from the strength analysis of empennage structure, aims at the characteristic under inertial load of empennage control surfaces, analyzes the characteristic of two different research methods. Meanwhile, it brings forward expectation and hope on some new problems.

关 键 词：尾翼 操纵面 载荷 受力分析 惯性载荷 

分 类 号：V224[航空宇航科学与技术—飞行器设计]