运输机机动载荷减缓的机翼质量分析研究

探索与飞机设计技术发展相适应的分析方法是质量设计人员面临的重要课题,是提升能力、创新手段的必然要求。本文以主动控制机动载荷减缓机翼为对象,应用气动、载荷、结构、强度、材料等多学科分析方法,对采用这一功能后机翼弯曲、剪切材料质量进行了系统的分析研究,并进行了应用验证。

Wing Structural Weight Analysis of Transport Aircraft with Maneuvering Load Alleviation Function

In order to promote innovation ability,an important task of designer is to grope for analysis methods which are applicable to modern advanced aircraft design technology.This paper aims at the subject of Maneuvering Load Alleviation Wing,utilizes multidisciplinary analysis methods,such as aerodynamics,loading,structure,strength,material etc,the wing bending and shear material weight are analysed systematically.The method has been validated by existing aircraft.