首页 | 本学科首页   官方微博 | 高级检索  
     检索      

民用飞机阵风载荷及减缓技术的研究
引用本文:赵继伟、胡赞远.民用飞机阵风载荷及减缓技术的研究[J].民用飞机设计与研究,2012(1):17-20.
作者姓名:赵继伟、胡赞远
作者单位:上海飞机设计研究院,上海,200232
摘    要:由于民用飞机机翼具有大展弦比的特点,因此阵风载荷经常成为民用飞机飞行载荷的严重情况,是各国适航标准重点考察的飞行情况。而且,阵风干扰还会因飞机机体的自身弹性引起结构弹性振动,使飞机结构刚度降低,造成机体疲劳损伤,甚至引起颤振。因此,在民用飞机载荷设计过程中对阵风载荷及其减缓技术进行研究具有非常重要的意义。介绍了民用飞机阵风载荷的原理及相关技术,以及阵风载荷减缓技术中用直接升力控制方法来实现机翼的阵风载荷减缓。

关 键 词:民用飞机  阵风载荷  减缓技术  直接升力控制

Research on Gust Load and its Load Alleviation Technology of Civil Aircrafts
Zhao Jiwei Hu Zanyuan.Research on Gust Load and its Load Alleviation Technology of Civil Aircrafts[J].Civil Aircraft Design and Research,2012(1):17-20.
Authors:Zhao Jiwei Hu Zanyuan
Institution:Zhao Jiwei Hu Zanyuan (Shanghai Aircraft Design and Research Institute, Shanhai 200232, China)
Abstract:Due to the characteristic of large ratio wing of civil aircrafts, gust load often composes of the severe conditions of civil aircrafts. And it must be emphasized by all countries' airworthiness regulations. Moreover, owing to the elasticity of the aircraft structure, gust disturbance induces the elastic vibrations, reduces the structure stress, produces the fatigue damage, and even promote flutter. Thus it is of very importance and significance to investigate and research in gust load and gust load alleviation technologies in flight load design. This paper gives a brief introduction of gust load theories and the relevant technologies and also puts forward a type of gust load alleviation of method direct lift control to carry out gust load alleviation of the wing.
Keywords:Civil Aircrafts  Gust Load  Alleviation Techniques  Direct Lift Control
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《民用飞机设计与研究》浏览原始摘要信息
点击此处可从《民用飞机设计与研究》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号