摘要
为满足全机静力试验加载、测控以及检查的需求,在国内静力试验中首次采用钢架结构的框架设计技术,参照建筑钢构形式及相应的设计规范,提出一体化框架设计技术,并提出了一套可行、通用的一体化框架设计规程,为后续一体化框架设计提供参考。
In order to meet the requirements of load,measure and controll and inspection in the static test of large transport aircraft,the frame design technology of steel frame structure was first adopted in the domestic static test.Referring to the form of building steel structure and the corresponding design specifications,an integrated frame design technology was put forward,and a feasible and universal integrated frame design specification was put forward,which provided a reference for the follow-up integrated frame design.
作者
杨鹏飞
Yang Pengfei(Full Scale Aircraft Structure Static/Fatigue Laboratory of Aircraft Strength Research Institute of China,Xi'an Shaanxi 710065,China)
出处
《工程与试验》
2019年第2期128-130,共3页
Engineering and Test
关键词
一体化加载框架
钢架结构
设计规程
integrated loading frame
steel frame structure
design specification
