铝锂合金机身壁板抗压能力对比  

Comparison on Compressive Bearing Capacity of Aluminum Lithium Alloy Fuselage Panel

作　　者：白杰[1] 郭沛欣[1] 张景新[1] 

机构地区：[1]中国商飞上海飞机设计研究院

出　　处：《航空制造技术》2012年第10期78-79,共2页Aeronautical Manufacturing Technology

摘　　要：本文通过有限元计算及试验两种方法对比分析了铝锂合金蒙皮和挤压铝锂合金长桁组成的机身壁板与铝锂合金蒙皮和钣弯7000系列高强度铝合金长桁所组成的壁板的抗压能力。通过分析验证得到了两种机身壁板的抗拉承载能力,并比较出了两种壁板的抗压承载能力强弱。分析结果表明,铝锂合金蒙皮和挤压铝锂合金长桁组成的机身壁板抗压承载能力高于等截面的铝锂合金蒙皮和钣弯7000系列高强度铝合金长桁所组成的壁板。Canparison of the compressive bearing capacity between the panel with aluminum lithium alloy skin adding aluminum lithium alloy stringers and the panel with aluminum lithium alloy skin adding 7000 series high strength aluminum alloy stringers is presented by the finite element calculation and tests. Through the calculation and the tests, the compressive bearing capacity of the two kinds panels are gotten. It is shown that the compressive bearing capacity of the panel with aluminum lithium alloy skin adding aluminum lithium alloy stringers is better than the other kinds of fuselage panels.

关 键 词：抗压承载能力 壁板 蒙皮 长桁 

分 类 号：V215.22[航空宇航科学与技术—航空宇航推进理论与工程]