摘要
初步探讨了飞机机翼翼梁接头高强度铝耳片与钢衬套过盈配合在应力腐蚀与干涉连接综合作用下 ,对耳片疲劳寿命的影响及影响程度 ,并提出了结构设计时应遵循的几项原则。
The influence of stress corrosion combined with interference fit between high-strength aluminum alloy wing spar joint and steel lining on the joint fatique life is preliminarily discussed.Some structural design guidelines are suggested.
出处
《飞机设计》
2003年第4期13-18,共6页
Aircraft Design
