Forming Process of Glass Fiber/Aluminum-Lithium Laminates Leading Edge Structure
HUA Xiaoge1, LI Huaguan1，2, LU Yi1, CHEN Yujie1, SUN Denghui2, TAO Jie1
( 1. College of Material Science and Technology, Nanjing University of Aeronautics and Astronautics,
Nanjing 210016, China;
2. School of Material Engineering, Nanjing Institute of Technology, Nanjing 211167, China )
Abstract：Aiming at the large curvature leading edge component, the self-forming characteristic of glass fiber/aluminum-
lithium super hybrid laminates (NFMLs) was studied. The results demonstrated that self-forming technology was
feasible to manufacture the large curvature NFMLs component such as the leading edge parts. The investigated component
exhibited no obvious interlaminar defect, presenting good fittability and thickness uniformity. Meanwhile, the forming process
hardly resulted in the generation of large residual stress, which provided a reference for the application of super hybrid
composites in the aircraft wing skin structure.
作者简介: 华小歌
硕士研究生，致力于纤维金属层板
制备及G l a r e 层板的性能评价工作，对
G l a r e 层板的力学性能进行了有限元分
析和试验研究。
引用本文:
华小歌1，李华冠1，2，陆 一1，陈虞杰1，孙邓辉2，陶 杰1. 玻璃纤维-铝锂合金层板机翼前缘结构的成型工艺研究*[J]. 航空制造技术, 2017, 60(16): 58-63.
HUA Xiaoge1, LI Huaguan1，2, LU Yi1, CHEN Yujie1, SUN Denghui2, TAO Jie1. Forming Process of Glass Fiber/Aluminum-Lithium Laminates Leading Edge Structure. Aeronautical Manufacturing Technology, 2017, 60(16): 58-63.
2017, 
