某型飞机复材翼盒结构设计

Structure Design on Composite Wing Box of an Aircraft

针对某型机机翼开展复合材料结构设计,在此基础上对结构形式、材料体系、密封形式、工艺方案等方面进行综合论述,验证主承力结构复材整体化设计及制造的可行性,可为主承力复材结构的工程化应用提供参考。

Concerning the composite structure developed for an aircraft wing, this paper presents a comprehensive description on structure type, material system, sealing ways, process program etc. It verifies the feasibility of designing and manufacturing composite integration of main force-bearing structure, which provides the reference for engineering application of main force-bearing composite structure.