无人直升机复合材料桨叶成型技术  

Development and Forming Technology of Full Composite Blades for Helicopter

作　　者：许大援 XU Dayuan(China Helicopter Research and Development Institute,Jingdezhen 333001,China)

机构地区：[1]中国直升机设计研究所,江西景德镇333001

出　　处：《直升机技术》2025年第1期36-41,共6页Helicopter Technique

摘　　要：以某无人直升机复合材料桨叶成型工艺过程为例,结合实际研制经验,针对研制成型过程中出现的问题进行了详细的分析和探讨,解决了复合材料桨叶成型过程中的一些关键技术和工艺难点,为类似的复合材料桨叶的成型工艺方案及设计积累了一定的经验。This paper made a detailed analysis and discussion on issues of composite blades forming process.By combining the composite blades forming process from a type of UAV with past experience of development,it solved some key issues on technique and technology during the forming process.Meanwhile,it provided some suggestions and experiences for the scheme and design of other composite blades forming process.

关 键 词：复合材料桨叶 模压成型 中温固化 

分 类 号：V261.97[航空宇航科学与技术—航空宇航制造工程]