Review on the automated fiber placement process for the aero-engine composite fan blade and its feasibility in element level

被引:0
|
作者
Zhou, He [1 ,2 ]
Li, Xiaoqiang [1 ,2 ]
Shao, Chengjie [3 ]
Li, Xiaobing [4 ]
Li, Yong [1 ]
Li, Dongsheng [1 ,2 ]
Feng, Jinzhang [5 ]
Ding, Xilun [1 ,2 ]
Zhu, Yu [6 ]
机构
[1] Beihang Univ, Sch Mech Engn & Automat, Beijing 100191, Peoples R China
[2] Beihang Univ, Ningbo Innovat Res Inst, Ningbo 315800, Peoples R China
[3] COMAC Shanghai Aircraft Mfg Co Ltd, Shanghai 201324, Peoples R China
[4] AVIC Composite Co Ltd, Beijing 101300, Peoples R China
[5] AECC Commercial Aircraft Engine Co Ltd, Shanghai 200241, Peoples R China
[6] Aero Engine Acad China, Beijing 101304, Peoples R China
关键词
Aero-engine fan blade; Polymer-matrix composites (PMCs); Automated fiber placement (AFP); Non-destructive testing; PROCESS PARAMETERS; OPTIMAL-DESIGN; HEAT-TRANSFER; MICROSTRUCTURE; OPTIMIZATION; BEHAVIOR; SURFACE;
D O I
10.1016/j.compositesa.2025.108875
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The application of carbon fiber-reinforced polymer matrix composite (CFRP) fan blades is crucial for weight reduction in high bypass ratio turbofan aircraft engines. Automated fiber placement (AFP) has the greatest potential for automating the production of CFRP fan blades. To help achieve high manufacturing quality and stability of fan blades, this review summarizes the key areas of AFP forming fan blades and generates an overall understanding of the key scientific challenges. Based on these understandings, an integrated research and development method for AFP (IRDM-AFP) is proposed, integrating virtual and measured data-driven modeling methods for parameter optimization to assist the manufacturing of high shape accuracy and performance of fan blades. The feasibility and necessity of IRDM-AFP is demonstrated through a preliminary study of AFP forming experiment for fan blade in an element level. This review provides a promising method for subsequent research and applications on AFP forming of CFRP fan blades.
引用
收藏
页数:20
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