Modeling and Optimization of Manufacturing Processes of the Hybrid Composite Propeller Blade

被引:0
|
作者
Puzyretskii E.A. [1 ]
Shabalin L.P. [1 ]
Savinov D.V. [1 ]
Mareskin I.V. [2 ]
机构
[1] Tupolev Kazan National Research Technical University, ul. Karla Marksa 10, Kazan
[2] Zhukovsky Central Aerohydrodynamics Institute (TsAGI), ul. Zhukovskogo 1, Zhukovsky
来源
Russian Aeronautics | 2022年 / 65卷 / 03期
基金
俄罗斯基础研究基金会;
关键词
composite material; finite element; hybrid structure; mold deflection; propeller blade; technological parameters;
D O I
10.3103/S1068799822030199
中图分类号
学科分类号
摘要
Abstract: The main stages of manufacturing a composite part are considered and calculation models for the analysis of draping, impregnation, curing and warping are developed. A good convergence of the simulation data with the results of technological experiment was obtained. © 2022, Allerton Press, Inc.
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页码:590 / 599
页数:9
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