基于参数化组件定义的复合材料旋翼桨叶结构优化设计

doi:10.7527/S1000-6893.2013.0092

Abstract

Abstract:

A composite rotor blade structure optimization design approach based on parametric module definition is presented to improve design efficiency for engineering application. By taking a C-spar composite rotor blade as the research object, both the profile and the overall structure optimization models are built based on parametric module definition. By using the results of the profile optimization, the initial values of the overall structure optimization model are obtained. Then, the overall structure optimization is implemented to obtain the best blade structure. A case study is performed. The results demonstrate that the proposed method can complete the structure design of composite rotor blades efficiently.

Key words: helicopter, composite material, blade, structure design, optimization design

CLC Number:

YANG Jianling, ZHANG Liyan, ZHOU Shaohua. Composite Helicopter Rotor Blade Optimization Design Based on Parametric Module Definition[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, doi: 10.7527/S1000-6893.2013.0092.

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Composite Helicopter Rotor Blade Optimization Design Based on Parametric Module Definition

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