Reducing the Structural Mass of Large Direct Drive Wind Turbine Generators through Triply Periodic Minimal Surfaces Enabled by Hybrid Additive Manufacturing

被引:9
|
作者
Hayes, Austin C. [1 ,2 ]
Whiting, Gregory L. [1 ,2 ]
机构
[1] Univ Colorado, Paul M Rady Dept Mech Engn, Boulder, CO 80303 USA
[2] 1111 Engn Dr Engn Mech Wing, Boulder, CO 80309 USA
来源
CLEAN TECHNOLOGIES | 2021年 / 3卷 / 01期
基金
美国国家科学基金会;
关键词
permanent magnet direct drive generator; additive manufacturing; structural optimization; implicit modeling; TPMS lattices; generative design; LATTICE STRUCTURES; TOPOLOGY OPTIMIZATION; COMPRESSIVE BEHAVIOR; DESIGN; SCAFFOLDS;
D O I
10.3390/cleantechnol3010013
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
As the power output of direct drive generators increases, they become prohibitively large with much of this material structural support. In this work, implicit modeling was coupled to finite element analysis through a genetic algorithm variant to automate lattice optimization for the rotor of a 5 MW permanent magnet direct drive generator for mass reduction. Three triply periodic minimal surfaces (TPMS) were chosen: Diamond, Schwartz Primitive, and Gyroid. Parameter and functionally graded lattice optimization were employed to reduce mass within deflection criteria. Inactive mass for the 5 MW Diamond, Schwartz Primitive, and Gyroid optimized designs was 10,043, 10,858, and 10,990 kg, respectively. The Schwartz Primitive rotor resulted in a 34% reduction in inactive mass compared to a 5 MW baseline design. Radial and axial deflections were below the critical limit of 0.65 and 32.17 mm, respectively. The lowest torsional deflection was seen in the Schwartz Primitive TPMS lattice at 3.89 mm. Based on these designs, hybrid additive manufacturing with investment casting was used to validate manufacturability in metal. A fused deposition modeling (FDM) TPMS topology was printed for validation of the FEA results. Comparison between digital image correlation of the FDM printed design and FEA design resulted in a 6.7% deformation difference for equivalent loading conditions.
引用
收藏
页码:227 / 242
页数:16
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