首页|期刊导航|空气动力学学报|考虑测量干扰抑制的风洞天平拓扑优化方法

考虑测量干扰抑制的风洞天平拓扑优化方法OA

Topology optimization method for wind tunnel balance considering suppression of measurement interference

中文摘要英文摘要

针对大载荷比天平小量值分量易受干扰、测量精度低,以及传统方法难以突破性能瓶颈问题,发展了考虑测量干扰抑制的风洞天平拓扑优化设计方法.基于轴向力测量干扰模式,提出"最小柔度"和"最小干扰"两种拓扑优化模型并建立数值优化流程,结合设计域"上下镜像"和"非镜像"策略完成多组算例,并开展典型算例实物加工和地面加载验证.结果表明:该方法可获得结构清晰、可制造拓扑构型,"最小干扰"模型所得构型更简洁可靠,"非镜像"策略虽能拓展设计空间,但工艺复杂度与计算成本提升;天平实物目标分量 Fx灵敏度显著,单独施加其余载荷时最大干扰输出小于 2.3%.该方法显著提升天平抗干扰能力和测量精度,为高精度天平及力传感器设计提供了新途径.

The strain gauge balance is the core device for accurately measuring aerodynamic loads acting on aircraft models in wind tunnel tests.As a special type of six-component force sensor,its design faces greater challenges due to the constrained design space,extreme mismatch in load magnitudes across the measured components,and harsh testing conditions.For sting-type balances,the measurement accuracy of the axial force component is inherently limited,as the measuring elements are prone to nonlinear deformation and torsional interference within the restricted design space-problems that are further exacerbated under high load-ratio conditions(e.g.,when subjected to large longitudinal loads).To address the interference susceptibility and low accuracy of low-magnitude components under high load-ratios,as well as the limitations of conventional design methods,a topology optimization method considering measurement interference suppression was developed for wind tunnel balances.Based on the interference patterns of axial force measurement,two optimization models-"minimum compliance"and"minimum interference"—were proposed,and a numerical optimization framework integrating the SIMP model,the MMA algorithm,and filtering/projection techniques was established.Multiple design cases were studied using mirrored and non-mirrored design domains strategies,and a prototype was fabricated and calibrated through ground loading tests.Results show that the proposed method yields clear and manufacturable topological configurations;the"minimum interference"model produces simpler and more reliable layouts;the non-mirrored strategy expands the design space but increases manufacturing complexity and computational cost.The fabricated balance exhibits high sensitivity in the target component Fx,with a maximum interference output below 2.3%when other loads are individually applied.The proposed method significantly enhances the anti-interference capability and measurement accuracy of the wind tunnel balance,providing a new approach for the design of high-precision balances and multi-component force sensors.

闫万方;穆向阳;蒋坤;魏巍;张江

中国航天空气动力技术研究院,北京 100074中国航天空气动力技术研究院,北京 100074中国航天空气动力技术研究院,北京 100074中国航天空气动力技术研究院,北京 100074中国航天空气动力技术研究院,北京 100074

航空航天

风洞天平拓扑优化结构设计大载荷比测量干扰

wind tunnel balancetopology optimizationstructural designhigh load ratiomeasurement interference

《空气动力学学报》 2026 (8)

58-69,12

10.7638/kqdlxxb-2026.0011

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