首页|期刊导航|机械与电子|一种具备扭矩滑模控制加载的风洞天平校准系统设计研究

一种具备扭矩滑模控制加载的风洞天平校准系统设计研究OA

Research on the Design of a Wind Tunnel Balance Calibration System with Torque Sliding Mode Control Loading

中文摘要英文摘要

针对六分量风洞天平在给定工况下的校准需求,提出了一种具备扭矩滑模控制加载的新型校准装置.该装置通过旋转驱动、重力补偿、扭矩加载和复合加载4大功能模块,实现了六分量载荷的独立/组合施加与传递.利用ANSYS平台进行了有限元仿真验证:在极限载荷下,整机最大等效应力为86.405 MPa,远低于材料屈服强度;天平安装轴段变形为12 μm,满足高精度测力要求;前六阶固有频率为155.04~589.25 Hz,有效避开了工作转速范围内的激振频率.该研究为风洞天平提供了可靠的校准解决方案.

To meet the rigorous calibration requirements for six-component wind tunnel balances un-der given working conditions,a novel calibration device with torque loading regulated by sliding mode con-trol(SMC)is proposed in this paper.The system integrates four specialized functional modules-rotary drive,gravity compensation,torque loading,and composite loading-to achieve the independent and coupled application of six-component loads.Finite element analysis(FEA)performed via the ANSYS platform validates the structural integrity and precision of the design.Under extreme loading conditions,the maxi-mum equivalent stress of the assembly is 86.405 MPa,which remains well within the yield strength of the material.Furthermore,the deformation at the balance mounting shaft section is restricted to 12 μm,satis-fying the stringent requirements for high-precision force measurement.Modal analysis indicates that the first six natural frequencies range from 155.04 to 589.25 Hz,effectively isolating the system from the exci-tation frequencies within the operating speed range.This research provides a robust and reliable calibration solution for the high-fidelity measurement of wind tunnel balances.

罗宇;徐志祥;金峰;董峻辰;魏向前;白鑫博;李福东

大连理工大学机械工程学院,辽宁大连 116024大连理工大学机械工程学院,辽宁大连 116024中国航空工业空气动力研究院,黑龙江哈尔滨 150001大连理工大学机械工程学院,辽宁大连 116024大连理工大学机械工程学院,辽宁大连 116024大连理工大学机械工程学院,辽宁大连 116024中国航空工业空气动力研究院,黑龙江哈尔滨 150001

航空航天

风洞天平校准装置有限元分析制动扭矩控制

wind tunnel balancecalibration devicefinite element analysis(FEA)braking torque control

《机械与电子》 2026 (5)

30-34,5

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