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螺旋锥齿轮模态试验与模型修正

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为准确提取螺旋锥齿轮模态参数,构建精确动力学模型,通过试验与仿真相结合的方法,采用移动力锤法进行模态试验,提取模态参数;基于实测数据建立精确仿真模型并进行模态分析;采用初等旋转变换法修正仿真模态振型,得到准确的试验和仿真模态置信度,提高分析精度;以试验模态频率为目标,采用响应面法修正模型材料参数.修正后固有频率最大相对误差由0.83%下降到0.353%,提高了仿真模型精度.试验与仿真频响分析结果表明:由仿真模型不准确导致的移频现象和加速度幅值误差得到有效控制,验证了动力学模型的准确性.研究方法为螺旋锥齿轮进一步的结构优化和减振避振奠定基础.
Modal test and model modification of spiral bevel gears
To accurately extract spiral bevel gears'modal parameters and construct an accurate dynamic model,a combination of experimental and simulation methods were used to conduct modal tests using the moving force hammer method to extract modal parameters;an accurate simulation model was established based on measured data and modal analysis was conducted;the elementary rotation transformation method was used to correct the simulation mode shapes,and the accurate confidence of the test and simulation modes was obtained to improve the analysis accuracy;taking the experimental modal frequency as the target,the response surface method was used to correct the material parameters of the model.After the correction,the maximum relative error of natural frequency was reduced from 0.83%to 0.353%,which improved the accuracy of the simulation model.The experimental and simulation frequency response analysis results showed that the frequency shift phenomenon and acceleration amplitude error caused by inaccurate simulation models were effectively controlled,verifying the accuracy of the dynamic model.The research method lays the foundation for further structural optimization and vibration reduction and avoidance of spiral bevel gears.

modal parameterspiral bevel gearmodal testmodel modifiedresponse surface method

何宏图、曹雪梅、许浩、侯圣文

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河南科技大学机电工程学院,河南洛阳 471003

中国航发中传机械有限公司,长沙 410200

陕西法士特齿轮有限责任公司陕西省齿轮传动重点试验室,西安 710119

模态参数 螺旋锥齿轮 模态试验 模型修正 响应面法

2024

航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
年,卷(期):2024.39(11)