噪声与振动控制
譟聲與振動控製
조성여진동공제
NOISE AND VIBRATION CONTROL
2015年
3期
5-9
,共5页
吴越%肖新标%刘佳%赵悦%温泽峰
吳越%肖新標%劉佳%趙悅%溫澤峰
오월%초신표%류가%조열%온택봉
振动与波%小弹性模量%振动梁法%损耗因子%阻尼测试
振動與波%小彈性模量%振動樑法%損耗因子%阻尼測試
진동여파%소탄성모량%진동량법%손모인자%조니측시
vibration and wave%low Young’s modulus%vibrating beam method%loss factor%damping test
振动梁法可以获取“金属层+阻尼层+金属层”三明治梁的结构损耗因子,进而求得阻尼材料的材料损耗因子。但是通过理论研究发现,当阻尼材料的弹性模量低于10 MPa时,在外载荷作用下,三明治梁的上下金属层对阻尼层产生明显的横向挤压,不满足振动梁法的理论假设。为此,提出一种仿真与试验相结合的方法获取了HT 800、Regufoam 2000和SR 450这三种小弹性模量阻尼材料的材料损耗因子。在试验部分,利用振动梁法获取三明治梁结构阻尼损耗因子,以此作为仿真中结构损耗因子的目标值。仿真部分,建立三明治梁有限元模型,通过不断改变材料损耗因子的输入值获取模型相应的结构损耗因子,直到仿真与试验结构损耗因子相等时,仿真中相应的材料损耗因子值即为小弹性模量阻尼材料损耗因子。该种测试方法为小弹性模态阻尼材料阻尼测试提供了参考。
振動樑法可以穫取“金屬層+阻尼層+金屬層”三明治樑的結構損耗因子,進而求得阻尼材料的材料損耗因子。但是通過理論研究髮現,噹阻尼材料的彈性模量低于10 MPa時,在外載荷作用下,三明治樑的上下金屬層對阻尼層產生明顯的橫嚮擠壓,不滿足振動樑法的理論假設。為此,提齣一種倣真與試驗相結閤的方法穫取瞭HT 800、Regufoam 2000和SR 450這三種小彈性模量阻尼材料的材料損耗因子。在試驗部分,利用振動樑法穫取三明治樑結構阻尼損耗因子,以此作為倣真中結構損耗因子的目標值。倣真部分,建立三明治樑有限元模型,通過不斷改變材料損耗因子的輸入值穫取模型相應的結構損耗因子,直到倣真與試驗結構損耗因子相等時,倣真中相應的材料損耗因子值即為小彈性模量阻尼材料損耗因子。該種測試方法為小彈性模態阻尼材料阻尼測試提供瞭參攷。
진동량법가이획취“금속층+조니층+금속층”삼명치량적결구손모인자,진이구득조니재료적재료손모인자。단시통과이론연구발현,당조니재료적탄성모량저우10 MPa시,재외재하작용하,삼명치량적상하금속층대조니층산생명현적횡향제압,불만족진동량법적이론가설。위차,제출일충방진여시험상결합적방법획취료HT 800、Regufoam 2000화SR 450저삼충소탄성모량조니재료적재료손모인자。재시험부분,이용진동량법획취삼명치량결구조니손모인자,이차작위방진중결구손모인자적목표치。방진부분,건립삼명치량유한원모형,통과불단개변재료손모인자적수입치획취모형상응적결구손모인자,직도방진여시험결구손모인자상등시,방진중상응적재료손모인자치즉위소탄성모량조니재료손모인자。해충측시방법위소탄성모태조니재료조니측시제공료삼고。
The structural loss factor of the metal sandwich beam with a damping core can be determined by using the vibration beam test method. Then, the material loss factor of the damping layer can be calculated. But the present theoretical study shows that if the Young’s modulus of the damping layer material is lower than 10 MPa, the damping layer can be strongly and transversely compressed by the metal-layers under the external loading. This phenomenon breaks the assumption of the vibration beam method. Therefore, a method combining testing and simulation was used to obtain the material loss factors of three low Young’s modulus damping materials, HT 800, Regufoam 2000 and SR 450. Using the vibration beam method in the testing, the structural loss factor of the sandwich beam was obtained. Then, this factor was used as the target of the simulation. In the simulation, the finite element model of the sandwich beam was developed to calculate the structural loss factor. Then, by changing different input values of the material loss factor until the simulation output of the structural loss factor identifies that of the testing, the real value of the material loss factor could be obtained. This method provides a reference for determination of the material loss factors of low Young’s modulus damping materials.