国防科技大学学报
國防科技大學學報
국방과기대학학보
JOURNAL OF NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY
2014年
6期
37-42
,共6页
孔晓鹏%曾新吾%田章福
孔曉鵬%曾新吾%田章福
공효붕%증신오%전장복
动圈扬声器%涡流效应%等效电路%曲线拟合
動圈颺聲器%渦流效應%等效電路%麯線擬閤
동권양성기%와류효응%등효전로%곡선의합
moving-coil loudspeakers%eddy-current effect%equivalent electrical circuit%curve-fitting
由音圈涡流效应引起的涡流阻抗对小信号下动圈扬声器的高频响应影响较大。基于集总参数系统等效电路法,将涡流阻抗的幅值和相位分别表示为角频率的幂指数函数,提出了音圈涡流阻抗的幂指模型。使用激光阻抗测量系统,测量得到了3种类型6只扬声器单元的电阻抗曲线,并采用最小二乘法对实测阻抗进行曲线拟合,得到了涡流阻抗的模型参数。分析了模拟阻抗值与实测值的误差,结果表明:幂指模型的模拟结果准确反映了实测涡流阻抗随频率的变化规律,幅值和相位误差均较小,与实验吻合较好。
由音圈渦流效應引起的渦流阻抗對小信號下動圈颺聲器的高頻響應影響較大。基于集總參數繫統等效電路法,將渦流阻抗的幅值和相位分彆錶示為角頻率的冪指數函數,提齣瞭音圈渦流阻抗的冪指模型。使用激光阻抗測量繫統,測量得到瞭3種類型6隻颺聲器單元的電阻抗麯線,併採用最小二乘法對實測阻抗進行麯線擬閤,得到瞭渦流阻抗的模型參數。分析瞭模擬阻抗值與實測值的誤差,結果錶明:冪指模型的模擬結果準確反映瞭實測渦流阻抗隨頻率的變化規律,幅值和相位誤差均較小,與實驗吻閤較好。
유음권와류효응인기적와류조항대소신호하동권양성기적고빈향응영향교대。기우집총삼수계통등효전로법,장와류조항적폭치화상위분별표시위각빈솔적멱지수함수,제출료음권와류조항적멱지모형。사용격광조항측량계통,측량득도료3충류형6지양성기단원적전조항곡선,병채용최소이승법대실측조항진행곡선의합,득도료와류조항적모형삼수。분석료모의조항치여실측치적오차,결과표명:멱지모형적모의결과준학반영료실측와류조항수빈솔적변화규률,폭치화상위오차균교소,여실험문합교호。
The eddy current impedance in voice coil affects the behaviors of the high-frequency response of moving-coil loudspeakers under small input voltage.Based on the equivalent electrical circuit method in lumped parametric system and using the power exponent function of angular frequency to fit the magnitude and phase of the eddy current impedance,the power exponent function model of voice-coil eddy-current impedance was presented.The electrical impedance curves of six loudspeaker units in three types were obtained by using the laser impedance measurement system and the model parameters of eddy current impedance were identified by fitting the measured impedance curves with the least square method. Error comparisons between the simulative values and the measured data show that the power exponent function model can accurately reflect the change relationships between the measured eddy-current impedance and frequency.The magnitude and phase have small errors and behave good correspondences with the measured data.