机械工程学报
機械工程學報
궤계공정학보
CHINESE JOURNAL OF MECHANICAL ENGINEERING
2014年
22期
16-21
,共6页
全息动平衡%初相矢%各向异性%时间耦合%相位补偿
全息動平衡%初相矢%各嚮異性%時間耦閤%相位補償
전식동평형%초상시%각향이성%시간우합%상위보상
holobalacing%initial phase vector%anisotropy of rotor systems%time coupling%phase compensation
全息动平衡法融合转子系统测振截面中两个相互垂直方向的振动参量制定系统的配重方案,以保证各测振截面周向各方向均具有良好的振动;然而全息动平衡法以初相矢为平衡目标制定的配重方案有时会出现不能保证测振截面周向振动的情况。通过各向异性转子系统失衡和响应关系的分析研究,发现初相矢与转子系统的失衡量之间存在线性映射关系;在原始失衡与配重截面存在轴向位置差异的条件下,受系统降维等效的影响,失衡和响应“椭圆映射”关系中的时间耦合问题是影响初相矢平衡方案不可靠的一个主要原因。在以上分析的基础上,提出一种相位补偿方法修正并优选初相矢对应的配重方案,以消除时时间耦合问题的影响;通过仿真试验,现场案例分析,验证了相位补偿方法对应配重方案的可靠性。
全息動平衡法融閤轉子繫統測振截麵中兩箇相互垂直方嚮的振動參量製定繫統的配重方案,以保證各測振截麵週嚮各方嚮均具有良好的振動;然而全息動平衡法以初相矢為平衡目標製定的配重方案有時會齣現不能保證測振截麵週嚮振動的情況。通過各嚮異性轉子繫統失衡和響應關繫的分析研究,髮現初相矢與轉子繫統的失衡量之間存在線性映射關繫;在原始失衡與配重截麵存在軸嚮位置差異的條件下,受繫統降維等效的影響,失衡和響應“橢圓映射”關繫中的時間耦閤問題是影響初相矢平衡方案不可靠的一箇主要原因。在以上分析的基礎上,提齣一種相位補償方法脩正併優選初相矢對應的配重方案,以消除時時間耦閤問題的影響;通過倣真試驗,現場案例分析,驗證瞭相位補償方法對應配重方案的可靠性。
전식동평형법융합전자계통측진절면중량개상호수직방향적진동삼량제정계통적배중방안,이보증각측진절면주향각방향균구유량호적진동;연이전식동평형법이초상시위평형목표제정적배중방안유시회출현불능보증측진절면주향진동적정황。통과각향이성전자계통실형화향응관계적분석연구,발현초상시여전자계통적실형량지간존재선성영사관계;재원시실형여배중절면존재축향위치차이적조건하,수계통강유등효적영향,실형화향응“타원영사”관계중적시간우합문제시영향초상시평형방안불가고적일개주요원인。재이상분석적기출상,제출일충상위보상방법수정병우선초상시대응적배중방안,이소제시시간우합문제적영향;통과방진시험,현장안례분석,험증료상위보상방법대응배중방안적가고성。
Through fusion of vibration information collected from two mutually perpendicular radial directions, the balancing scheme obtained by Holobalancing method can ensure the overall vibration level at any radial directions. However, there are still some deficiencies in the Holobalancing method when the initial phase vector(IPV) is used as the balancing object. According to the analysis of the relationship between mass unbalance response and the anisotropic rotor-bearing system, it is found that the unbalance mass is linearly mapped to the IPV. If the axial position of the original unbalance mass is inconsistent with the balancing planes, the time coupling problem brought by the elliptical mapping relationship between mass unbalance and system response is the main reason that makes the balancing scheme unreliable. A phase compensation method is presented to eliminate this problem through a balancing scheme optimization process. Finally, the reliability of this method is verified by simulation experiment and case study.