期刊文献+

弹性箔片动压径向气体轴承动特性的实验研究 被引量:15

Experimental Study on Dynamic Performance of Compliant Aerodynamic Foil Journal Air Bearings
下载PDF
导出
摘要 建立了新型弹性箔片动压气体轴承性能测试实验台,在静载60 N、转速9 000 r/m in条件下进行轴承性能测试试验,通过中心插值法获得轴承中心的扰动速度和加速度,采用时域最小二乘法计算不同激振频率下的8个轴承动态线性刚度和阻尼系数,考察了激振频率对轴承动特性系数的影响.结果表明:轴颈中心扰动轨迹为椭圆形且振幅随动态激振频率增加而增大;刚度和阻尼系数的直接项随动态激振频率增加而减小;交叉刚度和阻尼相对激振频率的变化较小,且其值小于直接项;当激振频率与轴颈转动频率相同时,工频成分的影响较大,轴心扰动幅值明显增大,刚度和阻尼的直接项小于其它频率时的值. A test rig was built to study the performances of new compliant aerodynamic foil journal air bearings. This paper introduced an experimental method to identify eight linear dynamic coefficients of the foil gas bearings under different excitation frequencies. The experiment was performed when the static load and the rotating speed were 60 N and 9 000 rpm, respectively. The disturbed speed and acceleration of the journal center were obtained by the method of center difference of its displacement. In time domain, the linear stiffness and damping coefficients of each excitation frequency were calculated by means of least mean square. Finally, the effect of the excitation frequency on the dynamic characteristics of the bearing was investigated. Experimental results show that the vibration orbit of the journal center is elliptic. And with the excitation frequency increasing, the perturbation amplitudes of the journal center increase, but the direct terms of the stiffness and damping coefficients of the bearing decrease. The cross-coupling terms change little with the changes of dynamic excitation frequency, and their values are much smaller than those of the direct terms. When the excitation frequency is equal to the working frequency of the rotor, because of the effect of the components of the working frequency, the perturbation amplitude of the journal center increase significantly and the direct terms of the stiffness and damping coefficients are much smaller than those of other excitation frequencies.
出处 《摩擦学学报》 EI CAS CSCD 北大核心 2006年第4期353-357,共5页 Tribology
基金 国家自然科学基金资助项目(50275116 50475088) 国家863重大项目资助(2002AA503020)
关键词 涡轮机械 箔片气体轴承 激振频率 线性刚度和阻尼系数 中心插值 turbomechinery, foil air bearings, excitation frequency, linear stiffness and damping coefficients, center difference
  • 相关文献

参考文献12

  • 1Blok H,VanRossum J J.The foil bearing-a new departure in hydrodynamic lubrication[J].ASLE Journal of Lubrication Engineering,1953,9:316-330.
  • 2Hayashi K.Development of aerodynamics foil bearings for highspeed rotor[J].21 th Leeds-Lyon Symposium Tribology,1994.
  • 3Heshmat H,Shapiro W,Gray S.Development of foil journal bearings for high load capacity and high speed whirl stability[J].Transaction of ASME Journal of Lubrication Technology,1982,104:149-156.
  • 4侯予,熊联友,王瑾,刘井龙,陈纯正.透平膨胀机新型动压径向气体轴承的试验研究[J].低温工程,1999(4):231-235. 被引量:1
  • 5Heshmat H.A feasibility study on the use of foil bearings in cryogenic turbopumps[J].AIAA Paper No.91-2103,The 27 th AIAA/SAE/ASME Joint Propulsion Conference,Sacremento,CA,1991.
  • 6Heshmat H,Hermel P.Compliant foil bearing technology and their application to high speed turbomachinery[J].19 th LeedsLyon Symposium on Tribology,Thin Films in Tribology,Leeds,UK,1992.
  • 7虞烈,戚社苗,耿海鹏.弹性箔片空气动压轴承的完全气弹润滑解[J].中国科学(E辑),2005,35(7):746-760. 被引量:26
  • 8Lund J W.Calculation of stiffness and damping properties of gas bearings[J].Transaction of ASME Journal of Lubrication Technology,1968,10:793-803.
  • 9Czolczynski K.How to obtain stiffness and damping coefficients of gas bearings[J].Wear,1996,201:265-275.
  • 10Heshmat H,Roger Ku C P.Structural damping of self-acting compliant foil journal bearings[J].Transaction of ASME Journal of Tribology,1994,116:76-82.

二级参考文献14

  • 1Radil K, Howard S, Dykas B. The role of radial clearance on the performance of foil air bearings. Tribology Transactions, 2002, 45(4): 485~490
  • 2Dellacorte C, Valco M J. Load capacity estimation of foil air journal bearings for oil-free turbomachinery applications. Tribology Transactions, 2000, 43(4): 795~801
  • 3Howard S A, Dellacorte C, Valco M J, et al. Steady-state stiffness of foil air journal bearings at elevated temperatures. Tribology Transactions, 2001, 44(3): 489~493
  • 4Heshmat H. Operation of foil bearings beyond the bending critical mode. Journal of Tribology, Transactions of the ASME, 2000, 122(1): 192~198
  • 5Ku C-P R, Heshmat H. Compliant foil bearing structural stiffness analysis: part I - theoretical model including strip and variable bump foil geometry. Journal of Tribology, Transactions of the ASME, 1992, 114(2): 394~400
  • 6Ku C-P R, Heshmat H. Structural stiffness and coulomb damping in compliant foil journal bearings: theoretical considerations. STLE Tribology Transactions, 1994, 37(3): 525~533
  • 7Heshmat H, Ku C-P R. Structural damping of self-acting compliant foil journal bearings. Journal of Tribology, Transactions of the ASME, 1994, 116(1): 76~82
  • 8Walowit J. Gas lubricated foil bearing technology development for propulsion and power system. Technical report, Air Force Aero Propulsion Laboratory, Ohio, 1973
  • 9Ku C-P R, Heshmat H. Structural stiffness and coulomb damping in compliant foil journal bearings: parametric studies. STLE Tribology Transactions, 1994, 37(3): 455~462
  • 10Lund J W. The stability of an elastic rotor in journal bearings with flexible, damped supports. Journal of Applied Mechanics, Transactions of the ASME, Series E, 1965, 87: 911~920

共引文献25

同被引文献204

引证文献15

二级引证文献76

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部