首页 | 本学科首页   官方微博 | 高级检索  
     


A rotating field mhd hydrostatic thrust bearing
Authors:Chuen-Yen Chow and R. D. Brunell
Affiliation:(1) Coop. Inst. for Research in the Environm. Sci. and Dept. of Aerospace Eng. Sci., University of Colorado, Boulder, Colo., USA;(2) Dept. of Aero-Space Engineering, University of Notre Dame, Notre Dame, Ind., USA
Abstract:
It is found that the load capacity of a magnetohydrodynamic thrust bearing with a rotating disk can be increased by rotating the axial magnetic field at a suitable speed in a direction opposite to that of the disk rotation. This method of improving the bearing performance is considered to be efficient if the Hartmann number is not too large. Thus for a given load, the size and weight of the magnet to be used in a thrust bearing with rotating field can be reduced considerably.Nomenclature a radius of plenum recess - b outside disk radius - B0 magnetic induction of applied axial magnetic field - Emacr hE0sgr1/2/aohgrmgr1/2, nondimensionalized electric field - E0 radial electric field at r=a - Er radial electric field - h half of lubricant film thickness - M (sgrB02h2/mgr)1/2, Hartmann number - P pressure - Pe pressure at r=b - P0 pressure at r=a - Q volume flow rate of lubricant - Q0 volume flow rate of a nonrotating bearing in the absence of applied magnetic field - r radial coordinate - u, v fluid velocity components in radial and circumferential directions, respectively - W load capacity of bearing - W0 load capacity of a nonrotating bearing in the absence of a magnetic field having a flow rate which the same bearing would have at Hartmann number M - z axial coordinate - theta azimuthal coordinate - mgr coefficient of viscosity of lubricant - mgre magnetic permeability - rgr fluid density - sgr electrical conductivity - ohgr angular velocity of rotating disk - ohgrC critical disk velocity at which W=0 - ohgrM angular velocity of axial magnetic field - 
$$(omega _{text{M}} )_{{text{opt}}}$$
optimum angular velocity of magnetic fieldOn leave of absence from Department of Aero-Space Engineering, University of Notre Dame, Notre Dame (Ind.), U.S.A.
Keywords:
本文献已被 SpringerLink 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号