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dc.contributor.advisorZoltan S. Spakovszky.en_US
dc.contributor.authorLiu, Lixian, Ph. D. Massachusetts Institute of Technologyen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Mechanical Engineering.en_US
dc.date.accessioned2008-11-10T20:02:58Z
dc.date.available2008-11-10T20:02:58Z
dc.date.issued2005en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/33921
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2005.en_US
dc.description"September 2005."en_US
dc.descriptionIncludes bibliographical references (p. [281]-283).en_US
dc.description.abstractThe goal of the MIT micro-engine project is to develop high-speed rotating Power MEMS (Micro-Electro-Mechanical Systems) using computer chip fabrication technologies. To produce high power (10-50 W) in a small volume (less than one cubic centimeter), the micro-turbo-machinery must be spun at a rotational speed on the order of million rpm. This ultra-high rotational speed, together with the small length-to-diameter ratio (L/D<0.07) limited by the chip manufacturing technology, entails many challenges in the design of the bearing system, such as an ultra-high whirl ratio of over 20 (compared with a whirl ratio of 2 for large-scale journal bearings) and a DN number of order 10 million mm-rpm. The thesis presents a newly developed theory for the hydrostatic gas journal- bearings for the micro-engine devices. To investigate the underlying physical mechanisms, fluid models are established to analytically calculate the hydrostatic, hydrodynamic, and damping bearing forces. It is found from first principles that the hydrodynamic force due to viscous drag becomes dominant with an L/D<<1 and acts in the opposite direction of the hydrodynamic force due to rotor pumping action.en_US
dc.description.abstract(cont.) As a result, the net destabilizing hydrodynamic force can vanish for certain bearing geometries, causing singular behavior in the whirl instability limit. Thus, the ultra-short bearing is suggested to enable a large DN number and a high whirl ratio in the micro-journal-bearing system. A novel variation of the axial-flow hydrostatic micro gas journal-bearing concept is introduced, which yields anisotropy in bearing stiffness. By departing from axial symmetry and introducing biaxial symmetry in hydrostatic stiffness, the bearing's top speed is increased and the fabrication tolerance requirements are substantially relieved. The third-order nonlinear resonances in the micro-journal-bearing system are investigated by both analytical models and numerical simulations, and the predictions from these models agree well with the experimental observations. The model predicts a subharmonic resonance in the isotropic journal-bearing system, with a slow rotating noncircular orbit such that the symmetry of the system is broken by itself in the nonlinear resonance.en_US
dc.description.abstract(cont.) Furthermore, the anisotropic journal-bearing system is found to be able to engage in multi-type nonlinear resonances: superharmonic resonances at one third of the natural frequencies, subharmonic resonances at three times the natural frequencies, and combinations (such as the average) of the two natural frequencies. The conditions under which these resonances can occur are derived analytically and are then verified by numerical simulation.en_US
dc.description.statementofresponsibilityby Lixian Liu.en_US
dc.format.extent283 p.en_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectMechanical Engineering.en_US
dc.titleTheory for hydrostatic gas journal bearings for micro-electro-mechanical systemsen_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Mechanical Engineeringen_US
dc.identifier.oclc67293632en_US


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