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    • 1. 发明申请
    • Hybrid touchdown bearing system
    • 混合触地轴承系统
    • US20090085419A1
    • 2009-04-02
    • US11904590
    • 2007-09-28
    • James ArseneauxJimpo Wang
    • James ArseneauxJimpo Wang
    • H02K7/02H02K7/09F16C19/54F16C32/06
    • H02K7/025F16C32/0442F16C39/02F16C39/066F16C2361/55H02K5/1732H02K7/09Y02E60/16
    • Upon operation, flywheel assemblies sand other such rotational mechanisms are released by mechanical backup bearings, which then normally remain disengaged until shutdown as the flywheel assembly is levitated by the axial magnetic field. However, either due to over heating of bearings, power failure or other stimuli, flywheels often suffer a phenomenon deemed as touchdown down from the levitation state. During this touchdown event, flywheels inherently lose rotational momentum, thus ceasing to generate and release power and often cause damage to components as well as casing. Enhancements developed herein, through the introduction of the instant secondary hybrid touchdown bearing system, allow flywheels and other such systems to retain rotational momentum and continue generation of energy. Further, the instant system negates damage to system components, as well as bearing wear.
    • 在操作时,飞轮组件沙其他这样的旋转机构由机械支撑轴承释放,然后机架支承轴承通常在飞轮组件被轴向磁场悬浮时保持分离直到停机。 然而,由于轴承过热,停电或其他刺激,飞轮经常遭受被认为从悬浮状态下降的现象。 在这次达阵事件中,飞轮固有地损失旋转动量,从而停止产生和释放动力,并经常导致部件和套管的损坏。 通过引入即时二次混合触地轴承系统,本文开发的增强功能允许飞轮和其他此类系统保持旋转动量并继续产生能量。 此外,即时系统会对系统组件以及轴承磨损造成损坏。
    • 2. 发明授权
    • Hybrid touchdown bearing system
    • 混合触地轴承系统
    • US07830055B2
    • 2010-11-09
    • US11904590
    • 2007-09-28
    • James ArseneauxJimpo Wang
    • James ArseneauxJimpo Wang
    • H02K7/09
    • H02K7/025F16C32/0442F16C39/02F16C39/066F16C2361/55H02K5/1732H02K7/09Y02E60/16
    • Upon operation, flywheel assemblies sand other such rotational mechanisms are released by mechanical backup bearings, which then normally remain disengaged until shutdown as the flywheel assembly is levitated by the axial magnetic field. However, either due to over heating of bearings, power failure or other stimuli, flywheels often suffer a phenomenon deemed as touchdown down from the levitation state. During this touchdown event, flywheels inherently lose rotational momentum, thus ceasing to generate and release power and often cause damage to components as well as casing. Enhancements developed herein, through the introduction of the instant secondary hybrid touchdown bearing system, allow flywheels and other such systems to retain rotational momentum and continue generation of energy. Further, the instant system negates damage to system components, as well as bearing wear.
    • 在操作时,飞轮组件沙其他这样的旋转机构由机械支撑轴承释放,然后机架支承轴承通常在飞轮组件被轴向磁场悬浮时保持分离直到停机。 然而,由于轴承过热,停电或其他刺激,飞轮经常遭受被认为从悬浮状态下降的现象。 在这次达阵事件中,飞轮固有地损失旋转动量,从而停止产生和释放动力,并经常导致部件和套管的损坏。 通过引入即时二次混合触地轴承系统,本文开发的增强功能允许飞轮和其他此类系统保持旋转动量并继续产生能量。 此外,即时系统会对系统组件以及轴承磨损造成损坏。
    • 3. 发明授权
    • Lift magnet mechanism for flywheel power storage systems
    • 飞轮蓄能系统提升磁铁机构
    • US07679247B2
    • 2010-03-16
    • US11820255
    • 2007-06-20
    • Jimpo Wang
    • Jimpo Wang
    • H02K7/09
    • H02K7/09F16C32/0459F16C2361/55H02K7/025Y02E60/16
    • Electric power is stored in a flywheel assembly, from a dc power buss, and supplied to the buss, through electronics associated with a motor/generator, its rotor integral with a flywheel supported by magnetic bearings. Upon operation, the flywheel assembly is released by mechanical backup bearings which then normally remain disengaged until shutdown as the flywheel assembly is levitated by the axial magnetic field. Enhancements developed herein smooth the flux density across discontinuities or segments present in permanent magnets due to presently limited capability for manufacture of large annular magnetic members. Herein, the introduction of a medium such as a steel cylindrical member to directly interface with the rotor as opposed to the segmented permanent magnet, greatly eradicates induced eddy current and heat on the rotor. In addition, exhibited is an annularly slotted rotor which allows for greater surface area for flux absorption.
    • 电力从直流电源总线存储在飞轮组件中,并通过与电动机/发电机相关联的电子器件供应到总线,其转子与由磁性轴承支撑的飞轮集成。 在操作时,飞轮组件由机械支撑轴承释放,然后通常由飞轮组件被轴向磁场悬浮而保持分离直到停机。 由于目前制造大型环形磁性构件的能力有限,本文开发的增强平滑了永久磁铁中存在的不连续部分或部分的磁通密度。 这里,与分段永久磁铁相反,引入诸如钢制圆柱形构件的介质直接与转子相接触,极大地消除了转子上的感应涡流和热。 此外,展示了一种环形开槽的转子,其允许更大的表面积用于磁通吸收。
    • 4. 发明申请
    • Lift magnet mechanism for flywheel power storage systems
    • 飞轮蓄能系统提升磁铁机构
    • US20080315696A1
    • 2008-12-25
    • US11820255
    • 2007-06-20
    • Jimpo Wang
    • Jimpo Wang
    • H02K7/02H02K7/09
    • H02K7/09F16C32/0459F16C2361/55H02K7/025Y02E60/16
    • Electric power is stored in a flywheel assembly, from a dc power buss, and supplied to the buss, through electronics associated with a motor/generator, its rotor integral with a flywheel supported by magnetic bearings. Upon operation, the flywheel assembly is released by mechanical backup bearings which then normally remain disengaged until shutdown as the flywheel assembly is levitated by the axial magnetic field. Enhancements developed herein smooth the flux density across discontinuities or segments present in permanent magnets due to presently limited capability for manufacture of large annular magnetic members. Herein, the introduction of a medium such as a steel cylindrical member to directly interface with the rotor as opposed to the segmented permanent magnet, greatly eradicates induced eddy current and heat on the rotor. In addition, exhibited is an annularly slotted rotor which allows for greater surface area for flux absorption.
    • 电力从直流电源总线存储在飞轮组件中,并通过与电动机/发电机相关联的电子器件供应到总线,其转子与由磁性轴承支撑的飞轮集成。 在操作时,飞轮组件由机械支撑轴承释放,然后通常由飞轮组件被轴向磁场悬浮而保持分离直到停机。 由于目前制造大型环形磁性构件的能力有限,本文开发的增强平滑了永久磁铁中存在的不连续部分或部分的磁通密度。 这里,与分段永久磁铁相反,引入诸如钢制圆柱形构件的介质直接与转子相接触,极大地消除了转子上的感应涡流和热。 此外,展示了一种环形开槽的转子,其允许更大的表面积用于磁通吸收。