Method and apparatus for reducing stress on shaft bearings
AssigneeGSI Lumonics Corporation
InventorDavid C. Brown
Life of this patent
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AssigneeGSI Lumonics Corporation
InventorDavid C. Brown
Estimating the term…
In a reciprocating rotor device such as a scanning galvanometer, a bearing assembly consisting of a Theological bearing coupler interposed between the rotor shaft and the bearing support structure or housing, where the Theological bearing coupler is relatively stiff during constant-velocity portions of rotor rotation, assuring adequate geometrical precision of the rotor within the rotor housing during the scanning phase. When loaded beyond a design load threshold by acceleration-induced moments causing lateral or asymmetrical force applied between the shaft and the bearing support structure during changes in rotor speed, becomes relatively compliant or resilient, absorbing a portion of the load at the expense of momentary axial misalignment of the rotor, then returning to original shape and realigning the rotor to it's correct precision axial position when the acceleration forces are abated.
A bearing assembly for a reciprocating rotor device comprising a Theological bearing coupler and a rotor shaft bearing, said assembly being interspersed between a rotor shaft and a bearing assembly support structure.
A bearing assembly for a galvanometer scanner comprising a rheological bearing coupler and a rotor shaft bearing, said assembly being interspersed between a rotor shaft and a bearing assembly support structure, said rheological bearing coupler configured to reduce axial bearing precision in respond to acceleration induced moment loads beyond a design threshold acceleration level.
A galvanometer scanner comprising upper and lower bearing assemblies, each said bearing assembly further comprising a rheological bearing coupler and a rotor shaft bearing, said being interspersed between a rotor shaft and a bearing assembly support structure, said Theological bearing coupler configured to reduce axial bearing precision in respond to acceleration induced moment loads beyond a design threshold acceleration level.
Dependencies are inferred from the claim text.