Aircraft actuator with no-back, load detent assembly
US-2017313409-A1 · Nov 2, 2017 · US
US9506541B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9506541-B2 |
| Application number | US-201113695732-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 10, 2011 |
| Priority date | May 5, 2010 |
| Publication date | Nov 29, 2016 |
| Grant date | Nov 29, 2016 |
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An eccentric bearing for an electrohydraulic piston-pump assembly of a vehicle brake system includes a shaft configured to be driven rotationally about its axis, a bearing ring eccentric relative to the shaft, and, in a gap between the bearing ring and shaft, rolling bodies with different diameters according to a differing width of the gap. When the shaft is rotationally driven, an eccentricity of the bearing ring circulates the shaft more slowly than the rotational speed of the shaft and drives a reciprocating movement of pump pistons which bear against the bearing ring. To ensure that the rolling bodies roll on and circulate the shaft, a radial elasticity loads the rolling bodies with prestress against the shaft and bearing ring. The prestress is caused by an undersize of the bearing ring or by an elastic ring on the shaft, on at least one rolling body or in the bearing ring.
Opening claim text (preview).
The invention claimed is: 1. An eccentric bearing for converting a rotary motion into a reciprocating motion comprising: a shaft configured to be driven rotationally; a bearing ring, which eccentrically surrounds the shaft; a plurality of rolling elements arranged around the shaft in a gap between the shaft and the bearing ring, wherein: at least one rolling element of the plurality of rolling elements includes at least one rolling element elastic ring arranged on the at lea…
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