Hydrodynamic bearing applied on a contact interface of a fluid compressor based on a spiral type mechanism
View Patent ↗The present disclosure refers to a partial texturization applied on a contact interface of a scroll fluid compressor. The scroll fluid compressor may have an orbiting whorl, a non-orbiting whorl, and a block frame which holds the orbiting whorl in contact with the non-orbiting whorl. The partial texturization can be applied on the lower surface of the orbiting whorl, the upper surface of the block frame, or both, and can include at least two first regions separated by second regions. The first regions have surfaces including a plurality of micro-cavities and the second regions have substantially smooth surfaces.
1. A fluid compressor comprising:
a hermetic housing;
an electric motor;
a block frame;
an orbiting whorl; and
a non-orbiting whorl;
wherein:
a lower surface of the orbiting whorl is in contact with an upper surface of the block frame;
at least one of the lower surface of the orbiting whorl and the upper surface of the block frame has a plurality of first regions and a plurality of second regions, and each two adjacent first regions are separated by at least one of the plurality of second regions;
at least one of the plurality of the first regions includes a plurality of micro-cavities;
at least one of the plurality of second regions has a smooth surface;
each of the plurality of micro-cavities:
has a depth in the range of 1 μm to 30 μm;
has a surface area in the range of 5 μm 2 to 100 μm 2 ;
has a border radius in the range of 0.01 μm to 30 μm; and
is separated from an adjacent micro-cavity by a distance in the range of 1 μm to 100 μm.
2. The fluid compressor of claim 1 , wherein a surface area of each of the plurality of micro-cavities forms a circular profile.
3. The fluid compressor of claim 1 , wherein a surface area of each of the plurality of micro-cavities forms an elliptical profile.
4. The fluid compressor of claim 1 , wherein a surface area of each of the plurality of micro-cavities forms a rectangular profile.
5. The fluid compressor of claim 1 , wherein the plurality of first regions and the plurality of second regions are defined on the lower surface of the orbiting whorl.
6. The fluid compressor of claim 1 , wherein the plurality of first regions and the plurality of second regions are defined on the upper surface of the block frame.
7. The fluid compressor of claim 1 , wherein the plurality of first regions and the plurality of second regions are defined on the lower surface of the orbiting whorl and the upper surface of the block frame.
8. The fluid compressor of claim 1 , wherein the sum of the surface area of the plurality of first regions constitutes a range between 30% to 80% of the surface area of at least one of the lower surface of the orbiting whorl and the upper surface of the block frame.
9. The fluid compressor of claim 1 , wherein at least one radial channel is located in at least one of the plurality of second regions.
10. The fluid compressor of claim 1 , wherein the plurality of micro-cavities are configured to store deposits of abrasive particles.