Thrust plate for reducing contact stress in a scroll compressor
A thrust plate for use in a scroll compressor is described. The thrust plate comprises a disk-shaped body defining a plane and having a first side and a second side, wherein the second side opposes the first side, at least one protrusion extending from the first side, and at least one recess located at the second side, wherein the at least one protrusion and the at least one recess overlap at least partially in a direction perpendicular to the plane. Further, a system is described, wherein the system comprises a thrust plate with at least one protrusion and an orbiting scroll plate with at least one recess, wherein the at least one protrusion and the at least one recess overlap. Also, a scroll compressor having either a corresponding thrust plate or a corresponding system is described.
1. A thrust plate for use in a scroll compressor, the thrust plate comprising:
a disk-shaped body defining a plane and having a first side and a second side, wherein the second side opposes the first side, wherein the disk-shaped body comprises a plurality of holes, which extend from a surface of the first side to a surface of the second side and which are configured to receive pins of an Oldham coupling;
at least one protrusion extending from the first side; and
at least one recess located at the second side;
wherein the at least one protrusion and the at least one recess overlap at least partially in a direction perpendicular to the plane, wherein the at least partial overlap is defined by the at least one protrusion overlapping entirely with the at least one recess.
2. The thrust plate according to claim 1 , wherein the disk-shaped body comprises an aperture, which extends from the surface of the first side to the surface of the second side and which is configured to receive a portion of a crankshaft and/or a portion of an orbiting scroll plate.
3. The thrust plate according to claim 1 , wherein the at least one recess is located at the surface of the second side.
4. The thrust plate according to claim 1 , wherein the at least one recess is located beneath the surface of the second side.
5. The thrust plate according to claim 1 , wherein at least a portion of the at least one recess does not overlap with the at least one protrusion.
6. The thrust plate according to claim 1 , wherein the first side comprises two or more protrusions and wherein each of the two or more protrusions overlaps entirely with at least a portion of the at least one recess.
7. The thrust plate according to claim 1 , wherein the at least one protrusion and the at least one recess form first and second patterns, respectively.
8. The thrust plate according to claim 7 , wherein the first pattern overlaps entirely with the second pattern, but wherein the at least one recess extends outwardly in every in-plane direction of the plane for a distance of 1 to 2 mm.
9. The thrust plate according to claim 1 , wherein the at least one protrusion has an annular shape and wherein the at least one recess has an annular shape.
10. The thrust plate according to claim 9 , wherein the first side comprises two or more protrusions, wherein the two or more protrusions form concentric rings, and/or wherein the second side comprises two or more recesses, wherein the two or more protrusions form concentric rings.
11. The thrust plate according to claim 1 , wherein each of the at least one protrusion is formed by a bar, which extend radially from a center of the disk-shaped body and wherein each of the at least one recess is formed by a groove, which extend radially from the center of the disk-shaped body, the number of the plurality of bars and the number of the plurality of grooves being the same.
12. A system comprising:
a thrust plate comprising:
a disk-shaped body defining a plane and having a first side and a second side, wherein the second side opposes the first side, wherein the disk-shaped body comprises a plurality of holes, which extend from a surface of the first side to a surface of the second side and which are configured to receive pins of an Oldham coupling, and
at least one protrusion extending from the first side; and
an orbiting scroll plate having a base plate with a frontside and a backside, wherein the orbiting scroll plate comprises at least one recess located at its backside;
wherein the backside of the orbiting scroll plate at least partially abuts at least a portion of the second side of the thrust plate, and
wherein the at least one protrusion and the at least one recess overlap at least partially in a direction perpendicular to the plane, wherein the at least partial overlap is defined by the at least one protrusion overlapping entirely with the at least one recess.
13. A scroll compressor comprising: either the thrust plate according to claim 1 and an orbiting scroll plate or the system of the orbiting scroll plate and the thrust plate according to claim 12 .