Compressor coupling component for coupling a drive shaft and a movable spiral in a scroll compressor
Abstract
A compressor coupling component includes a planar main body with a first, front side and a second, rear side opposite the first side, a cylindrical coupling neck, wherein the cylinder axis of the cylindrical coupling neck runs perpendicularly to the plane of the planar main body, and the cylindrical coupling neck protrudes from the planar main body in the axial direction, a counterweight, is integrally formed on an outer region of the planar main body, and protrudes beyond the planar main body in the axial direction on the rear side of the planar main body, wherein the planar main body has opposing outer edge regions which extend as far as ends of the counterweight which oppose each other in the arc direction of the counterweight, and run linearly in the manner of increasingly spaced-apart V-legs.
Claims
exact text as granted — not AI-modified1 - 11 . (canceled)
12 . A compressor coupling component for coupling a drive shaft and a movable spiral in a scroll compressor, the compressor coupling component comprising:
a planar main body with a front side and a rear side opposite the front side; a cylindrical coupling neck, which is integrally formed on or fastened to the planar main body or inserted into the planar main body, wherein a cylinder axis of the cylindrical coupling neck runs perpendicularly to a plane of the planar main body, and the cylindrical coupling neck protrudes from the planar main body in an axial direction, in relation to the cylinder axis of the cylindrical coupling neck, on the front side of the planar main body; and a counterweight, which is at least partially formed in the shape of a hollow cylindrical segment, has an arcuate outer contour, is integrally formed on an outer region of the planar main body which only partially encloses the cylindrical coupling neck and a neck-surrounding region which runs coaxially with the cylinder axis and completely encloses the cylindrical coupling neck, and protrudes beyond the planar main body in the axial direction on the rear side of the planar main body, wherein the planar main body has opposing outer edge regions which, starting from an arcuate base edge region of the planar main body partially enclosing the neck-surrounding region, extend as far as ends of the counterweight which oppose each other in an arc direction of the counterweight, and in an outer contour of the planar main body run linearly in a manner of increasingly spaced-apart V-legs.
13 . The compressor coupling component according to claim 12 , wherein a supporting element or multiple supporting elements is/are additionally formed in regions of the planar main body which are adjacent to the outer edge regions running in the manner of the V-legs in order to reinforce the compressor coupling component.
14 . The compressor coupling component according to claim 13 , wherein there are multiple supporting elements and the supporting elements are reinforcing ribs of a rib structure which protrudes from the planar main body in the axial direction on the rear side of the planar main body.
15 . The compressor coupling component according to claim 14 , wherein the rib structure with the reinforcing ribs as supporting elements extends as far as the counterweight.
16 . The compressor coupling component according to claim 14 , wherein the rib structure contains two reinforcing ribs as supporting elements, which are each adjacent to one of the opposing outer edge regions.
17 . The compressor coupling component according to claim 16 , wherein the two reinforcing ribs as supporting elements each extend as far as one of the ends of the counterweight which oppose each other in the arc direction.
18 . The compressor coupling component according to claim 14 , wherein the reinforcing ribs as supporting elements protrude in the axial direction on the rear side of the planar main body exactly as far as the counterweight protrudes beyond the planar main body on the rear side.
19 . The compressor coupling component according to claim 12 , wherein the compressor coupling component is produced by a metal powder forming process.
20 . The compressor coupling component according to claim 19 , wherein the compressor coupling component is produced by a steel powder pressing method.
21 . The compressor coupling component according to claim 12 , wherein the cylindrical coupling neck has a receiving bore oriented eccentrically to the cylinder axis.
22 . The scroll compressor for a gaseous fluid, comprising:
a compressor housing and two interleaving spirals inside the compressor housing, wherein a first one of the spirals is stationary, and a second one of the spirals is the movable spiral and is movable eccentrically on a circular trajectory, and a volume of compression chambers formed between the first one of the spirals and the second one of the spirals can be changed cyclically by a movement of the second one of the spirals, an eccentric drive, by means of which the second one of the spirals is movable on the circular trajectory and which comprises the drive shaft which is rotatable and the compressor coupling component according to claim 12 which is rotatable with the drive shaft, wherein the second one of the spirals is connected eccentrically to the drive shaft via the compressor coupling component.Join the waitlist — get patent alerts
Track US2026016008A1 — get alerts on status changes and closely related new filings.
We store only your email — no account needed. See our privacy policy.