Centrifugal compressor

Patent metadata

Field	Value
Publication number	US-11209015-B2
Application number	US-201716305478-A
Country	US
Kind code	B2
Filing date	Jun 21, 2017
Priority date	Jul 1, 2016
Publication date	Dec 28, 2021
Grant date	Dec 28, 2021

Abstract

In a compressor, a scroll includes a winding end portion, a discharge potion connected to the winding end portion, a winding start portion connected to the discharge potion, and a flow passage inner surface and when a projection plane is assumed for the scroll in a case in which a viewing point is located on a rotation axis of a compressor impeller and on a fluid suction side, and the flow passage inner surface on the projection plane includes a curved protrusion portion protruding outward in relation to the reference line.

First claim

The invention claimed is:

1. A centrifugal compressor comprising:
an impeller; and
a scroll which is disposed around the impeller and includes a flow passage formed in a rotation direction of the impeller,
wherein the flow passage includes a spiral scroll flow passage along the rotation direction and a discharge flow passage connected to the scroll flow passage in a tangential direction of the scroll flow passage,
wherein the scroll includes a discharge portion in which the discharge flow passage is formed, a winding start portion connected to a side portion of the discharge portion as a start point of the scroll flow passage along the rotation direction, a winding end portion connected to the discharge portion as an end point of the scroll flow passage along the rotation direction, and a flow passage inner surface facing the discharge flow passage,
wherein when a projection plane in which the scroll is projected onto a plane orthogonal to the rotational axis of the impeller is presumed, the flow passage inner surface on the projection plane includes a reference start point that is a position closest to the winding end portion at the winding start portion and a reference end point that is a position closest to the rotational axis at the winding end portion, and
wherein when a reference straight line connecting the reference start point and the reference end point is presumed, the flow passage inner surface of the projection plane includes a curved protrusion portion protruding toward the outside corresponding to a centrifugal direction in relation to the reference straight line.

2. The centrifugal compressor according to claim 1 ,
wherein the protrusion portion and an upstream inner surface on an opposite side of the rotation direction in relation to the protrusion portion, in the flow passage inner surface of the scroll, have a continuous inclination in the tangential direction.

3. The centrifugal compressor according to claim 1 ,
wherein the protrusion portion and a downstream inner surface on the rotation direction side in relation to the protrusion portion in the flow passage inner surface of the scroll have a continuous inclination in the tangential direction.

4. The centrifugal compressor according to claim 2 ,
wherein the protrusion portion and a downstream inner surface on the rotation direction side in relation to the protrusion portion in the flow passage inner surface of the scroll have a continuous inclination in the tangential direction.

5. The centrifugal compressor according to claim 1 ,
wherein a most protruding position of the protrusion portion from the reference straight line on the projection plane is closer to the reference start point than the reference end point.

6. The centrifugal compressor according to claim 2 ,
wherein a most protruding position of the protrusion portion from the reference straight line on the projection plane is closer to the reference start point than the reference end point.

7. The centrifugal compressor according to claim 3 ,
wherein a most protruding position of the protrusion portion from the reference straight line on the projection plane is closer to the reference start point than the reference end point.

8. The centrifugal compressor according to claim 4 ,
wherein a most protruding position of the protrusion portion from the reference straight line on the projection plane is closer to the reference start point than the reference end point.

9. A centrifugal compressor comprising:
an impeller; and
a scroll which is disposed around the impeller and includes a flow passage formed in a rotation direction of the impeller,
wherein the flow passage includes a spiral scroll flow passage along the rotation direction and a discharge flow passage connected to the scroll flow passage in a tangential direction of the scroll flow passage,
wherein the scroll includes a discharge portion in which the discharge flow passage is formed, a winding start portion connected to a side portion of the discharge portion as a start point of the scroll flow passage along the rotation direction, a winding end portion connected to the discharge portion as an end point of the scroll flow passage along the rotation direction, and a flow passage inner surface facing the discharge flow passage,
wherein when a projection plane in which the scroll is projected onto a plane orthogonal to the rotational axis of the impeller is presumed, the flow passage inner surface on the projection plane includes a reference start point that is a position closest to the winding end portion at the winding start portion and a reference end point that is a position on the winding end portion and has a rotation angle of −60° with respect to the reference start point, and
wherein when a reference straight line connecting the reference start point and the reference end point on the projection plane is presumed, the flow passage inner surface on the projection plane includes a curved protrusion portion which protrudes toward the outside corresponding to a centrifugal direction in relation to the reference straight line.

Assignees

• Ihi Corp

Inventors

• Ueno Takahiro

Classifications

• F02B39/00

  Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00 · CPC title

• F04D25/024 Primary

  the driving means being assisted by a power recovery turbine · CPC title

• F04D29/441 Primary

  especially adapted for elastic fluid pumps · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F04D29/4206

  especially adapted for elastic fluid pumps · CPC title