Multistage radial compressor baffle

Patent metadata

Field	Value
Publication number	US-9856886-B2
Application number	US-201514592120-A
Country	US
Kind code	B2
Filing date	Jan 8, 2015
Priority date	Jan 8, 2015
Publication date	Jan 2, 2018
Grant date	Jan 2, 2018

Abstract

An assembly can include a first radial compressor wheel that has a rotational axis and that includes a hub surface that includes an annular ridge disposed at a radius measured from the rotational axis; a second radial compressor wheel that includes a hub surface; and an annular baffle disposed at least in part between the hub surfaces where the annular baffle includes an outer surface and an inner edge that defines an opening having a central axis where the outer surface includes a surface portion to one side of the inner edge that faces the hub surface of the first radial compressor wheel, where the surface portion includes an annular channel over a radial width measured from the central axis and where the radial width spans the radius of the annular ridge.

First claim

What is claimed is:

1. An annular baffle for a two stage radial compressor assembly with first and second radial compressor wheels assembled in a hub-to-hub orientation with respect to corresponding first and second exducer portions, the annular baffle comprising:
an outer edge;
a substantially parabolic portion that comprises an inner edge that defines an opening having a central axis and opposing surfaces that extend from the inner edge wherein one of the opposing surfaces comprises an annular notch adjacent to the inner edge wherein the annular notch is defined in part by a radial notch width; and
between the inner edge and the outer edge, a first diffuser surface that forms a portion of a first diffuser section that receives gas that exits the first exducer portion and an opposing second diffuser surface that forms a portion of a second diffuser section that receives gas that exits the second exducer portion.

2. The annular baffle of claim 1 wherein one of the opposing surfaces comprises a first substantially semi-parabolic shape and wherein the other of the opposing surfaces comprises a second substantially semi-parabolic shape wherein a radial offset between ends of the opposing surfaces defines the radial notch width.

3. The annular baffle of claim 1 wherein the annular notch comprises an annular axial face.

4. The annular baffle of claim 1 wherein one of the opposing surfaces comprises an annular channel located between the inner edge and the outer edge.

5. The annular baffle of claim 4 wherein the annular channel is located between the annular notch and the outer edge.

6. The annular baffle of claim 4 wherein the one of the opposing surfaces comprises at least two annular channels located between the inner edge and the outer edge.

7. The annular baffle of claim 1 wherein one of the opposing surfaces comprises a low pressure surface portion to one side of the inner edge for facing a first hub portion of the first radial compressor wheel and the other of the opposing surfaces comprises a high pressure surface portion to the other side of the inner edge for facing a second hub portion of the second radial compressor wheel.

8. The annular baffle of claim 7 wherein the low pressure surface portion comprises the annular notch adjacent to the inner edge.

9. The annular baffle of claim 8 wherein the low pressure surface portion comprises at least one annular channel.

10. The annular baffle of claim 9 wherein the low pressure surface portion comprises at least two annular channels.

11. The annular baffle of claim 10 comprising an annular wall disposed between two of the at least two annular channels.

12. The annular baffle of claim 11 wherein the annular wall comprises a wall width that is less than a minimum annular channel width of the two of the at least two annular channels.

13. The annular baffle of claim 1 wherein the annular notch is defined at least in part by a surface that comprises a radius of curvature defined by a portion of a torus.

14. An assembly comprising:
a first radial compressor wheel that has a rotational axis and that comprises a first hub surface that comprises an annular ridge disposed at a radius measured from the rotational axis;
a second radial compressor wheel that comprises a second hub surface; and
an annular baffle disposed at least in part between the first and second hub surfaces wherein the annular baffle comprises an outer surface and an inner edge that defines an opening having a central axis wherein the outer surface comprises a surface portion to one side of the inner edge that faces the first hub surface, wherein the surface portion comprises an annular channel that comprises a radial width, as measured with respect to the central axis, and wherein the radial width of the annular channel of the annular baffle spans the radius of the annular ridge of the first hub surface of the first radial compressor wheel.

15. The assembly of claim 14 wherein the annular baffle comprises two annular channels and wherein the first hub surface comprises two annular ridges.

16. The assembly of claim 14 wherein the outer surface comprises a surface portion to the other side of the inner edge that faces the second hub surface wherein the surface portion comprises a continuous semi-parabolic shape.

17. The assembly of claim 16 wherein the second hub surface of the second radial compressor wheel comprises a continuous semi-parabolic shape.

18. The assembly of claim 14 wherein the annular baffle comprises an annular notch adjacent to the inner edge.

19. The assembly of claim 18 wherein the annular notch comprises an axial annular face that faces an axial face of the first radial compressor wheel.

20. The assembly of claim 14 wherein the first radial compressor wheel comprises an axial face defined by a first diameter and wherein the second radial compressor wheel comprises an axial face defined by a second diameter wherein the first diameter exceeds the second diameter.

Assignees

• Honeywell Int Inc

Inventors

• Kares Vaclav
• Houst Vit
• Lednicky Ondrej
• Mokos Michal
• Nejedly Milan
• Oseljsek Zbynek
• Turecek Daniel

Classifications

• F04D29/2266

  for sealing or thrust balance (F04D29/04 and F04D29/16 take precedence) · CPC title

• F04D17/122

  the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors · CPC title

• F04D29/083 Primary

  especially adapted for elastic fluid pumps · CPC title

• F04D29/284

  for compressors · CPC title

• F04D17/12

  Multi-stage pumps · CPC title