Centrifugal compressor and turbocharger

Patent metadata

Field	Value
Publication number	US-11408439-B2
Application number	US-201716482046-A
Country	US
Kind code	B2
Filing date	Mar 28, 2017
Priority date	Mar 28, 2017
Publication date	Aug 9, 2022
Grant date	Aug 9, 2022

Abstract

A centrifugal compressor 10 includes a diffuser 13 that comprises: a shroud wall surface 131 that extends in the radial direction of a rotating shaft 3; and a hub wall surface 132 that extends in the radial direction and opposes the shroud wall surface 131 on the downstream side of a flow in the axial direction of the rotating shaft 3, the hub wall surface having a gap between itself and the shroud wall surface 131, and with that gap, forming an annular diffuser flow path 130 through which a fluid flows. A hub-side convex portion 132b is formed over the entire periphery of the hub wall surface 132, the hub-side convex portion 132b protruding toward the shroud wall surface 131 side relative to a straight line L1 that connects a starting end 132s on an inlet 130a side of the diffuser flow path 130 and a terminating end 132e on an outlet 130b side of the diffuser flow path 130.

First claim

The invention claimed is:

1. A centrifugal compressor comprising:
an impeller boosting a fluid by rotation about an axis of a rotating shaft; and.
a diffuser converting a dynamic pressure of the fluid boosted by the impeller into a static pressure, wherein
the diffuser has an inlet, an outlet, a shroud wall surface extending in a radial direction of the centrifugal compressor and a hub wall surface extending in the radial direction and opposing the shroud wall surface on a downstream side of a flow in an axial direction of the centrifugal compressor, the diffuser having a gap between the hub wall surface and the shroud wall surface and forming an annular diffuser flow path with the gap, the fluid flowing through the diffuser flow path,
a hub-side convex portion is formed over an entire periphery of the hub wall surface, the hub-side convex portion protruding toward the shroud wall surface side relative to a straight line connecting a starting end on an inlet side of the diffuser flow path and a terminating end on an outlet side of the diffuser flow path,
the hub-side convex portion is formed so as to have a size at which an annular area as a product of a circumferential length and a width of the diffuser flow path at any radial position is greater than an annular area as a product of a circumferential length and a width of the diffuser flow path at the inlet,
the shroud wall surface has a shroud-side concave portion provided so as to oppose the hub-side convex portion and be concave to a side opposite to the hub wall surface, and
a vertex of the hub-side convex portion is provided in a range inward in the radial direction from a central portion of the hub-side convex portion in the radial direction.

2. The centrifugal compressor according to claim 1 , wherein the vertex of the hub-side convex portion is formed at a radial position 1.05 to 1.4 times a radius from the rotating axis at the inlet of the diffuser flow path.

3. The centrifugal compressor according to claim 2 , wherein the hub-side convex portion is provided inside a position in the radial direction, the position having a radius of 0.9 or less times a radius from the rotating axis at the outlet of the diffuser flow path.

4. The centrifugal compressor according to claim 2 , wherein the hub-side convex portion has a distance from the straight line to the vertex in the axial direction ranging from 0.1 times to 0.3 times a width of the diffuser flow path at the outlet.

5. The centrifugal compressor according to claim 1 , wherein the hub-side convex portion is provided inside a position in the radial direction, the position having a radius of 0.9 or less times a radius from the rotating axis at the outlet of the diffuser flow path.

6. The centrifugal compressor according to claim 5 , wherein the hub-side convex portion has a distance from the straight line to the vertex in the axial direction ranging from 0.1 times to 0.3 times a width of the diffuser flow path at the outlet.

7. The centrifugal compressor according to claim 1 , wherein the hub-side convex portion has a distance from the straight line to the vertex in the axial direction ranging from 0.1 times to 0.3 times a width of the diffuser flow path at the outlet.

8. The centrifugal compressor according to claim 1 , wherein the shroud-side concave portion is formed so as to have a size, as a maximum, at which a width of the diffuser flow path becomes constant in the radial direction between the hub-side convex portion and the shroud-side concave portion.

9. The centrifugal compressor according to claim 1 wherein
the impeller has an impeller hub rotating integrally with the rotating shaft and a blade attached to the impeller hub,
the impeller hub includes a linear portion extending in a direction orthogonal to the rotating shaft to an impeller outlet, and
the hub wall surface forming the diffuser flow path extends obliquely toward the downstream side in the axial direction from the starting end toward the terminating end.

10. The centrifugal compressor according to claim 1 , wherein the shroud wall surface has an asymptotic portion that is asymptotic toward the hub wall surface side radially outward from the inlet.

11. A turbocharger comprising:
the centrifugal compressor according to claim 1 ; and
a turbine that is coaxially connected to the centrifugal compressor via the rotating shaft.

12. A centrifugal compressor comprising:
an impeller boosting a fluid by rotation about an axis of a rotating shaft; and
a diffuser converting a dynamic pressure of the fluid boosted by the impeller into a static pressure, wherein
the diffuser has an inlet, an outlet, a shroud wall surface extending in a radial direction of the centrifugal compressor and a hub wall surface extending in the radial direction and opposing the shroud wall surface on a downstream side of a flow in an axial direction of the centrifugal compressor, the diffuser having a gap between the hub wall surface and the shroud wall surface and forming an annular diffuser flow path with the gap, the fluid flowing through the diffuser flow path,
a hub-side convex portion is formed over an entire periphery of the hub wall surface, the hub-side convex portion protruding toward the shroud wall surface side relative to a straight line connecting a starting end on an inlet side of the diffuser flow path and a terminating end on an outlet side of the diffuser flow path,
the hub-side convex portion is formed so as to have a size at which an annular area as a product of a circumferential length and a width of the diffuser flow path at any radial position is greater than an annular area as a product of a circumferential length and a width of the diffuser flow path at the inlet,
the impeller has an impeller hub rotating integrally with the rotating shaft and a blade attached to the impeller hub,
the impeller hub includes an inclined portion extending obliquely toward the downstream side in the axial direction toward the hub wall surface forming the diffuser flow path, and
the hub wall surface forming the diffuser flow path has a hub-side concave portion that is concave toward a side opposite to the shroud wall surface and has an inclination angle conforming to an inclination angle of the inclined portion of the impeller hub radially inside the hub-side convex portion.

13. The centrifugal compressor according to claim 12 , wherein thea vertex of the hub-side convex portion is provided in a range inward in the radial direction from a central portion of the hub-side convex portion in the radial direction.

14. The centrifugal compressor according to claim 12 , wherein a vertex of the hub-side convex portion is formed at a radial position 1.05 to 1.4 times a radius from the rotating axis at the inlet of the diffuser flow path.

15. The centrifugal compressor according to claim 12 , wherein the hub-side convex portion is provided inside a position in the radial direction, the position having a radius of 0.9 or less times a radius from the rotating axis at the outlet of the diffuser flow path.

16. The centrifugal compressor according to claim 12 , wherein the hub-side convex portion has a distance from the straight line to a vertex in the axial direction ranging from 0.1 times to 0.3 times a width of the diffuser flow path at the outlet.

17. The centrifugal compressor according to claim 12 , wherein the shroud wall surface has an asymptotic portion that is asymptotic toward the hub wall surface side radially outward from the inlet.

18. A turbocharger comprising:
the centrifugal compressor according t

Assignees

• Mitsubishi Heavy Ind Engine & Turbocharger Ltd

Inventors

• Higashimori Hirotaka
• Kanzaka Tadashi

Classifications

• F04D29/284

  for compressors · CPC title

• F05D2250/52

  Outlet · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F04D29/441 Primary

  especially adapted for elastic fluid pumps · CPC title

• F04D17/10

  for compressing or evacuating · CPC title