Impeller and rotary machine

Patent metadata

Field	Value
Publication number	US-9404506-B2
Application number	US-201013262929-A
Country	US
Kind code	B2
Filing date	Feb 18, 2010
Priority date	Jul 13, 2009
Publication date	Aug 2, 2016
Grant date	Aug 2, 2016

Abstract

An impeller of a rotary machine, in which the direction of flow changes from an axial direction to a radial direction as it goes from the inside in the radial direction of a fluid flow passage to the outside in the radial direction thereof, includes a hub surface constituting at least a portion of the fluid flow passage. The impeller also includes a blade surface constituting at least a portion of the fluid flow passage, and a bulge that bulges toward the inside of the fluid flow passage at a corner where a pressure surface, which configures the blade surface, comes in contact with the hub surface in the vicinity of an inlet of the fluid flow passage.

First claim

The invention claimed is:

1. An impeller of a compressor, in which a direction of flow changes from an axial direction to a radial direction from an inlet in the radial direction of a fluid flow passage to an outlet in the radial direction thereof, the impeller comprising:
a hub surface constituting at least a portion of the fluid flow passage;
a blade surface constituting at least a portion of the fluid flow passage;
a bulge that is formed at a corner where a pressure surface, which configures the blade surface, comes in contact with the hub surface in the vicinity of the inlet of the fluid flow passage; and
a second bulge that bulges toward an inside of the fluid flow passage at a corner where a suction surface of a blade comes in contact with the hub surface in the vicinity of the inlet of the fluid flow passage, wherein
the bulge has a curved surface smoothly protruding from a leading edge of the blade toward the inside of the fluid flow passage, the bulge having a width and a height that gradually decrease in a downstream direction of the fluid flow passage, and
the bulge has a curved surface smoothly protruding from the corner where the pressure surface comes in contact with the hub surface toward the inside of the fluid flow passage, the width of the bulge gradually decreasing as extending outward in the radial direction of the fluid flow passage, and the height of the bulge gradually decreasing in the axial direction.

2. A compressor comprising the impeller according to claim 1 .

3. The impeller according to claim 1 , wherein the leading edge of the blade has a rounded surface.

4. The impeller according to claim 3 , wherein the bulge smoothly bulges along the flow direction from an apex of the rounded surface of the leading edge of the blade towards downstream.

5. The impeller according to claim 3 , wherein the rounded surface is a convex surface.

6. The impeller according to claim 5 , wherein the bulge smoothly bulges along the flow direction from an apex of the convex surface of the leading edge of the blade towards downstream.

7. The impeller according to claim 1 , wherein the bulge smoothly bulges along a portion of the leading edge of the blade.

Assignees

• Masutani Jo
• Mitsubishi Heavy Ind Ltd

Inventors

• Masutani Jo

Classifications

• F04D29/286

  multi-stage rotors · CPC title

• F04D29/30 Primary

  Vanes · CPC title

• F04D29/284

  for compressors · CPC title