Centrifugal compressor impeller

Patent metadata

Field	Value
Publication number	US-9494160-B2
Application number	US-201113877678-A
Country	US
Kind code	B2
Filing date	Dec 6, 2011
Priority date	Dec 27, 2010
Publication date	Nov 15, 2016
Grant date	Nov 15, 2016

Abstract

Provided is a centrifugal compressor impeller which is characterized in that leading edges 7 a on a shroud side of splitter blades 7 are offset from a circumferentially equidistant position between full blades 5 R and 5 F toward a suction side Sb of the full blade 5 F, and trailing edges 7 b on a hub side of the splitter blades 7 are offset from a circumferentially equidistant position between the full blades toward the suction side Sb of the full blade 5 F, so that a tip leakage vortex W flowing from a tip clearance between the tips of the full blades 5 F and the shroud toward the leading edges 7 a of the splitter blades 7 flows over the leading edges 7 a of the splitter blades 7.

First claim

The invention claimed is:

1. A centrifugal compressor impeller, comprising:
a plurality of full blades that stand equally spaced in a circumferential direction and extend from a fluid inlet part to a fluid outlet part on a surface of a hub; and
splitter blades each of which is disposed in a flow passage formed between two of the full blades arranged adjacent to each other so as to extend from a downstream point on a downstream side of the fluid inlet part in the flow passage to the fluid outlet part,
wherein the centrifugal compressor includes a tip clearance between tips of the full blades and a shroud, and a leading edge portion on a shroud side of each of the splitter blades is offset from a circumferentially equidistant position between said two of the full blades at the downstream point toward a suction side of a front side full blade which is disposed on a downstream side in a rotational direction of the centrifugal compressor impeller among said two of the full blades, while a trailing edge portion on a hub side of each of the splitter blades is offset from a circumferentially equidistant position between said two of the full blades at the fluid outlet part toward the suction side of the front side full blade, so that a tip leakage vortex flowing from the tip clearance toward the leading edge portion of each of the splitter blades flows over the leading edge portion of said each of the splitter blades, or so that the leading edge portion of each of the splitter blades conforms to a direction of the tip leakage vortex, and
wherein a trailing edge portion on the shroud side of each of the splitter blades is offset from the circumferentially equidistant position between said two of the full blades at the fluid outlet part toward a pressure side of a rear side full blade which is disposed on an upstream side in the rotational direction of the centrifugal compressor impeller among said two of the full blades.

2. A centrifugal compressor impeller, comprising:
a plurality of full blades that stand equally spaced in a circumferential direction and extend from a fluid inlet part to a fluid outlet part on a surface of a hub; and
splitter blades each of which is disposed in a flow passage formed between two of the full blades arranged adjacent to each other so as to extend from a downstream point on a downstream side of the fluid inlet part in the flow passage to the fluid outlet part,
wherein the centrifugal compressor includes a tip clearance between tips of the full blades and a shroud, and a leading edge portion on a shroud side of each of the splitter blades is offset from a circumferentially equidistant position between said two of the full blades at the downstream point toward a suction side of a front side full blade which is disposed on a downstream side in a rotational direction of the centrifugal compressor impeller among said two of the full blades, while a trailing edge portion on a hub side of each of the splitter blades is offset from a circumferentially equidistant position between said two of the full blades at the fluid outlet part toward the suction side of the front side full blade, so that a tip leakage vortex flowing from the tip clearance toward the leading edge portion of each of the splitter blades flows over the leading edge portion of said each of the splitter blades, or so that the leading edge portion of each of the splitter blades conforms to a direction of the tip leakage vortex, and
wherein a trailing edge portion on the shroud side of each of the splitter blades is offset from the circumferentially equidistant position between said two of the full blades at the fluid outlet part toward a pressure side of a rear side full blade which is disposed on an upstream side in the rotational direction of the centrifugal compressor impeller among said two of the full blades, and
wherein ratios of cross-sectional areas at the leading edges and trailing edges of the splitter blades in respective passages on each side of each of the splitter blades at positions with a minimum distance from the splitter blade to a pressure side of the rear side full blade or the suction side of the front side full blade are made uniform.

3. A centrifugal compressor impeller, comprising:
a plurality of full blades that stand equally spaced in a circumferential direction and extend from a fluid inlet part to a fluid outlet part on a surface of a hub; and
splitter blades each of which is disposed in a flow passage formed between two of the full blades arranged adjacent to each other so as to extend from a downstream point on a downstream side of the fluid inlet part in the flow passage to the fluid outlet part,
wherein the centrifugal compressor includes a tip clearance between tips of the full blades and a shroud, and a leading edge portion on a shroud side of each of the splitter blades is offset from a circumferentially equidistant position between said two of the full blades at the downstream point toward a suction side of a front side full blade which is disposed on a downstream side in a rotational direction of the centrifugal compressor impeller among said two of the full blades, while a trailing edge portion on a hub side of each of the splitter blades is offset from a circumferentially equidistant position between said two of the full blades at the fluid outlet part toward the suction side of the front side full blade, so that a tip leakage vortex flowing from the tip clearance toward the leading edge portion of each of the splitter blades flows over the leading edge portion of said each of the splitter blades, or so that the leading edge portion of each of the splitter blades conforms to a direction of the tip leakage vortex, and
wherein the leading edge portion on the shroud side of each of the splitter blades is offset from the circumferentially equidistant position between said two of the full blades at the downstream point toward the suction side of the front side full blade such that the leading edge portion is positioned at the circumferentially equidistant position between said two of the full blades at the downstream point up to about 70% of a total height of the splitter blades and portions above about 70% of the total height of the splitter blades are inclined from a point corresponding to about 70% of the total height toward distal ends thereof.

4. The centrifugal compressor impeller according to claim 3 , wherein ratios of cross-sectional areas at the leading edges and trailing edges of the splitter blades in respective passages on each side of each of the splitter blades at positions with a minimum distance from the splitter blade to a pressure side of the rear side full blade or the suction side of the front side full blade are made uniform.

Assignees

• Tomita Isao
• Hoshi Toru
• Kanzaka Tadashi
• Mitsubishi Heavy Ind Ltd

Inventors

• Tomita Isao
• Hoshi Toru
• Kanzaka Tadashi

Classifications

• F04D17/10 Primary

  for compressing or evacuating · CPC title

• F04D29/30 Primary

  Vanes · CPC title

• F04D29/284

  for compressors · CPC title