Impeller for centrifugal compressor

Patent metadata

Field	Value
Publication number	US-9683445-B2
Application number	US-201113813351-A
Country	US
Kind code	B2
Filing date	Dec 5, 2011
Priority date	Dec 13, 2010
Publication date	Jun 20, 2017
Grant date	Jun 20, 2017

Abstract

An impeller for a centrifugal compressor is characterized in that a shroud side of a front edge 7 a of a splitter blade 7 is disposed so as to be displaced toward a negative-pressure surface Sb of a full blade 5 F from a position equidistant from the full blades 5 R and 5 F in a circumferential direction such that a blade-end leakage vortex generated during a high flow rate which occurs from a blade-end clearance between the tip of the full blade 5 F and a shroud toward the portion of the front edge 7 a of the splitter blade 7 gets over the front edge 7 a of the splitter blade 7.

First claim

The invention claimed is:

1. An impeller for a centrifugal compressor, comprising:
a plurality of full blades, each full blade extending from an entrance portion to an exit portion of a fluid path on a hub surface;
a splitter blade provided from a midpoint in the flow path, formed between the full blades provided adjacent to each other, to the exit portion, the splitter blade having a front edge and a rear edge in a flow direction of the fluid, the front edge being positioned on an upstream side than the rear edge in the flow direction of the fluid, the splitter blade having a hub side and a shroud side in a direction of height of the splitter blade from a hub surface;
the shroud side of the front edge of the splitter blade being displaced toward a negative-pressure surface of the full blade from a position equidistant from the adjacent full blades in a circumferential direction of the impeller such that a blade-end leakage vortex generated during a high flow rate, which occurs from a blade-end clearance formed between a tip of the full blade and a shroud toward the front edge of the splitter blade, gets over the front edge of the splitter blade or such that the shroud side of the front edge of the splitter blade matches a direction of the blade-end leakage vortex, and
the hub side of the rear edge of the splitter blade being displaced toward a positive-pressure surface of the full blade from the position equidistant from the full blades in the circumferential direction.

2. The impeller for a centrifugal compressor according to claim 1 , wherein the hub side of the front edge of the splitter blade is displaced toward a positive-pressure surface of the full blade from the position equidistant from the full blades in the circumferential direction.

3. The impeller for a centrifugal compressor according to claim 2 , wherein the shroud side of the rear edge of the splitter blade is displaced toward the negative-pressure surface of the full blade from the position equidistant from the full blades in the circumferential direction.

4. The impeller for a centrifugal compressor according to claim 1 , wherein an inclination angle of the front edge of the splitter blade opposing the flow direction of the fluid is increased to be larger than an inclination angle of the full blade at a height identical to that of the front edge of the splitter blade.

5. An impeller for a centrifugal compressor, comprising:
a plurality of full blades, each full blade extending from an entrance portion to an exit portion of a fluid path on a hub surface;
a splitter blade provided from a midpoint in the flow path, formed between the full blades provided adjacent to each other, towards the exit portion, the splitter blade having a front edge and a rear edge in a flow direction of the fluid, the splitter blade having a hub side and a tip side in a direction of height of the splitter blade from a hub surface;
the tip side of the front edge of the splitter blade being displaced toward a negative-pressure surface of the full blade from a position equidistant from the adjacent full blades in a circumferential direction of the impeller;
the hub side of the front edge of the splitter blade being placed at the position equidistant from the adjacent full blades or displaced toward a positive-pressure surface of the full blade from a position equidistant from the adjacent full blades in the circumferential direction; and
the hub side of the rear edge of the splitter blade being displaced toward the positive-pressure surface of the full blade from the position equidistant from the full blades in the circumferential direction.

Assignees

• Hoshi Toru
• Tomita Isao
• Iwakiri Kenichiro
• Shiraishi Takashi
• Mitsubishi Heavy Ind Ltd

Inventors

• Hoshi Toru
• Tomita Isao
• Iwakiri Kenichiro
• Shiraishi Takashi

Classifications

• F04D29/30

  Vanes · CPC title

• F01D5/225 Primary

  by shrouding · CPC title

• F04D29/284 Primary

  for compressors · CPC title