Compressor wheel for turbocharger

Patent metadata

Field	Value
Publication number	US-11193494-B2
Application number	US-201916693251-A
Country	US
Kind code	B2
Filing date	Nov 23, 2019
Priority date	Apr 23, 2019
Publication date	Dec 7, 2021
Grant date	Dec 7, 2021

Abstract

A compression wheel for a turbocharger includes: a wheel hub; and a plurality of blades that are arranged around the wheel hub in a spiral shape, where a round portion is provided at a tip of a leading edge of each of the blades.

First claim

What is claimed is:

1. A compressor wheel for a turbocharger, the compressor wheel comprising:
a wheel hub; and
a plurality of blades provided around the wheel hub in a spiral shape,
wherein when the plurality of blades is arranged such that relatively large main blades and relatively small sub blades are alternately arranged around the wheel hub, a round portion is provided only in a tip of a leading edge of each of the relatively large main blades.

2. The compressor wheel of claim 1 , wherein the round portion is configured such that a round projected area that is an area of a round projected length sweeping away on a projection plane by one rotation is within a range of 15% to 20% of an effective inlet area that is an area of the leading edge of each of the plurality of blades sweeping away on the projection plane by said one rotation, the round projected length being a radial length of the compressor wheel that is obtained by projecting the round portion on the projection plane perpendicular to a rotation shaft of the compressor wheel.

3. The compressor wheel of claim 2 , wherein the round projected length is determined by an equation:
√{square root over ( R 2 −0.15( R 2 −R H 2 ))}≤ R ≤√{square root over ( R 2 −0.2( R 2 −R H 2 ))},

wherein R is the round projected length,
R is a maximum radius at an inlet side of the compressor wheel, and
R H is a radius of the wheel hub.

4. The compressor wheel of claim 2 , wherein the leading edge of each of the plurality of blades is cut within 30% of an overall length of the leading edge from the tip of the leading edge and within a predetermined reference length.

5. The compressor wheel of claim 4 , wherein the predetermined reference length is 0.2 mm.

Assignees

• Hyundai Motor Co Ltd
• Kia Motors Corp
• Korea Advanced Inst Sci & Tech

Inventors

• Cho Teock Hyeong
• Jung Gue Hyun
• Lee Yong Cheol
• Kim Young Sik
• Shin Dal Heun
• Kwon O Jun
• Lee Duck Joo
• Seo Dong Ho

Classifications

• F04D29/284 Primary

  for compressors · CPC title

• F04D29/30

  Vanes · CPC title

• F04D29/666

  by means of rotor construction or layout, e.g. unequal distribution of blades or vanes · CPC title

• F05D2240/307

  related to the tip of a rotor blade · CPC title

• F04D29/663

  Sound attenuation · CPC title