IP Library › Granted Patent US 10,364,825
Granted Patent B2
US 10,364,825 · App. 15/468,278 · Granted Jul 30, 2019

Centrifugal compressor and turbocharger

Inventor: Yasutaka Bessho (Tokyo, JP)
Assignee: IHI Corporation
F04D29/441F02B39/00F04D17/10F04D29/284F04D29/4206F04D29/4213F04D29/681F04D29/685F02B33/40F02B37/00F05D2220/40F05D2270/101F05D2270/17
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Quick Facts
Patent No.
US 10,364,825
App. No.
15/468,278
Granted
Jul 30, 2019
Kind
B2
Abstract

A centrifugal compressor includes a flow changing groove that is formed on an inner wall of the suction passage and extends in a rotation direction of the compressor wheel. A boundary part of a groove wall of the flow changing groove and the inner wall of the suction passage includes an upstream boundary part positioned on an upstream side in the circulation direction of the gas, and a downstream boundary part positioned on a downstream side in the circulation direction. The upstream boundary part is positioned on the inner side in a radial direction of the compressor wheel than the downstream boundary part, and the flow changing groove is positioned on the upstream side of the wheel in the circulation direction.

Claims (16)

1. A centrifugal compressor comprising:

a housing including a suction passage inside thereof;

a wheel accommodated inside the suction passage; and

a flow changing groove that is formed on an inner wall of the suction passage and extends in a rotation direction of the wheel, wherein

a boundary part that continuously connects a groove wall of the flow changing groove and the inner wall of the suction passage includes an upstream boundary part and a downstream boundary part positioned downstream from the upstream boundary part in a circulation direction of suction gas,

the upstream boundary part is positioned on an upstream side of the groove wall in the circulation direction and inward of the downstream boundary part in a radial direction of the wheel, and

the downstream boundary part is positioned on a downstream side of the groove wall and upstream from the wheel in the circulation direction.

2. The centrifugal compressor according to claim 1 , wherein an angle, in the upstream boundary part, between the groove wall of the flow changing groove or the tangential direction thereof and the inner wall of the suction passage or the tangential direction thereof is 90 degrees or less.

3. The centrifugal compressor according to claim 2 , wherein an angle, in the downstream boundary part, between the groove wall of the flow changing groove or the tangential direction thereof and the inner wall of the suction passage or the tangential direction thereof is 90 degrees or more.

4. The centrifugal compressor according to claim 2 , wherein the flow changing groove includes an upstream groove wall portion that extends in a direction parallel to the radial direction of the wheel from the upstream boundary part, and a downstream groove wall portion that extends from the upstream groove wall portion until the downstream boundary part and is connected to the upstream groove wall portion at an acute angle.

5. The centrifugal compressor according to claim 1 , wherein an angle, in the downstream boundary part, between the groove wall of the flow changing groove or the tangential direction thereof and the inner wall of the suction passage or the tangential direction thereof is 90 degrees or more.

6. The centrifugal compressor according to claim 5 , wherein the flow changing groove includes an upstream groove wall portion that extends in a direction parallel to the radial direction of the wheel from the upstream boundary part, and a downstream groove wall portion that extends from the upstream groove wall portion until the downstream boundary part and is connected to the upstream groove wall portion at an acute angle.

7. The centrifugal compressor according to claim 3 , wherein the flow changing groove includes an upstream groove wall portion that extends in a direction parallel to the radial direction of the wheel from the upstream boundary part, and a downstream groove wall portion that extends from the upstream groove wall portion until the downstream boundary part and is connected to the upstream groove wall portion at an acute angle.

8. The centrifugal compressor according to claim 1 , wherein the flow changing groove includes an upstream groove wall portion that extends in a direction parallel to the radial direction of the wheel from the upstream boundary part, and a downstream groove wall portion that extends from the upstream groove wall portion until the downstream boundary part and is connected to the upstream groove wall portion at an acute angle.

9. The centrifugal compressor according to claim 8 , wherein a boundary part of the upstream groove wall portion and the downstream groove wall portion is curved.

10. A turbocharger comprising the centrifugal compressor according to claim 1 .

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 24, 2017
From: BESSHO, YASUTAKA
To: IHI CORPORATION
Reel/Frame 041719/0128 →
Priority Claims (1)
JP 2015-029784 · Feb 18, 2015 · national
Continuity (2)
Continuation PCTJP2015085451 · Dec 18, 2015
Related Publication 20170198713A1 · Jul 13, 2017
Cited By (1)
US 12,247,578