IP Library › Granted Patent US 12,031,450
Granted Patent B2
US 12,031,450 · App. 17/819,641 · Granted Jul 9, 2024

Turbocharger with vaned diffuser for the compressor

Inventors: Haiying Sun (Shanghai, CN); Xiongxiong Tang (Wuhan, CN); Guangqing Zheng (Shanghai, CN)
Assignee: GARRETT TRANSPORTATION I INC.
F01D25/246F01D9/041F01D11/003F05D2220/40F05D2230/64F05D2240/14F05D2250/12F05D2260/36
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Quick Facts
Patent No.
US 12,031,450
App. No.
17/819,641
Granted
Jul 9, 2024
Kind
B2
Abstract

A turbocharger having a centrifugal compressor includes a vaned diffuser. The vaned diffuser is formed by a diffuser ring formed separately from the compressor housing and center housing. The diffuser ring is installed between the compressor and center housings such that a diffuser passage is defined between a surface of the compressor housing and a surface of the diffuser ring. Integral vanes on the diffuser ring extend only partially across the axial width of the diffuser passage. A rectangular-section seal ring is axially compressed between the compressor housing and the diffuser ring for sealing and axial locating of the diffuser ring. Radial locating of the diffuser ring is accomplished by an integral locating pin on the ring, which fits into a receptacle in the center housing.

Claims (10)

1. A turbocharger comprising:

a compressor housing and a centrifugal compressor wheel mounted within the compressor housing and affixed to one end of a shaft, the compressor housing defining a volute for receiving compressed air from the compressor wheel;

a turbine housing and a turbine wheel mounted within the turbine housing and affixed to an opposite end of the shaft;

a center housing containing bearings for the shaft, one side of the center housing abutting the compressor housing and an opposite side of the center housing abutting the turbine housing;

a diffuser ring mounted between the compressor housing and the center housing such that a diffuser passage is defined between a surface of the compressor housing and a surface of the diffuser ring, the diffuser ring defining vanes integrally formed with and axially projecting from said surface of the diffuser ring, an axial height of the vanes being smaller than an axial width of the diffuser passage

a seal ring axially compressed between the compressor housing and the diffuser ring, and

wherein the diffuser ring defines an integrally formed locating pin that axially projects toward the center housing, and the center housing defines a blind receptacle into which the locating pin is received for radially locating the diffuser ring relative to the center housing, and

wherein the center housing defines an integrally formed, axially projecting fence located radially outwardly of and proximate to a radially outer periphery of the seal ring.

2. The turbocharger according to claim 1 , wherein the axial height of the vanes is between one-third and one-half of the axial width of the diffuser passage.

3. The turbocharger according to claim 1 , wherein the seal ring has a rectangular cross-sectional shape.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 15, 2022
From: SUN, HAIYING; TANG, XIONGXIONG; ZHENG, GUANGQING
To: GARRETT TRANSPORTATION I INC.
Reel/Frame 060802/0480 →
Continuity (1)
Related Publication 20240044263A1 · Feb 8, 2024