Turbocharger having adjustable-trim centrifugal compressor including air inlet wall having cavities for suppression of noise and flow fluctuations

Patent metadata

Field	Value
Publication number	US-11808283-B2
Application number	US-202117445734-A
Country	US
Kind code	B2
Filing date	Aug 24, 2021
Priority date	Apr 26, 2019
Publication date	Nov 7, 2023
Grant date	Nov 7, 2023

Abstract

A compressor for a turbocharger includes an inlet-adjustment mechanism in an air inlet for the compressor, operable to move between an open position and a closed position in the air inlet. The compressor housing upstream of the inlet-adjustment mechanism defines a series of acoustic cavities, and openings are defined in the compressor housing wall leading into the acoustic cavities. The openings and cavities are aimed at mitigating noise and flow pulsation in the air inlet caused when the inlet-adjustment mechanism is adjusted to the closed position to effectively reduce the inlet diameter approaching the compressor wheel.

First claim

What is claimed is:

1. A turbocharger, comprising:
a turbine including a turbine housing;
a compressor assembly comprising a compressor housing and a compressor wheel mounted in the compressor housing and connected to a rotatable shaft for rotation therewith, the compressor wheel having blades and defining an inducer portion, the compressor housing comprising a first housing portion and a second housing portion, the first housing portion comprising an outer wall and an inlet wall formed as a unitary member, the outer wall being disposed radially outwardly of the inlet wall, the inlet wall circumscribing an air inlet for the compressor wheel, the second housing portion defining a tip shroud for the compressor wheel and defining a volute for receiving compressed air from the compressor wheel, the compressor housing upstream of the compressor wheel defining an annular space located radially outward of the air inlet, an axial extent of the annular space being bounded between a radially extending upstream wall which is part of the first housing portion and a radially extending downstream wall which is part of the second housing portion, a radially innermost extremity of the annular space being open to the air inlet;
an inlet-adjustment mechanism disposed in the annular space and adjustable between an open position and a closed position, the inlet-adjustment mechanism being movable radially inwardly from the annular space into the air inlet into the closed position so as to create an orifice having a reduced diameter relative to a nominal diameter of the air inlet; and
wherein the first housing portion defines a first quarter-wave resonator cavity wholly disposed between the outer wall and the inlet wall of the first housing portion, the first housing portion further defining a first opening in the radially extending upstream wall, the first opening leading into the first quarter-wave resonator cavity.

2. The turbocharger of claim 1 , wherein the radially extending upstream wall defines a second opening circumferentially spaced from the first opening, and wherein the first housing portion defines a second quarter-wave resonator cavity wholly disposed between the outer wall and the inlet wall and circumferentially spaced from the first quarter-wave resonator cavity, the second opening leading into the second quarter-wave resonator cavity.

3. The turbocharger of claim 2 , wherein the radially extending upstream wall defines a third opening and a fourth opening, wherein the first housing portion defines a third quarter-wave resonator cavity and a fourth quarter-wave resonator cavity each wholly disposed between the outer wall and the inlet wall, the third opening and the fourth opening respectively leading into the third quarter-wave resonator cavity and the fourth quarter-wave resonator cavity, and wherein the first opening, the second opening, the third opening, and the fourth opening are circumferentially spaced apart, and the first quarter-wave resonator cavity, the second quarter-wave resonator cavity, the third quarter-wave resonator cavity, and the fourth quarter-wave resonator cavity are circumferentially spaced apart.

Assignees

• Garrett Transportation I Inc

Inventors

• Lombard Alain
• Mohtar Hani
• Colombier Dominique
• Pees Stephane

Classifications

• F04D29/665 Primary

  by means of resonance chambers or interference · CPC title

• F01D9/04

  forming ring or sector · CPC title

• F01D17/10

  Final actuators (valves in general F16K {; blades with variable camber F01D5/148}) · CPC title

• F02B33/40

  of non-positive-displacement type · CPC title

• F04D29/4206 Primary

  especially adapted for elastic fluid pumps · CPC title