Adjustable-trim centrifugal compressor, and turbocharger having same

Patent metadata

Field	Value
Publication number	US-9708925-B2
Application number	US-201414573603-A
Country	US
Kind code	B2
Filing date	Dec 17, 2014
Priority date	Dec 17, 2014
Publication date	Jul 18, 2017
Grant date	Jul 18, 2017

Abstract

A centrifugal 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 inlet-adjustment mechanism includes a variable-geometry orifice actuated by a rotatable actuator ring. In the closed position, the orifice's inner diameter is smaller than that of a shroud surface of the compressor housing and therefore dictates the effective inlet diameter for the compressor. In the open position the orifice no longer forms an inner diameter smaller than the shroud surface, so that the effective inlet diameter is determined by the shroud surface.

First claim

What is claimed is:

1. A turbocharger, comprising:
a turbine housing and a turbine wheel mounted in the turbine housing and connected to a rotatable shaft for rotation therewith, the turbine housing receiving exhaust gas and supplying the exhaust gas to the turbine wheel;
a centrifugal compressor assembly comprising a compressor housing and a compressor wheel mounted in the compressor housing and connected to the rotatable shaft for rotation therewith, the compressor wheel having blades and defining an inducer portion, the compressor housing defining an air inlet for leading air generally axially into the compressor wheel, the compressor housing further defining a volute for receiving compressed air discharged generally radially outwardly from the compressor wheel, the air inlet having an inner surface that extends for an axial length along a downstream direction, followed by a shroud surface that is adjacent to outer tips of the blades of the compressor wheel; and
a compressor inlet-adjustment mechanism disposed in the air inlet of the compressor housing and movable between an open position and a closed position, the inlet-adjustment mechanism comprising a variable-geometry orifice, the variable-geometry orifice in the closed position having an inner diameter that is smaller than an inner diameter of the shroud surface of the compressor housing at the inducer portion of the compressor wheel, and the variable-geometry orifice in the closed position being positioned such that the effective diameter of the air inlet at the inducer portion is determined by the inner diameter of the variable-geometry orifice, the variable-geometry orifice in the open position being moved such that an effective diameter of the air inlet at the inducer portion is determined by the shroud surface, the inlet-adjustment mechanism further comprising a rotatable actuator member engaged with the variable-geometry orifice for moving the variable-geometry orifice between the open and closed positions,
wherein the variable-geometry orifice comprises a first annular ring formed in two semi-annular halves that are pivotable about a common axis extending transversely to the rotation axis of the compressor wheel, in the closed position the two halves of the first annular ring being substantially co-planar so as to form the first annular ring, in the open position the two halves being pivoted in opposite directions so that the halves no longer form the first annular ring.

2. The turbocharger of claim 1 , wherein the rotatable actuator member includes gears and the two halves of the first annular ring are attached to axles that have gears meshed with the gears of the rotatable actuator member such that rotation of the rotatable actuator member causes the two halves of the first annular ring to be pivoted via the respective gears.

3. The turbocharger of claim 1 , wherein the variable-geometry orifice further comprises a second annular ring arranged such that the first and second annular rings comprise concentric inner and outer annular rings, respectively each formed in two semi-annular halves, all four of the halves being pivotable about the common axis extending transversely to the rotation axis of the compressor wheel, and the rotatable actuator member comprises a rotatable first actuator ring in driving engagement with the two halves of the inner annular ring and a rotatable second actuator ring in driving engagement with the two halves of the outer annular ring, in the closed position the two halves of the outer annular ring being substantially co-planar so as to form the outer annular ring and the two halves of the inner annular ring being substantially co-planar so as to form the inner annular ring, such that the effective diameter of the air inlet at the inducer portion of the compressor wheel is dictated by the inner diameter of the inner annular ring, the variable-geometry orifice having a partially open position in which the two halves of the inner annular ring are pivoted in opposite directions so that these halves no longer form the inner annular ring, but the two halves of the outer annular ring are still co-planar to form the outer annular ring, such that the effective diameter of the air inlet at the inducer portion of the compressor wheel is dictated by the inner diameter of the outer annular ring, and in the open position the two halves of the inner annular ring are pivoted in opposite directions so that these halves no longer form the inner annular ring, and the two halves of the outer annular ring are pivoted in opposite directions so that these halves no longer form the outer annular ring, such that the effective diameter of the air inlet at the inducer portion of the compressor wheel is dictated by the shroud surface of the compressor housing.

4. The turbocharger of claim 3 , wherein each of the first and second actuator rings includes gears and the two halves of the inner annular ring are attached to axles that have gears meshed with the gears of the first actuator ring, and the two halves of the outer annular ring are attached to axles that have gears meshed with the gears of the second actuator ring.

Assignees

• Honeywell Int Inc

Inventors

• Mohtar Hani
• Villemin Pascal
• Pees Stephane
• Smith William Joseph
• Tingaud Aurelien
• Toussaint Lionel

Classifications

• F05D2220/40

  in turbochargers · CPC title

• F05D2250/51

  Inlet · CPC title

• F01D17/146 Primary

  by throttling the volute inlet of radial machines or engines · CPC title

• F01D17/141

  by means of shiftable members or valves obturating part of the flow path · CPC title

• F05D2250/313

  the axes being perpendicular to each other · CPC title