Adjustable-trim centrifugal compressor, and turbocharger having same

Patent metadata

Field	Value
Publication number	US-9845723-B2
Application number	US-201414551218-A
Country	US
Kind code	B2
Filing date	Nov 24, 2014
Priority date	Nov 24, 2014
Publication date	Dec 19, 2017
Grant date	Dec 19, 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 conical mechanism comprising a plurality of vanes that in the closed position collectively form a frusto-conical inlet member having a trailing edge 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 such that an effective diameter of the air inlet at the inducer portion is determined by the trailing edge inner diameter of the variable-geometry conical mechanism. The vanes in the open position are pivoted radially outwardly so as to increase the trailing edge inner diameter of the inlet member and thereby increase the effective diameter of the air inlet at the inducer portion.

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 compressor inlet-adjustment mechanism disposed in the air inlet, followed by a shroud surface that is adjacent to outer tips of the blades of the compressor wheel;
the compressor inlet-adjustment mechanism being movable between an open position and a closed position, the inlet-adjustment mechanism comprising a variable-geometry conical mechanism comprising a plurality of vanes each extending along the downstream direction, from a leading edge to a trailing edge of the vane, the vanes in the closed position collectively forming a frusto-conical inlet member having a trailing edge 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 such that an effective diameter of the air inlet at the inducer portion is determined by the trailing edge inner diameter of the variable-geometry conical mechanism, the vanes in the open position being pivoted radially outwardly about the leading edges of the vanes so as to increase the trailing edge inner diameter of the inlet member and thereby increase the effective diameter of the air inlet at the inducer portion,
wherein the variable-geometry conical mechanism includes a plurality of vane-moving members each extending along the downstream direction, from a leading edge to a trailing edge of the vane-moving member, the vane-moving members being disposed on radially outer sides of the vanes, one said vane-moving member for each said vane, and an actuator member engaged with the vane-moving members, wherein each of the vane-moving members pivots about the leading edge of the vane-moving member, and the actuator member is movable so as to pivot the vane-moving members radially inwardly and radially outwardly for moving the variable-geometry conical mechanism between the closed and open positions respectively.

2. The turbocharger of claim 1 , wherein the vane-moving members include control arms extending from the trailing edges of the vane-moving members, and the actuator member comprises a rotatable ring having generally circumferentially extending cam slots in which the control arms are engaged, each cam slot varying in radius in a circumferential direction of the actuator member such that rotational movement of the actuator member translates into radial movement of the control arms and thus pivotal movement of the vane-moving members.

3. 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 compressor inlet-adjustment mechanism disposed in the air inlet, followed by a shroud surface that is adjacent to outer tips of the blades of the compressor wheel;
the compressor inlet-adjustment mechanism being movable between an open position and a closed position, the inlet-adjustment mechanism comprising a variable-geometry conical mechanism comprising a plurality of vanes each extending along the downstream direction, from a leading edge to a trailing edge of the vane, the vanes in the closed position collectively forming a frusto-conical inlet member having a trailing edge 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 such that an effective diameter of the air inlet at the inducer portion is determined by the trailing edge inner diameter of the variable-geometry conical mechanism, the vanes in the open position being pivoted radially outwardly about the leading edges of the vanes so as to increase the trailing edge inner diameter of the inlet member and thereby increase the effective diameter of the air inlet at the inducer portion; and
a plurality of leading-edge guides mounted respectively at the leading edges of the vanes, and a wire threaded through the leading-edge guides, the vanes pivoting about the wire.

4. The turbocharger of claim 3 , further comprising a plurality of trailing-edge guides mounted respectively at the trailing edge of the vanes, and a drawstring threaded through the trailing-edge guides, with end portions of the drawstring extending out in opposite directions from the trailing-edge guides such that pulling on the end portions in opposite directions causes the circumference of the drawstring to be reduced so as to pivot the vanes inwardly about the wire at the leading edges of the vanes.

5. The turbocharger of claim 3 , further comprising an inflatable bladder mounted about the trailing edges of the vanes, inflation of the bladder exerting radially inward pressure on the vanes to cause the vanes to pivot inwardly.

Assignees

• Honeywell Int Inc

Inventors

• Mohtar Hani
• Villemin Pascal
• Pees Stephane
• Tingaud Aurelien
• Lombard Alain
• Marsal Damien

Classifications

• F05D2220/40

  in turbochargers · CPC title

• F04D29/462 Primary

  especially adapted for elastic fluid pumps · CPC title

• F02B37/22 Primary

  by varying cross-section of exhaust passages or air passages {, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits} (F02B37/24 takes precedence) · CPC title

• F04D29/4213

  suction ports · CPC title

• F04D27/0253

  by throttling (F04D27/0246 takes precedence) · CPC title