Adjustable-trim centrifugal compressor, and turbocharger having same

Patent metadata

Field	Value
Publication number	US-9683484-B2
Application number	US-201514642825-A
Country	US
Kind code	B2
Filing date	Mar 10, 2015
Priority date	Mar 10, 2015
Publication date	Jun 20, 2017
Grant date	Jun 20, 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 conduit comprising a plurality of vanes that in the closed position collectively form a converging 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 conduit. 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 compressor housing defining a shroud surface that is adjacent to outer tips of the blades of the compressor wheel;
a compressor inlet-adjustment mechanism disposed in the air inlet and being movable between an open position and a closed position, the inlet-adjustment mechanism comprising a variable-geometry conduit comprising a plurality of vanes that in the closed position collectively form a converging 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 conduit, the vanes in the open position being 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,
the variable-geometry conduit further including a plurality of vane-moving members disposed on radially outer sides of the vanes, wherein each of the vane-moving members pivots about a leading edge of the vane-moving member, a movable actuator member engaged with the vane-moving members, and a transmission that converts the movement of the actuator member into pivoting of the vane-moving members for moving the variable-geometry conduit between the closed and open positions respectively.

2. The turbocharger of claim 1 , wherein the actuator member is axially movable for adjusting the inlet-adjustment mechanism between the open and closed positions.

3. The turbocharger of claim 2 , wherein the transmission includes control arms that have respective radially outer ends engaged with the actuator member and radially inner ends respectively engaged with the vane-moving members, the control arms being arranged such that axial movement of the actuator member causes the control arms to pivot about respective axes that extend substantially in a circumferential direction about an axis of the compressor, wherein in one axial position of the actuator member the control arms are tilted more toward the circumferential direction of the compressor, and in another axial position of the actuator member the control arms are tilted less in the circumferential direction and more in a radial direction of the compressor, the inner ends of the control arms engaging the vane-moving members at a location spaced downstream from the leading edges of the vane-moving members, such that pivoting of the control arms causes the vane-moving members to pivot which in turn causes the vanes to also pivot.

4. The turbocharger of claim 1 , wherein the actuator member is rotatable for adjusting the inlet-adjustment mechanism between the open and closed positions.

5. The turbocharger of claim 4 , wherein the transmission includes control arms that have respective radially outer ends engaged with the actuator member and radially inner ends respectively engaged with the vane-moving members, the control arms being arranged such that rotational movement of the actuator member causes the control arms to pivot about respective axes that extend substantially in an axial direction of the compressor, wherein in one rotational position of the actuator member the control arms are tilted more toward a circumferential direction about an axis of the compressor, and in another rotational position of the actuator member the control arms are tilted less in the circumferential direction and more in a radial direction, the inner ends of the control arms engaging the vane-moving members at a location spaced downstream from the leading edges of the vane-moving members such that pivoting of the control arms causes the vane-moving members to pivot which in turn causes the vanes to also pivot.

Assignees

• Honeywell Int Inc

Inventors

• Tingaud Aurelien
• Marsal Damien
• Groves Chris
• Lombard Alain
• Toussaint Lionel
• Mohtar Hani

Classifications

• F02B37/24 Primary

  by using pumps or turbines with adjustable guide vanes · CPC title

• Y02T10/144

  Cross-Sectional Technologies · mapped topic

• F04D29/464

  adjusting flow cross-section, otherwise than by using adjustable stator blades · CPC title

• F05D2250/51

  Inlet · CPC title

• F02B2037/125

  Control for avoiding pump stall or surge · CPC title