Turbomachine

• US 8,696,308 B2
• Filed: 10/06/2010
• Issued: 04/15/2014
• Est. Priority Date: 10/06/2009
• Status: Active Grant

• Current Assignee: Cummins Limited (Cummins Incorporated)
• Original Assignee: Cummins Limited (Cummins Incorporated)
• Inventors: Denholm, Tim, McEwen, James Alexander, Roberts, Tom J., Holroyd, Robert L., Normington, Christopher, Vijayakumar, Arun, Garrett, Stephen Edward
• Primary Examiner(s): Look, Edward
• Assistant Examiner(s): Hargitt, Christopher J
• Application Number:
  US12/899,298
• Publication Number:
  US 20110194929A1
• Time in Patent Office: 1,287 Days
• Field of Search: 415/151, 415/157, 415/158, 415/160, 415/165, 415/166, 415/167, 415/183, 415/184, 415/185, 415/186, 415/191, 415/203, 415/204, 415/206
• US Class Current: 415/158
• CPC Class Codes: F01D 17/143 the shiftable member being a wall, or part thereof of a radial diffuser
• CPC Class Codes: F01D 17/162 for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line F01D17/167 takes precedence
• CPC Class Codes: F01D 17/165 for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line F01D17/167 takes precedence
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F05D 2250/25 helical
• CPC Class Codes: F05D 2250/314 the axes being inclined in relation to each other

Abstract

According to a first aspect of the present invention there is provided a variable geometry turbine comprising: a turbine wheel mounted for rotation about a turbine axis within a housing, the housing defining an annular inlet surrounding the turbine wheel and defined between first and second inlet sidewalls, the annular inlet being divided into at least two axially offset inlet portions; a cylindrical sleeve axially movable across the annular inlet to vary the size of a gas flow path through the inlet; and a guide for guiding the movement of the cylindrical sleeve, the guide being at least partially located within the inlet at a radially extent of the inlet portions, and extending in an axial direction parallel to the turbine axis.

Claims

1. A variable geometry turbine comprising:

a turbine wheel mounted for rotation about a turbine axis within a housing, the housing defining an annular inlet surrounding the turbine wheel and defined between first and second inlet sidewalls, the annular inlet being divided into at least two axially offset inlet portions;

a cylindrical sleeve axially movable across the annular inlet to vary the size of a gas flow path through the inlet; and

a guide for guiding the movement of the cylindrical sleeve, the guide being at least partially located within the inlet at a radially extent of the inlet portions, and extending in an axial direction parallel to the turbine axis;

wherein the guide comprises one or more elongate members; and

wherein the elongate members are located at an outer radially extent of the inlet portions if the sleeve has an inner diameter that is greater than an outer diameter of inlet portions.

2. The variable geometry turbine of claim 1, wherein the elongate members are located at an inner radially extent of the inlet portions if the sleeve has an outer diameter that is less than an inner diameter of inlet portions.

3. A variable geometry turbine comprising:

a turbine wheel mounted for rotation about a turbine axis within a housing, the housing defining an annular inlet surrounding the turbine wheel and defined between first and second inlet sidewalls, the annular inlet being divided into at least two axially offset inlet portions;

a cylindrical sleeve axially movable across the annular inlet to vary the size of a gas flow path through the inlet; and

a guide for guiding the movement of the cylindrical sleeve, the guide being at least partially located within the inlet at a radially extent of the inlet portions, and extending in an axial direction parallel to the turbine axis;

one or more vanes located in one or both inlet portions, the one or more vanes dividing an inlet portion into at least two inlet passages,

and wherein the guide comprises;

one or more edges of the one or more vanes.

4. The variable geometry turbine of claim 3, wherein, if the sleeve has an inner diameter greater than an outer diameter of the inlet portions, the one or more edges is a leading edge, or are leading edges, of the one or more vanes.

5. The variable geometry turbine of claim 3, wherein, if the sleeve has an outer diameter that is less than an inner diameter of the inlet portions, the one or more edges is a trailing edge, or are trailing edges, of the one or more vanes.

6. A variable geometry turbine comprising:

a turbine wheel mounted for rotation about a turbine axis within a housing, the housing defining an annular inlet surrounding the turbine wheel and defined between first and second inlet sidewalls, the annular inlet being divided into at least two axially offset inlet portions;

a sleeve assembly, comprising a sleeve that is movable in a direction parallel to the turbine axis and across the annular inlet to vary the size of a gas flow path through the inlet, and an actuator for affecting movement of the sleeve;

wherein a helical interface is present in the sleeve assembly, the helical interface being arranged to induce, in use, helical movement of a part of the sleeve assembly;

wherein at least a part of the actuator comprises the helical interface, and the sleeve is arranged to move axially, and/or helically.

7. The variable geometry turbine of claim 6, wherein the sleeve comprises a helical groove or slit, and the actuator comprises:

a rotatable collar that surrounds, or is surrounded by, the sleeve, the rotatable collar being fixed in position in an axial direction, and the rotatable collar being provided with a helical groove or slit; and

a helically or axially moveable annulus located in-between the sleeve and the rotatable collar, the annulus housing one or more bearings configured to sit in the helical groove or slit of the rotatable collar, and to sit in the helical groove or slit provided in the sleeve,

the helical groove or slit of the sleeve, and the helical groove or slit of the rotatable collar, having different handedness.

8. The variable geometry turbine of claim 6, wherein the sleeve comprises a helical groove or slit, and the actuator comprises:

a collar that surrounds, or is surrounded by, the sleeve, the collar being fixed in position, and the collar being provided with a helical groove or slit; and

a helically moveable annulus located in-between the sleeve and the collar, the annulus housing one or more bearings configured to sit in the helical groove or slit of the rotatable collar, and to sit in the helical groove or slit provided in the sleeve,

the helical groove or slit of the sleeve, and the helical groove or slit of the collar, having the same handedness.

9. The variable geometry turbine of claim 7 or claim 8, wherein one or more of the collar, rotatable collar and/or sleeve comprise a plurality of helical grooves or slits, disposed around a circumference of the respective collar, rotatable collar and/or sleeve.