Vane for variable nozzle turbocharger

• US 6,419,464 B1
• Filed: 01/16/2001
• Issued: 07/16/2002
• Est. Priority Date: 01/16/2001
• Status: Expired due to Term

• Current Assignee: Garrett Transportation I Inc. (Garrett Motion, Inc.)
• Original Assignee: Honeywell International Inc.
• Inventors: Arnold, Steven Don
• Primary Examiner(s): Denion, Thomas
• Assistant Examiner(s): TRIEU, THAI BA
• Application Number:
  US09/761,277
• Publication Number:
  US 20020094284A1
• Time in Patent Office: 546 Days
• Field of Search: 415/150, 415/159, 415/160, 415/163, 415/166, 415/164, 415/165, 417/407, 606/02
• US Class Current: 417/407
• 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: F01D 5/141 Shape, i.e. outer, aerodynamic form F01D5/148 - F01D5/20 take precedence; blade construction F01D5/147
• CPC Class Codes: F01D 5/18 Hollow blades, i.e. blades with cooling or heating channels or cavities structure of hollow blades in general F01D5/147; Heating, heat-insulating or cooling means on blades
• CPC Class Codes: F02C 6/12 Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F05D 2250/411 in rotation

Abstract

A vane and post arrangement for a variable geometry turbocharger employs vanes having a hole in a first end surface receiving a post extending from a surface of the nozzle in the turbine housing. A second end surface on each vane incorporates an extending tab which is received in a respective slot in a unison ring for rotation of the vanes on the posts upon movement of the unison ring.

Claims

1. A variable geometry turbocharger assembly comprising:

a turbine housing having an inlet for exhaust gas and an outlet, a volute connected to the inlet, and an integral outer nozzle wall adjacent the volute;

a turbine wheel carried within the turbine housing and attached to a shaft;

a plurality of vanes disposed within the turbine housing, each vane having a hole disposed within a first axial vane surface substantially parallel to the outer nozzle wall, each vane hole receiving a respective post therein, said post projecting outwardly from the outer nozzle wall, the vanes further having actuation tabs extending from a second axial vane surface opposite from the first vane surface;

a rotatable annular unison ring positioned axially adjacent the vanes, the unison ring having a plurality of slots each configured to accommodate a respective tab therein, wherein rotation of the unison ring causes each tab to slide within a respective slot, moving each vane radially within the turbine housing relative to the shaft, such radial vane movement being facilitated by pivoting movement of each vane about a respective post.

2. The variable geometry turbocharger assembly as recited in claim 1 wherein the each post comprises a first diameter section that extends axially from a first post end to an intermediate position on the post, and a second diameter section that is smaller in diameter than the first diameter section, the second diameter section extending axially along the post from the intermediate position to a second post end.

3. The variable geometry turbocharger assembly as recited in claim 1 wherein each vane includes an inner radial surface directed towards the turbine wheel, an outer radial surface opposite from the inner radial surface, and wherein the vane axial surfaces extend between the radial surfaces, wherein the vane axial surfaces include one or more hollow sections.

4. A variable geometry turbocharger assembly comprising:

a turbine housing having an exhaust gas inlet and an exhaust gas outlet, a volute connected to the inlet, and an integral outer nozzle wall adjacent the volute, the nozzle wall comprising a plurality of posts projecting outwardly therefrom;

a turbine wheel carried within the turbine housing and attached to a shaft;

a plurality of vanes pivotably disposed within the turbine housing, each vane having a hole disposed within an axial vane surface positioned substantially parallel to the outer nozzle wall, each vane hole accommodating placement of a respective post therein for providing pivoting vane movement, each vane further comprising an elongated actuation tab extending outwardly from an axial vane surface opposite from the holes;

an annular unison ring disposed within the turbine housing and positioned axially adjacent the axial vane surface of each vane providing the actuating tabs, the unison ring having a plurality of slots to accommodate a respective vane tab therein, wherein each slot is configured to provide nonrotating sliding movement of a respective tab therein; and

means for rotating the unison ring within the turbine housing along an axis running through the shaft, wherein rotation of the ring causes the tabs to slide within respective slots and cause the vanes to move radially inwardly or outwardly relative to the shaft, such radial vane movement being facilitated by the pivoting action of each vane about a respective post.