Integrated vane stops for variable-geometry turbocharger mechanism

Patent metadata

Field	Value
Publication number	US-10240518-B2
Application number	US-201414774165-A
Country	US
Kind code	B2
Filing date	Mar 12, 2014
Priority date	Mar 15, 2013
Publication date	Mar 26, 2019
Grant date	Mar 26, 2019

Abstract

A variable-geometry turbocharger (1) with a vane lever (11) that provides a stop function at full open position of the guide vanes (8). The integrated vane-open stop controls the full open position of the VTG mechanism. A vane lever (11) preferably has an integrated protrusion (50) that functions as a vane-open stop that contacts an adjacent vane lever (11), an integrated bolt (56), or the upper vane ring (16) at the full open position to regulate maximum exhaust gas flow to the turbine wheel (5).

First claim

What is claimed is:

1. A method for operating a turbocharger ( 1 ) with a variable-turbine geometry mechanism ( 30 ) having lower vane ring ( 12 ), an upper vane ring ( 16 ), and guide vanes ( 8 ) pivotally positioned at least partially between the lower vane ring ( 12 ) and the upper vane ring ( 16 ) for pivoting between a fully open and a fully closed position, and actuator learn software, the method comprising:
adjusting the guide vanes ( 8 ) through a range of operation, the range spanning from a minimum vane position to a maximum vane position of the variable geometry turbocharger while receiving in the actuator learn software a signal indicative of vane position;
adjusting a vane actuator to a maximum open setting when said guide vanes ( 8 ) are in the maximum open position, and
discontinuing learning of vane position when the actuator learn software has learned the maximum open position of the guide vanes ( 8 ),
wherein the guide vanes ( 8 ) change their angle of attack via a vane lever ( 11 ), and wherein the variable-turbine geometry mechanism ( 30 ) includes an integrated vane open stop that controls the full open position of the variable-turbine geometry mechanism ( 30 ).

2. The turbocharger ( 1 ) of claim 1 wherein the vane lever ( 11 ) has an integrated protrusion ( 50 ) that functions as the vane-open stop when contacting other components of the variable-turbine geometry mechanism ( 30 ) to control the full open position of the guide vanes ( 8 ) to regulate exhaust gas flow to the turbine wheel ( 5 ).

3. The turbocharger ( 1 ) of claim 2 wherein the protrusion ( 50 ) extends from an arm member ( 42 ) of the vane lever ( 11 ) to contact a base extension ( 52 ) of an adjacent vane lever ( 11 ) in the full open position.

4. The turbocharger ( 1 ) of claim 3 wherein each vane lever ( 11 ) has said protrusion ( 50 ) and its own base extension ( 52 ) that are coplanar with the vane lever ( 11 ) on opposite sides of the vane lever ( 11 ).

5. The turbocharger ( 1 ) of claim 2 further comprising a bolt ( 56 ) that limits travel at the fully-open guide vanes ( 8 ) wherein the protrusion ( 50 ) on an arm member ( 42 ) of the vane lever ( 11 ) contacts the bolt ( 56 ).

6. The turbocharger ( 1 ) of claim 3 further comprising a bolt ( 56 ) that limits travel at the fully-open guide vanes ( 8 ) when a base extension ( 52 ) of the vane lever ( 11 ) contacts the bolt ( 56 ).

7. The turbocharger ( 1 ) of claim 2 wherein the protrusion ( 50 ) transversely extends from the vane lever ( 11 ) to contact the upper vane ring ( 16 ) at the full open position of the guide vanes ( 8 ).

8. A method for operating a variable-geometry turbocharger ( 1 ) comprising
a compressor impeller ( 33 ) and a turbine wheel ( 5 ) connected by a rotating shaft ( 4 ) and
a vane ring assembly ( 17 ) including a lower vane ring ( 12 ), an upper vane ring ( 16 ), and guide vanes ( 8 ) pivotally positioned at least partially between the lower vane ring ( 12 ) and the upper vane ring ( 16 ) for pivoting between a fully open and a fully closed position, and
a series of vane levers ( 11 ) having respectively an integrated protrusion ( 50 ) extending from an arm member ( 42 ) of the vane lever ( 11 ) that functions as vane-open stops when contacting other components of the turbocharger ( 1 ) to control the full open position of the guide vanes ( 8 ) to regulate exhaust gas flow to the turbine wheel ( 5 ), the method comprising:
adjusting the guide vanes ( 8 ) through a range of operation, the range spanning from a minimum vane position to a maximum vane position of the variable geometry turbocharger while receiving in the actuator learn software a signal indicative of vane position;
adjusting a vane actuator to a maximum open setting in response to the vane position sensor when said guide vanes ( 8 ) are in the maximum open position, and
discontinuing learning of vane position when the actuator learn software has learned the maximum open position of the guide vanes ( 8 ).

9. The turbocharger ( 1 ) of claim 8 wherein the protrusion ( 50 ) contacts an adjacent vane lever ( 11 ) in the full open position.

10. The turbocharger ( 1 ) of claim 8 further comprising a bolt ( 56 ) that limits travel at the fully-open guide vanes ( 8 ) when the protrusion ( 50 ) contacts the bolt ( 56 ).

11. The turbocharger ( 1 ) of claim 8 wherein the protrusion ( 50 ) transversely extends from the arm member ( 42 ) to contact the upper vane ring ( 16 ) at the full open position of the guide vanes ( 8 ).

Assignees

• Borgwarner Inc

Inventors

• Alajbegovic Vahidin
• Van Saun Daniel J
• Lerosen Robert S
• Ward Daniel N

Classifications

• F05D2220/40

  in turbochargers · CPC title

• F01D17/165

  for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line (F01D17/167 takes precedence) · CPC title

• F02B37/24 Primary

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

• Y02T10/144

  Cross-Sectional Technologies · mapped topic

• Y02T10/12

  Improving ICE efficiencies · CPC title