IP Library Granted Patent US 7,593,828
Granted Patent B2
US 7,593,828 · App. 11/839,707 · Granted Sep 22, 2009

Method and apparatus for monitoring a variable geometry intake air compressor device

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,593,828
App. No.
11/839,707
Granted
Sep 22, 2009
Kind
B2
Abstract

A method for monitoring operation of a variable geometry turbocharger device includes monitoring exhaust gas pressure and vane position of the variable geometry turbocharger device. Exhaust pressure and vane position are estimated. Residual exhaust pressure and vane position are calculated based upon differences between the estimated and monitored exhaust gas pressures and vane positions. The turbocharger is determined operating properly based upon the exhaust pressure residual and the vane position residual.

Claims (59)

1. A method for monitoring operation of a variable geometry turbocharger device, comprising:

applying a plurality of control signals to an engine system including said variable geometry turbocharger device;

monitoring exhaust gas pressure and vane position of the variable geometry turbocharger device;

estimating an exhaust pressure and a vane position based on the control signals and the monitored exhaust gas pressure and vane positions;

calculating an exhaust pressure residual and a vane position residual based upon differences between the estimated exhaust gas pressures and vane positions and the monitored exhaust gas pressures and vane positions; and,

determining the turbocharger is operating properly based upon the exhaust pressure residual and the vane position residual.

2. The method of claim 1 , wherein determining the turbocharger is operating properly further comprises determining components of the turbocharger are operating properly based upon the exhaust pressure residual and the vane position residual.

3. The method of claim 1 , further comprising identifying a fault in a component of the turbocharger based upon the exhaust pressure residual and the vane position residual.

4. The method of claim 3 , further comprising mitigating effects of the identified fault in the component of the turbocharger to prevent damage to an engine attached thereto.

5. The method of claim 3 , wherein identifying the fault in a component of the turbocharger based upon the exhaust pressure residual and the vane position residual comprises calculating cumulative sums of the exhaust pressure residual and the vane position residual over a period of time, and comparing the cumulative sums to thresholds.

6. The method of claim 5 , comprising identifying an in-range fault in the exhaust pressure sensor when the cumulative sum of the exhaust pressure residual surpasses a threshold.

7. The method of claim 5 , comprising identifying a position sensor fault when the cumulative sum of the vane residual surpasses a threshold.

8. The method of claim 1 , wherein estimating an exhaust pressure comprises:

determining an exhaust flow mass and vane opening position of the variable geometry turbocharger;

determining an exhaust pressure ratio based upon the exhaust flow and the opening of the intake air compressing device; and,

determining exhaust pressure based upon the exhaust pressure ratio.

9. A method for monitoring operation of a variable geometry turbocharger device, comprising:

monitoring exhaust gas pressure and vane position of the variable geometry turbocharger device;

estimating an exhaust pressure and a vane position;

calculating an exhaust pressure residual and a vane position residual based upon differences between the estimated and monitored exhaust gas pressures and vane positions;

determining the turbocharger is operating properly based upon the exhaust pressure residual and the vane position residual; and,

identifying a fault in a component of the turbocharger based upon the exhaust pressure residual and the vane position residual comprising identifying and isolating component faults comprising stuck vanes, vane position sensor in-range, exhaust pressure sensor in-range, and a stuck wastegate bypass valve.

10. A method for monitoring operation of a variable geometry turbocharger device, comprising:

monitoring exhaust gas pressure and vane position of the variable geometry turbocharger device;

estimating an exhaust pressure and a vane position;

calculating an exhaust pressure residual and a vane position residual based upon differences between the estimated and monitored exhaust gas pressures and vane positions;

determining the turbocharger is operating properly based upon the exhaust pressure residual and the vane position residual;

identifying a fault in a component of the turbocharger based upon the exhaust pressure residual and the vane position residual comprising calculating cumulative sums of the exhaust pressure residual and the vane position residual over a period of time, and comparing the cumulative sums to thresholds; and,

identifying a vane-stuck fault when the cumulative sum of the vane residual surpasses a threshold.

11. A method for monitoring operation of an internal combustion engine equipped with a variable geometry turbocharger, comprising:

applying a plurality of control signals to the internal combustion engine;

monitoring signals output from an exhaust pressure sensor and a vane position sensor for the variable geometry turbocharger;

estimating an engine exhaust pressure signal and a vane position signal based on the control signals and the monitored signals output from the exhaust pressure sensor and the the vane position sensor;

calculating an exhaust pressure residual and a vane position residual based upon differences between the monitored signals and estimated signals; and,

identifying a fault in a component of the turbocharger based upon the exhaust pressure residual and the vane position residual.

12. A method for monitoring operation of an internal combustion engine equipped with a variable geometry turbocharger, comprising:

monitoring signals output from an exhaust pressure sensor and a vane position sensor for the variable geometry turbocharger;

estimating an engine exhaust pressure and a vane position;

calculating an exhaust pressure residual and a vane position residual based upon differences between the monitored and estimated signals; and,

identifying a fault in a component of the turbocharger based upon the exhaust pressure residual and the vane position residual wherein identifying the fault in a component of the turbocharger comprises identifying and isolating component faults in vanes of the variable geometry turbocharger, the vane position sensor, an exhaust pressure sensor, and a wastegate bypass valve.

13. The method of claim 12 , further comprising identifying and isolating a stuck vane for the variable geometry turbocharger based upon the exhaust pressure residual and the vane position residual.

14. The method of claim 12 , further comprising identifying and isolating an in-range fault for the vane position sensor based upon the exhaust pressure residual and the vane position residual.

15. The method of claim 12 , further comprising identifying and isolating a wastegate fault based upon the exhaust pressure residual and the vane position residual.

16. The method of claim 12 , further comprising identifying and isolating an in-range fault for the exhaust pressure sensor based upon the exhaust pressure residual and the vane position residual.

17. An article of manufacture, comprising a storage medium having a computer program encoded therein and operative to monitor operation of a variable geometry turbocharger device for an internal combustion engine, the program comprising:

code to apply a plurality of control signals to the internal combustion engine;

code to monitor signals output from an exhaust pressure sensor and a vane position sensor for the variable geometry turbocharger device;

code to estimate an engine exhaust pressure signal and a vane position signal based on the control signals and the monitored signals output from the exhaust pressure sensor and the vane position sensor;

code to calculate an exhaust pressure residual and a vane position residual based upon differences between the monitored and estimated signals;

code to determine components of the turbocharger are operating properly based upon the exhaust pressure residual and the vane position residual; and,

code to identify a fault in the turbocharger based upon the exhaust pressure residual and the vane position residual.

18. The article of claim 17 , wherein the code to identify the fault in a component of the turbocharger based upon the exhaust pressure residual and the vane position residual comprises code to calculate cumulative sums of the exhaust pressure residual and the vane position residual over a period of time, and compare the cumulative sums to thresholds.

19. A method for monitoring operation of a variable geometry turbocharger device, comprising:

monitoring exhaust gas pressure and vane position of the variable geometry turbocharger device;

estimating an exhaust pressure and a vane position;

calculating an exhaust pressure residual and a vane position residual based upon differences between the estimated and monitored exhaust gas pressures and vane positions;

determining the turbocharger is operating properly based upon the exhaust pressure residual and the vane position residual;

identifying a fault in a component of the turbocharger based upon the exhaust pressure residual and the vane position residual wherein identifying the fault comprises calculating cumulative sums of the exhaust pressure residual and the vane position residual over a period of time, and comparing the cumulative sums to thresholds; and,

identifying a wastegate fault when the cumulative sum of the exhaust pressure residual surpasses a threshold subsequent to a command to open the wastegate.

Assignments (12)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034185/0587 →
CHANGE OF NAME Recorded Feb 10, 2011
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 025781/0035 →
SECURITY AGREEMENT Recorded Nov 8, 2010
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: WILMINGTON TRUST COMPANY
Reel/Frame 025324/0057 →
RELEASE OF SECURITY INTEREST Recorded Nov 5, 2010
From: UAW RETIREE MEDICAL BENEFITS TRUST
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025314/0946 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025245/0656 →
SECURITY AGREEMENT Recorded Aug 28, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UAW RETIREE MEDICAL BENEFITS TRUST
Reel/Frame 023162/0140 →
SECURITY AGREEMENT Recorded Aug 27, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 023156/0264 →
RELEASE OF SECURITY INTEREST Recorded Aug 21, 2009
From: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES; CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023155/0880 →
RELEASE OF SECURITY INTEREST Recorded Aug 20, 2009
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023124/0670 →
SECURITY AGREEMENT Recorded Apr 16, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES; CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES
Reel/Frame 022554/0479 →
SECURITY AGREEMENT Recorded Feb 4, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 022201/0448 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 16, 2007
From: WANG, YUE-YUN; HASKARA, IBRAHIM
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 019705/0339 →