Method of avoiding low cycle fatigue failure of turbochargers

• US 6,163,254 A
• Filed: 11/23/1999
• Issued: 12/19/2000
• Est. Priority Date: 11/23/1999
• Status: Active Grant

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Incorporated
• Inventors: Smith, Ronald E., Uhland, Gregg W.
• Primary Examiner(s): Lefkowitz, Edward
• Application Number:
  US09/447,614
• Time in Patent Office: 392 Days
• Field of Search: 340/438, 340/439, 340/441, 60/602, 60/605.1, 60/608, 73/116, 73/117.2, 73/117.3, 73/117.4, 73/118.1, 123/478, 123/479, 123/486, 701/29, 701/54, 701/101, 701/102
• US Class Current: 340/439
• CPC Class Codes: F02B 37/00 Engines characterised by provision of pumps driven at least for part of the time by exhaust
• CPC Class Codes: F02B 39/16 Other safety measures for, or other control of, pumps
• CPC Class Codes: F02D 2041/228 Warning displays
• CPC Class Codes: F05B 2220/40 in turbochargers

Abstract

A method of avoiding low cycle fatigue failure of a turbocharger for an internal combustion engine having an electronic control module comprising the steps of: counting the number of cycles the speed of the engine and the fuel rate exceed a predetermined combination for a period of time and then drop below a lower predetermined combination for a period of time, determining an allowable number of said speed cycles that the turbocharger can experience without low cycle fatigue failure, comparing the counted number of speed cycles to the allowed number of speed cycles, providing an indication of the percentage of the counted speed cycles compared to the allowable number of speed cycles, and providing a signal that will alert an operator that the turbocharger is approaching low cycle fatigue failure.

Claims

1. A method of avoiding low cycle fatigue failure of a turbocharger for an internal combustion engine having an electronic control module comprising the steps of:

counting the number of cycles the speed of the turbocharger exceeds a high predetermined speed for a period of time and then drops below a lower predetermined speed for a period of time;

determining an allowable number of said speed cycles that the turbocharger can experience without low cycle fatigue failure;

comparing the counted number of speed cycles to the allowed number of speed cycles; and

providing a signal that will alert an operator that the turbocharger is approaching low cycle fatigue failure.

2. The method as set forth in claim 1, further comprising the step of providing an indication of the percentage of counted speed cycles compared to said allowable number of speed cycles.

3. The method as set forth in claim 1, further comprising the step of determining said high and lower predetermined turbocharger speeds utilizing a torque, speed and fuel rate map and picking a high engine speed and fuel rate at which the engine must operate and then a lower engine speed and fuel rate at which the engine must operate to constitute one speed cycle.

4. The method as set forth in claim 3, wherein the step of determining the allowable number of speeds cycles, further comprises applying an altitude factor to reduce the number of allowable speed cycles as altitude at which the engine operates increases.

5. The method as set forth in claim 1, wherein the step of determining the allowable number of speed cycles that the turbocharger can experience with out low cycle fatigue failure comprises making a detailed stress analysis of the turbocharger to determine speed at which the turbocharger will fail due to over speeding, the stress caused by speed cycles and the number of speed cycles that result in low cycle fatigue failure.

6. The method as set forth in claim 1, further comprising the step of empirically testing the turbochargers for low cycle fatigue failure by counting the number of speed cycles required for the turbocharger to fail.

7. The method as set forth in claim 6, wherein the step of determining the allowable number of speed cycles further comprises applying an altitude factor that decreases the allowable number of speed cycles as the altitude at which the engine operates increases.

8. The method as set forth in claim 5, wherein the step of determining the allowable number of speed cycles further comprises applying an altitude factor that decreases the allowable number of speed cycles as the altitude at which the engine operates increases.

9. The method as set forth in claim 3, wherein the predetermined high engine speed and fuel rate is below a lowest normal engine operating speed and fuel rate and the predetermined lower engine speed and fuel rate is above an engine idle speed and fuel rate.

10. The method as set forth in claim 1, wherein the predetermined high engine speed and fuel rate is below a lowest normal engine operating speed and fuel rate and the predetermined lower engine speed and fuel rate is above an engine idle speed and fuel rate.

11. An electronic control module for an internal combustion engine having a turbocharger, wherein the control module counts the number of cycles the speed of the turbocharger exceeds a high predetermined speed for a period of time and then drops below a lower predetermined speed for a period of time;

is provided with an allowable number of said speed cycles that the turbocharger can experience without low cycle fatigue failure;

compares the counted number of speed cycles to the allowed number of speed cycles; and

provides a signal that will alert an operator that the turbocharger is approaching low cycle fatigue failure.

12. The control module as set forth in claim 11, that provides an indication of the percentage of counted speed cycles compared to said allowable number of speed cycles.

13. The control module as set forth in claim 11, that utilizes a torque, speed and fuel rate map and a predetermined high engine speed and fuel rate at which the engine must operate and then a predetermined lower engine speed and fuel rate at which the engine must operate to constitute one speed cycle.

14. The control module as set forth in claim 13, that reduces the number of allowable speed cycles as altitude at which the engine operates increases.

15. The control module as set forth in claim 14, that provides an indication of the percentage of counted speed cycles compared to said allowable number of speed cycles.

16. The control module as set forth in claim 15, wherein the predetermined high engine speed and fuel rate is set below a lowest normal engine operating speed and fuel rate and the predetermined lower engine speed and fuel rate is set above an engine idle speed and fuel rate.

17. The control module as set forth in claim 11, wherein the predetermined high engine speed and fuel rate is set below a lowest normal engine operating speed and fuel rate and the predetermined lower engine speed and fuel rate is set above an engine idle speed and fuel rate.