Turbocharger fatigue life monitor

• US 6,209,390 B1
• Filed: 05/14/1999
• Issued: 04/03/2001
• Est. Priority Date: 05/14/1999
• Status: Expired due to Term

• Current Assignee: Garrett Transportation I Inc. (Garrett Motion, Inc.)
• Original Assignee: Alliedsignal Inc.
• Inventors: LaRue, Gerald Duane, Baker, Donald Ervin
• Primary Examiner(s): MCCALL, ERIC SCOTT
• Application Number:
  US09/312,380
• Time in Patent Office: 690 Days
• Field of Search: 73/112, 73/116, 73/117.2, 73/117.3, 73/118.1, 73/119 R
• US Class Current: 73/112.01
• CPC Class Codes: F02D 41/22 Safety or indicating devices for abnormal conditions in air/fuel ratio feedback systems F02D41/1495, in electric control linkage F02D11/107, in purge control systems F02M25/0809
• CPC Class Codes: G07C 3/00 Registering or indicating the condition or the working of machines or other apparatus, other than vehicles
• CPC Class Codes: Y02T 10/40 Engine management systems

Abstract

Turbocharger fatigue life monitors comprise at least one sensor that measures an actual operating condition of the turbocharger, e.g., turbine rotational speed or turbine inlet temperature. The device comprises a central processing unit for receiving information from each sensor and processing the information, using programs and predetermined turbocharger information, e.g., turbocharger material and stress data stored in one or more storage device in communication with the central processing unit, to provide an actual probability of turbocharger failure. The central processing unit compares the calculated probability of turbocharger failure to a predetermined specified probability of turbocharger failure stored in a storage device to determine whether turbocharger service is needed. The central processing unit provides a signal that operates an annunciator to indicate recommended or necessary turbocharger service when the actual probability of turbocharger failure exceeds the specified probability of turbocharger failure. The central processing unit and storage devices can be packaged independent of or as part of an existing turbocharged application system, e.g., an engine control module when the turbocharged application is a vehicle.

Claims

1. A turbocharger fatigue life monitoring device comprising:

a sensor for measuring rotational speed of a turbocharger shaft;

processing means for receiving a rotational speed signal from the sensor, calculating a probability of turbocharger failure based on the rotational speed signal, and comparing the calculated probability of turbocharger failure to a predetermined specified probability of turbocharger failure, the processing means generating an output signal when the calculated probability of turbocharger failure exceeds the specified probability of turbocharger failure;

indicating means responsive to the output signal from the processing means.

2. The device as recited in claim 1 further comprising a sensor for measuring temperature of a turbocharger turbine inlet, wherein the processing means additionally receives a temperature signal from the temperature sensor to calculate a probability of turbocharger failure.

3. The device as recited in claim 1 further comprising means for converting the rotational speed signal to a fatigue duty cycle that is accessed by the processing means.

4. The device as recited in claim 3 wherein the means for converting is stored in a read-only memory device.

5. The device as recited in claim 3 further comprising means for calculating the fatigue life of a turbocharger from the fatigue duty cycle that is accessed by the processing means.

6. The device as recited in claim 5 wherein the means for calculating is stored in a read-only memory device.

7. The device as recited in claim 5 further comprising means for storing predetermined turbocharger material and stress information for access by the processing means.

8. The device as recited in claim 7 wherein the means for storing is an erasable programmable read only memory device.

9. A turbocharger fatigue life monitor device comprising:

a sensor for measuring rotational speed of a turbocharger shaft;

at least one means for storing a counting program for converting rotational speed information to a fatigue life duty cycle, for storing predetermined turbocharger material and stress information, for storing a predetermined specified probability of turbocharger failure, and for storing a probability program that converts the fatigue life duty cycle and predetermined turbocharger information into a probability of turbocharger failure;

means for processing in communication with the sensor and the at least one storing means receiving rotational speed information from the sensor and the counting program, material and stress information and probability program in the at least one storing means to calculate a probability of turbocharger failure, and to compare the calculated probability of turbocharger failure to the predetermined specified probability of turbocharger failure;

means for indicating that the calculated probability of turbocharger failure exceeds the specified probability of turbocharger failure, the indicating means responsive to an output signal from the processing means.

10. The device as recited in claim 9 further comprising a sensor for measuring temperature of a turbine inlet, wherein the processing means is in communication with the temperature sensor and additionally processes a temperature signal from the temperature sensor to calculate a probability of turbocharger failure.

11. The device as recited in claim 9 wherein the counting program is stored in a read-only memory device.

12. The device as recited in claim 9 wherein the predetermined turbocharger material and stress information is stored in an erasable programmable read only memory device.

13. The device as recited in claim 9 wherein the specified probability of turbocharger failure is stored in an erasable programmable read only memory device.

14. The device as recited in claim 9 wherein the probability program converts the fatigue life duty cycle and predetermined turbocharger information into an is stored in a read-only memory device.

15. A method for determining a service interval for a turbocharger comprising the steps of:

measuring rotational speed of a turbocharger shaft;

converting the measured rotational speed into a fatigue duty cycle;

calculating a probability of turbocharger failure using the fatigue duty cycle and predetermined turbocharger material and stress information;

comparing the calculated probability of turbocharger failure to a predetermined specified probability of turbocharger failure; and

providing an indication that turbocharger service is recommended when the calculated probability of turbocharger failure exceeds the specified probability of turbocharger failure.

16. The method as recited in claim 15, further comprising the step of measuring gas temperature at a turbocharger turbine inlet, and the calculating step includes using the measured gas temperature to calculate the probability of turbocharger failure.

17. The method as recited in claim 15, wherein the steps of converting, calculating and comparing are performed by a central processing unit.

18. The method as recited in claim 17 wherein information used to process rotational speed information into the actual probability of turbocharger failure is stored in one or more storage devices in communication with the central processing unit.

19. The method as recited in claim 16 wherein the steps of converting, calculating and comparing is performed by a central processing unit.

20. The method as recited in claim 19 wherein information used to process rotational speed and temperature information into the probability of turbocharger failure is stored in one or more storage devices in communication with the central processing unit.