Bearing health monitor

• US 20090266073A1
• Filed: 06/03/2009
• Published: 10/29/2009
• Est. Priority Date: 10/11/2005
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Greentree, Christopher
• Granted Patent: US 8,146,358 B2
• Time in Patent Office: Days
• US Class Current: 60/602
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H
• CPC Class Codes: F01D 25/16 Arrangement of bearings; Supporting or mounting bearings in casings bearings per se F16C
• CPC Class Codes: F02B 39/16 Other safety measures for, or other control of, pumps
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F05D 2270/301 Pressure
• CPC Class Codes: F05D 2270/304 Spool rotational speed
• CPC Class Codes: F05D 2270/42 passive or reactive, e.g. using large wind vanes
• CPC Class Codes: F16C 2360/24 Turbochargers in general F02C6/12

Abstract

A turbocharger monitor including a sensor adapted and positioned with respect to a turbocharger housing to sense passing compressor blades, generating both rotor rotation information and rotor displacement information. A controller is configured to receive the generated information from the blade sensor, and to establish rotor rotation speed and an indicator of bearing condition.

Claims

1. A method for monitoring the wear of a bearing of a turbocharger, wherein the turbocharger has a housing containing a wheel rotating with respect to the housing, the wheel including a plurality of blades, comprising:

detecting blade proximity information for the plurality of blades on the rotating wheel as they pass by a blade sensor, the blade proximity information being indicative of a blade distance between passing blades and the blade sensor; and

monitoring the wear of a bearing by establishing a bearing condition based on a variation range over a series of passing blades between the blade proximity information of the minimum blade distance and the blade proximity information of the maximum blade distance, and comparing that variation range to a previously established variation range representing a healthy bearing condition.

2. The method of claim 1, and further comprising notifying an operator of a bearing problem when the bearing condition indicates the bearing wear has exceeded a bearing wear limit.

3. The method of claim 1, and further comprising reducing the rate of compressor wheel rotation when the bearing condition indicates the bearing wear has exceeded a bearing wear limit.

4. The method of claim 1, wherein the bearing condition is only evaluated when established under preestablished operating conditions.

5. The method of claim 1, and further comprising:

tracking information pertaining to the bearing condition; and

reporting the tracked information during a diagnostic procedure.

6. A bearing wear monitor for monitoring the wear of a bearing of a turbocharger, wherein the turbocharger has a housing containing a wheel rotating with respect to the housing, the wheel including a plurality of blades, comprising:

a sensor configured to detect blade proximity information for the plurality of blades on the rotating wheel as they pass by the blade sensor, the blade proximity information being indicative of a blade distance between passing blades and the blade sensor; and

a means for monitoring the wear of a bearing by establishing a bearing condition based on a variation range over a series of passing blades between the blade proximity information of the minimum blade distance and the blade proximity information of the maximum blade distance, and comparing that variation range to a previously established variation range representing a healthy bearing condition.

7. A bearing wear monitor for monitoring the wear of a bearing of a turbocharger, wherein the turbocharger has a housing containing a wheel rotating with respect to the housing, the wheel including a plurality of blades, comprising:

a sensor configured to detect blade proximity information for the plurality of blades on the rotating wheel as they pass by the blade sensor, the blade proximity information being indicative of a blade distance between passing blades and the blade sensor; and

a controller configured to monitor the wear of a bearing by calculating a bearing condition based on a variation range over a series of passing blades between the blade proximity information of the minimum blade distance and the blade proximity information of the maximum blade distance, and comparing that variation range to a previously established variation range representing a healthy bearing condition.

8. The bearing wear monitor of claim 7, wherein the controller is operative to measure and store the previously established variation range at a time when the level of bearing wear was minimal.

9. The bearing wear monitor of claim 7, wherein the controller is configured to only evaluate the bearing condition when the bearing condition is developed at substantially the rotor rotational speed at which the previously established variation range was developed.

10. The bearing wear monitor of claim 7, wherein the controller is configured to only evaluate the bearing condition when the bearing condition is developed at substantially the rotor rotational speed, temperature and oil pressure at which the previously established variation range was developed.

11. The bearing wear monitor of claim 10, wherein the controller is operative to store the previously established variation range for only one operating condition.

12. The bearing wear monitor of claim 7, wherein the controller is operative to send a signal when the bearing condition indicates that bearing wear has exceeded a bearing wear threshold.

13. The bearing wear monitor of claim 7, wherein the controller is operative to light a warning light when the bearing condition indicates that bearing wear has exceeded a first bearing wear threshold, and to reduce the rate of rotor rotation when the bearing condition indicates that bearing wear has exceeded a second bearing wear threshold.

14. A turbocharger, comprising:

a turbine housing containing an exhaust-driven turbine;

a compressor housing containing a compressor wheel configured to be driven in rotation with respect to the compressor housing by the turbine, the compressor wheel including a plurality of compressor blades; and

the bearing wear monitor of claim 7, being operative to detect blade proximity information from the blades of the compressor wheel.

15. An internal combustion engine, comprising:

the turbocharger of claim 14;

a block defining a combustion chamber for combusting fuel;

an intake manifold adapted to received pressurized air from the turbocharger compressor to be mixed with fuel and combusted in the combustion chamber; and

an exhaust manifold adapted to drive the turbocharger turbine with combusted gasses exhausted by the combustion chamber.

16. The internal combustion engine of claim 15, and further comprising an engine control unit adapted to serve as the controller, wherein the controller receives an unconditioned signal from the sensor.

17. The internal combustion engine of claim 16, wherein the controller is adapted to light a warning light when the bearing condition indicates that bearing wear has exceeded a first bearing wear threshold, and when the bearing condition indicates that bearing wear has exceeded a second bearing wear threshold, to do at least one of:

restrict fuel flow to the combustion chamber, and reduce the speed of compressor wheel rotation.

18. The internal combustion engine of claim 15, and further comprising:

an engine control unit adapted to serve as the controller; and

an electric actuator operative to control operation of the turbocharger and digitally communicate with the engine control unit;

wherein the electric actuator is operative to receive the blade proximity information in an analog format from the sensor; and

wherein the electric actuator is operative to provide the blade proximity information to the engine control unit in a digital format.