System and method for turbocharger early failure detection and avoidance

• US 20070283695A1
• Filed: 06/13/2006
• Published: 12/13/2007
• Est. Priority Date: 06/13/2006
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Figura, Giorgio
• Application Number:
  US11/452,855
• Publication Number:
  US 20070283695A1
• Time in Patent Office: Days
• US Class Current: 60/601
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H
• 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: F02D 41/0007 for control of turbo-charged or super-charged engines control of the pumps per se F02B37/12
• CPC Class Codes: F02D 41/221 relating to the failure of actuators or electrically driven elements
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F05D 2260/80 Diagnostics
• CPC Class Codes: F05D 2260/96 Preventing, counteracting or reducing vibration or noise
• CPC Class Codes: F05D 2270/09 to cope with emergencies
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies
• CPC Class Codes: Y02T 10/40 Engine management systems

Abstract

Early detection and avoidance of turbocharger failure are provided by monitoring vibration of the turbocharger rotor using a vibration sensor and providing the output signal of the sensor to a controller programmed to periodically compare the magnitude of the vibration to a predetermined maximum limit. Upon the magnitude of the vibration exceeding the maximum limit, thus indicating a potential abnormal condition, the controller issues a command to a fuel controller for the engine to cause the fuel controller to place the engine in a predetermined safe operating mode selected to reduce the likelihood of turbocharger and engine damage from the abnormal condition.

Claims

1. A method for operating a turbocharged engine system having an internal combustion engine coupled to a turbocharger, the turbocharger having a rotor comprising a turbine and a compressor connected by a rotatable shaft that extends through a bearing-containing center housing of the turbocharger, the turbine being arranged to receive exhaust gas from the engine in order to drive the compressor, the compressor being arranged to supply pressurized air to an intake of the engine, the method comprising the steps of:

detecting vibration of the rotor using a vibration sensor that produces an output signal indicative of the vibration of the rotor;

providing the output signal of the vibration sensor to a controller programmed to periodically compare a magnitude of the vibration to a predetermined maximum limit for vibration magnitude; and

upon the magnitude of the vibration exceeding the maximum limit, thus indicating a potential abnormal condition, the controller issuing a command to a fuel controller for the engine to cause the fuel controller to place the engine in a predetermined safe operating mode selected to reduce the likelihood of turbocharger and engine damage from the abnormal condition.

2. The method of claim 1, wherein upon the magnitude of the vibration exceeding the maximum limit, the controller causes an alarm to be given to an operator of the turbocharged engine system.

3. The method of claim 1, further comprising the step of recording the output signal of the vibration sensor on a recording device as a function of time so as to produce a history of rotor vibration for diagnostic purposes.

4. The method of claim 1, wherein the safe operating mode of the engine is initiated by the controller causing the fuel controller to reduce a rate of fuel flow provided to the engine relative to a rate in effect when the potential abnormal condition is detected.

5. A system for operating a turbocharged engine system having an internal combustion engine coupled to a turbocharger, the turbocharger having a rotor comprising a turbine and a compressor connected by a rotatable shaft that extends through a bearing-containing center housing of the turbocharger, the turbine being arranged to receive exhaust gas from the engine in order to drive the compressor, the compressor being arranged to supply pressurized air to an intake of the engine, the system comprising:

a vibration sensor structured and arranged for detecting vibration of the rotor and producing an output signal indicative of the vibration of the rotor; and

a controller programmed to periodically compare a magnitude of the vibration to a predetermined maximum limit for vibration magnitude and, upon the magnitude of the vibration exceeding the maximum limit, thus indicating a potential abnormal condition, to issue a command to a fuel controller for the engine to cause the fuel controller to place the engine in a predetermined safe operating mode selected to reduce the likelihood of turbocharger and engine damage from the abnormal condition.

6. The system of claim 5, the controller being programmed to cause an alarm to be given to an operator of the turbocharged engine system upon the magnitude of the vibration exceeding the maximum limit.

7. The system of claim 5, further comprising a recording device structured and arranged for recording the output signal of the vibration sensor as a function of time so as to produce a history of rotor vibration for diagnostic purposes.

8. The system of claim 5, wherein the controller comprises an engine control unit for the engine.

9. The system of claim 5, wherein the controller is programmed to initiate the safe operating mode of the engine by causing the fuel controller to reduce a rate of fuel flow provided to the engine relative to a rate in effect when the potential abnormal condition is detected.