Ball bearing turbocharger balancer

• US 9,181,804 B1
• Filed: 02/17/2015
• Issued: 11/10/2015
• Est. Priority Date: 02/17/2015
• Status: Active Grant

• Current Assignee: BorgWarner Incorporated
• Original Assignee: BorgWarner Incorporated
• Inventors: Kennedy, Donald Michael
• Primary Examiner(s): Kwok, Helen
• Application Number:
  US14/624,140
• Time in Patent Office: 266 Days
• Field of Search: 734/60, 734/62, 734/68, 734/55, 734/73, 734/76, 734/77, 700/279
• US Class Current: 1/1
• CPC Class Codes: B23P 19/04 for assembling or disassembling parts
• CPC Class Codes: F01D 5/027 Arrangements for balancing for balancing rotating bodies in general F16F15/32; for compensating unbalance G01M1/36
• CPC Class Codes: F04D 25/024 the driving means being assisted by a power recovery turbine
• CPC Class Codes: F04D 29/059 Roller bearings
• CPC Class Codes: F04D 29/601 specially adapted for elastic fluid pumps
• CPC Class Codes: F04D 29/662 Balancing of rotors compensating unbalance G01M1/36
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: F05D 2230/80 Repairing, retrofitting or upgrading methods
• CPC Class Codes: G01M 1/22 and converting vibrations due to imbalance into electric variables
• CPC Class Codes: G01M 1/30 Compensating imbalance

Abstract

A method of balancing a core assembly of a turbocharger. The core assembly may include a rotor assembly having a compressor wheel and a turbine wheel connected for common rotation by a shaft. A first bending critical speed of the rotor assembly may be determined. The core assembly may be mounted in a balancing machine. A drive source may be engaged with the core assembly to impart rotation. The rotor assembly may be rotated at an initial phase speed that is between approximately 5500 revolutions per minute and the first bending critical speed. A state of imbalance of the rotor assembly may be determined at the initial phase speed.

Claims

1. A method of balancing a core assembly of a turbocharger, the core assembly including a rotor assembly having a compressor wheel and a turbine wheel connected for common rotation by a shaft, the method comprising:

determining a first bending critical speed of the rotor assembly;

mounting the core assembly in a balancing machine;

engaging a drive source with the core assembly to rotate the rotor assembly;

rotating the rotor assembly to an initial phase speed that is between approximately 5500 revolutions per minute and the first bending critical speed; and

sensing a state of imbalance of the rotor assembly at the initial phase speed.

2. The method according to claim 1 further comprising:

calculating a correction amount needed to provide balance to the rotor assembly based on the state of imbalance of the rotor assembly; and

modifying a mass of the rotor assembly based on the correction amount.

3. The method according to claim 2 further comprising:

rotating the rotor assembly to a secondary phase speed after modifying the mass, wherein the secondary phase speed is equal to an operational speed of the core assembly.

4. The method according to claim 3 wherein the secondary phase speed is in excess of 200,000 revolutions per minute.

5. The method according to claim 1 wherein the first bending critical speed is at least approximately 30,000 revolutions per minute.

6. The method according to claim 1 wherein the initial phase speed is near the first bending critical speed.

7. The method according to claim 1 further comprising:

calibrating the machine by adding a weight to the rotor assembly and rotating the rotor assembly at the initial phase speed to determine a reference imbalance.

8. The method according to claim 7 further comprising:

comparing the state of imbalance to the reference imbalance.

9. The method according to claim 1 wherein the core assembly is configured to circulate a lubricant.

10. A method of balancing a core assembly of a turbocharger comprising:

assembling a rotor assembly from a compressor wheel and a turbine wheel connected for common rotation by a shaft;

determining a first bending critical speed of the rotor assembly, wherein the first bending critical speed corresponds to a natural frequency of the rotor assembly;

loading the core assembly in a balancing machine;

engaging a drive source with the core assembly to rotate the rotor assembly;

rotating the rotor assembly to an initial phase speed that is between approximately 5500 revolutions per minute and the first bending critical speed;

sensing a state of imbalance of the rotor assembly;

calculating a correction amount needed to provide balance to the rotor assembly based on the state of imbalance of the rotor assembly;

modifying a mass of the rotor assembly based on the correction amount; and

rotating the rotor assembly at a secondary phase speed after modifying the mass, wherein the secondary phase speed is equal to an operational speed of the core assembly.

11. The method according to claim 10 wherein the secondary phase speed is in excess of 200,000 revolutions per minute.

12. The method according to claim 10 wherein the first bending critical speed is at least approximately 30,000 revolutions per minute.

13. The method according to claim 12 wherein the initial phase speed is near the first bending critical speed.

14. The method according to claim 10 further comprising:

calibrating the machine by adding a weight to the rotor assembly and rotating the rotor assembly at the initial phase speed to determine a reference imbalance.

15. The method according to claim 14 further comprising:

comparing the state of imbalance to the reference imbalance.

16. The method according to claim 10 wherein the core assembly is configured to circulate a lubricant.

17. The method according to claim 10 further comprising:

providing the drive source with a motor; and

engaging the motor with the compressor wheel through a belt.

18. The method according to claim 10 wherein the sensing a state of imbalance of the rotor assembly, involves sensing vibration of the rotor assembly.

19. The method according to claim 17 wherein the balancing machine is configured with a compressed air drive and further comprising rotating the rotor assembly by the compressed air drive.

20. A method of balancing a turbocharger that has a ball bearing system supporting a rotor assembly, the method comprising:

assembling a compressor wheel, a turbine wheel, and a shaft to form the rotor assembly;

determining a first bending critical speed of the rotor assembly, wherein the first bending critical speed results in a resonant vibration response of the rotor assembly;

mounting a core assembly in a balancing machine;

engaging a drive source with the core assembly to rotate the rotor assembly;

rotating the rotor assembly at an initial phase speed that is at least 5500 revolutions per minute and that is less than the first bending critical speed;

sensing a state of imbalance of the rotor assembly;

calculating a correction amount needed to provide balance to the rotor assembly based on the state of imbalance of the rotor assembly;

modifying a mass of the rotor assembly based on the correction amount; and

rotating the rotor assembly to a secondary phase speed after modifying the mass, wherein the secondary phase speed is equal to an operational speed of the core assembly.

21. A method of balancing a core assembly of a turbocharger comprising:

assembling a rotor assembly from a compressor wheel and a turbine wheel connected for common rotation by a shaft;

determining a first bending critical speed of the rotor assembly, wherein the first bending critical speed corresponds to a lowest rotational speed for a natural frequency of the rotor assembly;

loading the core assembly in a balancing machine;

engaging a drive source with the core assembly to rotate the rotor assembly;

rotating the rotor assembly to an initial phase speed that is at least 5500 revolutions per minute and is less than the first bending critical speed;

sensing a state of imbalance of the rotor assembly;

calculating a correction amount needed to provide balance to the rotor assembly based on the state of imbalance of the rotor assembly;

stopping the rotor assembly;

changing a mass of the rotor assembly based on the correction amount; and

rotating the rotor assembly at a secondary phase speed after modifying the mass, wherein the secondary phase speed is equal to an operational speed of the core assembly and is faster than the first bending critical speed.

22. The method according to claim 21 wherein the initial phase speed is approximately equal to but less than the first bending critical speed.

23. The method according to claim 21 wherein changing the mass of the rotor assembly involves removing material from the rotor assembly.

24. The method according to claim 21 wherein changing the mass of the rotor assembly involves adding material to the rotor assembly.

25. The method according to claim 21 wherein changing the mass of the rotor assembly is done after rotating the rotor assembly to the initial phase speed and before rotating the rotor assembly to the secondary phase speed.

26. The method according to claim 21 wherein the secondary phase speed is a normal operating speed of the rotor assembly and the initial phase speed is lower than the secondary phase speed.

27. The method according to claim 21 wherein the secondary phase speed is over 200,000 revolutions per minute and the initial phase speed is between 5500 revolutions per minute and 30,000 revolutions per minute.

28. The method according to claim 21 further comprising calibrating the balancing machine by placing a known weight at a selected radius on the rotor assembly;

measuring a first imbalance of the rotor assembly with the known weight;

measuring a second imbalance of the rotor assembly without the known weight while rotating the rotor assembly at the initial phase speed that corresponds to the state of imbalance; and

comparing the first imbalance to the second imbalance.