TURBOCHARGER OPERATING SYSTEM AND METHOD FOR AN INTERNAL COMBUSTION ENGINE

• US 20120177476A1
• Filed: 11/18/2011
• Published: 07/12/2012
• Est. Priority Date: 11/19/2010
• Status: Active Grant

• Current Assignee: Gregg Jones
• Original Assignee: Gregg Jones
• Inventors: Jones, Gregg
• Granted Patent: US 9,062,595 B2
• Time in Patent Office: Days
• US Class Current: 415/1
• CPC Class Codes: F02B 39/14 Lubrication of pumps; Safety measures therefor
• CPC Class Codes: F02D 2200/024 Fluid pressure of lubricating oil or working fluid
• 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: F16C 2360/24 Turbochargers in general F02C6/12
• CPC Class Codes: F16C 25/06 Ball or roller bearings
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A method of operating a turbocharger apparatus on an internal combustion engine, having a first oil circuit and a second oil circuit, includes steps of sensing a plurality of engine operating parameters via a plurality of sensors associated with the internal combustion engine; providing oil to the engine from the first oil circuit at a first pressure level; controlling operation of the second oil circuit for said engine via an electronic control unit, based on the sensed engine operating parameters; and applying a variable hydraulic preload to said first and second bearing assemblies via the operation of the second oil circuit, wherein oil from the second oil circuit is provided at a second pressure level which is different from the first pressure level. A system usable for carrying out such method is also described.

Claims

8. A turbocharger system for an internal combustion engine, said turbocharger system comprising

a turbocharger apparatus operatively connected with the engine;

said turbocharger apparatus comprising;

an elongated center housing having a hollow central bore formed therethrough, and having first, second and third oil routing channels formed therein,

a turbine member comprising a shaft portion extending through the central bore of the elongated center housing, said turbine member having an intake turbine attached to a first end of the shaft portion, and an exhaust turbine attached to a second end of the shaft portion;

a first bearing assembly and second bearing assembly, each operatively supporting said turbine member;

said first and second bearing assemblies are axially separated from each other;

said first bearing assembly connected to said first oil routing channel, and said second bearing assembly connected to said second oil routing channel;

an electronic control unit;

a first oil circuit connected to said third oil routing channel, and operable to provide oil to the turbocharger apparatus at a first pressure level;

an second oil circuit connected to each of said first and third oil routing channels, and operable to provide oil at a second pressure level which is one of same or different from the first pressure level; and

a plurality of operational sensors mounted on the engine;

wherein during operation, said electronic control unit is operable to control operation of the second oil circuit based in part on the input received from the plurality of operational sensors mounted on the engine for achieving desired pre-loading of the first and second bearing assemblies.

1. A turbocharger system comprising:

an electronic control unit;

a first oil circuit operable to provide oil at a first pressure level;

a second oil circuit which is operable to provide oil at a second pressure level which is different from the first pressure level, wherein operation of the second oil circuit is controlled by the electronic control unit; and

a turbocharger apparatus, comprising;

a center housing having a hollow central bore formed therethrough and having first, second and third oil routing channels formed therein, wherein the first and second oil routing channels are in fluid communication with the second oil circuit;

a first cylindrical sleeve which fits inside of the center housing, the first cylindrical sleeve having a first end with a first seat formed therein and a second end with a second seat formed therein, and a central portion disposed between the first and second ends;

a first disc member which fits into the first seat, the first disc member having a first fluid supply passage formed therethrough which communicates with the first oil routing channel of the center housing, the first fluid passage configured and arranged to receive oil from the second oil circuit;

a first bearing assembly which fits into the first seat adjacent the first disc member, the first bearing assembly receiving oil from the first fluid supply passage;

a second disc member which fits into the second seat, the second disc member having a second fluid supply passage formed therethrough which communicates with the second oil routing channel of the center housing, the second fluid supply passage also configured and arranged to receive oil from the second oil circuit;

a second bearing assembly which fits into the second seat adjacent the second disc member, the second bearing assembly receiving oil from the second fluid supply passage;

a second cylindrical sleeve which fits coaxially inside of the first cylindrical sleeve, wherein the first and second disc members receive respective ends of the second cylindrical sleeve therein; and

a turbine member comprising a shaft portion which extends through the central bore of the center housing and through the second cylindrical sleeve, an intake turbine attached to a first end of the shaft portion, and an exhaust turbine attached to a second end of the shaft portion;

wherein the second oil circuit is operable by the electronic control unit to apply a selectively variable hydraulic preload to the first and second bearing assemblies.

2. A turbocharger system according to claim 1, further comprising an engine speed sensor, a coolant temperature sensor, and an intake manifold pressure sensor, each operatively mounted on the engine, wherein said electronic control unit controls operation of the second oil circuit for achieving desired oil pressure based on input received from the engine speed sensor, the coolant temperature sensor, and the intake manifold pressure sensor.

3. A turbocharger system according to claim 2, wherein said electronic control unit is operable to control the second oil circuit such that a reduced pre-load is applied to the bearing assemblies at a low engine speed, and increased pre-load is applied to the bearing assemblies at a high engine speed.

4. A turbocharger system according to claim 1, wherein the second oil circuit is separately controlled from the first oil circuit.

5. A turbocharger system according to claim 1, further comprising a spring which is disposed in the central portion of the first cylindrical sleeve between the first and second disc members, and which surrounds the second cylindrical sleeve.

6. A turbocharger system according to claim 1, wherein the second oil circuit receives oil from a source different from an oil pan of the engine.

7. A turbocharger system according to claim 1, further comprising an oil pressure sensor operatively associated with the first and second oil routing channels;

wherein said control unit is configured to receive input from said oil pressure sensor, and further control the operation the second oil circuit for regulating the oil pressure applied the first and second bearing assemblies for achieving desired pre-loading thereof based in part on the input received from said oil pressure sensor.

9. A turbocharger system according to claim 8, wherein said plurality of sensors comprise an engine speed sensor, a coolant temperature sensor, and an intake manifold pressure sensor.

10. A turbocharger system according to claim 9, wherein said electronic control unit is operable to control the second oil circuit such that reduced pre-load is applied to bearing assemblies at low engine speed, and increased pre-load is applied to the bearing assemblies at high engine speed.

11. A turbocharger system according to claim 8, wherein the second oil circuit is separate from the first oil circuit.

12. A turbocharger system according to claim 8, wherein each of the first oil circuit and the second oil circuit receives oil stored in an oil pan of the engine.

13. A turbocharger system according to claim 8, wherein the third oil routing channel is arranged between said first and second oil routing channels.

14. A turbocharger system according to claim 8, further comprising an oil pressure sensor operatively associated with the first and second oil routing channels;

wherein said control unit is configured to receive input from said oil pressure sensor, and further control the operation of the second oil circuit for regulating the oil pressure applied the first and second bearing assemblies for achieving desired pre-loading thereof based in part on the input received from said oil pressure sensor.

15. A method of operating a turbocharger apparatus on an internal combustion engine having a first oil circuit and a second oil circuit, said turbocharger apparatus having a pair of axially separated bearing assemblies, said method comprising the steps of:

a) sensing a plurality of engine operating parameters via a plurality of sensors associated with the internal combustion engine;

b) providing oil to the turbocharger apparatus from the first oil circuit at a first pressure level;

c) controlling operation of the second oil circuit for said engine via an electronic control unit, based on the sensed engine operating parameters; and

d) applying a variable hydraulic preload to said pair of bearing assemblies via the operation of said second oil circuit, wherein oil from the second oil circuit which is provided at a second pressure level which is one of same and different from the first pressure level.

16. A method according to claim 15, wherein said electronic control unit is operable to control the second oil circuit such that reduced pre-load is applied to bearing assemblies at low engine speed, and increased pre-load is applied to the bearing assemblies at high engine speed.

17. A method according to claim 14, wherein the second oil circuit is separate from the first oil circuit.

18. A method according to claim 14, wherein each of the first oil circuit and the second oil circuit receives oil stored in an oil pan of the engine.

19. A method according to claim 14, wherein the second oil circuit receives oil from a source different from an oil pan of the engine.

20. A method according to claim 14, wherein said control unit receives input from an oil pressure sensor operatively associated with the first and second oil routing channels, and further controls the operation the second oil circuit for regulating the oil pressure applied the first and second bearing assemblies for achieving desired pre-loading thereof based in part on the input received from the oil pressure sensor.

15-1. A method according to claim 14, wherein the sensed engine operating parameters include engine speed, intake manifold pressure, engine temperature, and exhaust back pressure.