Engine motion active control

• US 7,225,783 B2
• Filed: 10/04/2005
• Issued: 06/05/2007
• Est. Priority Date: 06/21/2005
• Status: Active Grant

• Current Assignee: GM Global Technology Operations LLC (General Motors Company)
• Original Assignee: GM Global Technology Operations Incorporated (Motors Liquidation Co. GUC Trust)
• Inventors: Tervo, Steven A., Bors, Wolfgang, Fariborzi, Borz, Jacobson, Eric N., Ferrari, Brian E., Wise, Scott, Elzinga, Donald R. Jr., Defenderfer, Eric J., Hohnstadt, Frederick P.
• Primary Examiner(s): Kamen; Noah P.
• Application Number:
  US11/243,518
• Publication Number:
  US 20060283416A1
• Time in Patent Office: 609 Days
• Field of Search: 123/192.1, 123/198.F
• US Class Current: 123/192.1
• CPC Class Codes: F02D 13/06 Cutting-out cylinders
• CPC Class Codes: F02D 17/02 Cutting-out cutting-out engines in multiple engine arrangements F02D25/04
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

An engine active motion control system for controlling engine dynamic torque includes an engine that generates a first dynamic torque. A first module selectively initiates generation of a second dynamic torque about an axis of rotation of a crankshaft of the engine in a direction opposite that of the first dynamic torque generated through the crankshaft.

Claims

1. An engine active motion control system for controlling engine dynamic torque, comprising:

an engine that generates a first dynamic torque; and

a first module that selectively initiates generation of a second dynamic torque about an axis of rotation of a crankshaft of said engine in a direction opposite that of said first dynamic torque generated through said crankshaft, wherein said torque is generated when an engine speed is greater than a first engine speed threshold and is less than a second engine speed threshold.

2. The engine active motion control system of claim 1 further comprising a first pair of active mass absorbers (AMAs) that are offset from said axis of rotation and that each generate a force in a direction that is parallel to a plane defined through said axis of rotation to induce said torque.

3. The engine active motion control system of claim 2 wherein said AMAs are positioned on opposite sides of said axis of rotation and are offset an equivalent distance from said axis of rotation.

4. The engine active motion control system of claim 2 wherein said AMAs are positioned on opposite sides of said axis of rotation, are offset at different distances from said axis of rotation, wherein a force generated by one of said first pair of AMAs is greater than a force generated by another of said first pair of said AMAs.

5. The engine active motion control system of claim 2 further comprising a second pair of AMAs that are offset from said axis of rotation and that each generate a force in a direction that is parallel to a plane defined through said axis of rotation to induce said torque.

6. The engine active motion control system of claim 1 wherein said engine is a displacement on demand engine that is operable in activated and deactivated modes.

7. A method for controlling engine operation during activated and deactivated modes in a displacement on demand engine, comprising:

transitioning said engine to said deactivated mode; and

selectively generating a torque about an axis of rotation of a crankshaft of said engine in a direction opposite that of a drive torque generated through said crankshaft, wherein said torque is generated when an engine speed is greater than a first engine speed threshold and is less than a second engine speed threshold.

8. The method of claim 7 further comprising providing a first pair of active mass absorbers (AMAs) that are offset from said axis of rotation and that each generate a force in a direction that is parallel to a plane defined through said axis of rotation to induce said torque.

9. The method of claim 8 wherein said AMAs are positioned on opposite sides of said axis of rotation and are offset an equivalent distance from said axis of rotation.

10. The method of claim 8 wherein said AMAs are positioned on opposite sides of said axis of rotation, are offset at different distances from said axis of rotation, wherein a force generated by one of said first pair of AMAs is greater than a force generated by another of said first pair of said AMAs.

11. The method of claim 8 further comprising providing a second pair of AMAs that are offset from said axis of rotation and that each generate a force in a direction that is parallel to a plane defined through said axis of rotation to induce said torque.

12. A method of reducing engine vibration during a deactivated mode of a displacement on demand engine, comprising:

determining whether to transition said engine to said deactivated mode;

monitoring an engine speed; and

activating an active mass absorber (AMA) based on said engine speed to generate a torque about an axis of rotation of a crankshaft of said engine in a direction opposite that of a drive torque generated through said crankshaft, wherein said torque is generated when said engine speed is greater than a first engine speed threshold and is less than a second engine speed threshold.

13. The method of claim 12 further comprising providing a first pair of active mass absorbers (AMAs) that are offset from said axis of rotation and that each generate a force in a direction that is parallel to a plane defined through said axis of rotation to induce said torque.

14. The method of claim 13 wherein said AMAs are positioned on opposite sides of said axis of rotation and are offset an equivalent distance from said axis of rotation.

15. The method of claim 13 wherein said AMAs are positioned on opposite sides of said axis of rotation, are offset at different distances from said axis of rotation, wherein a force generated by one of said first pair of AMAs is greater than a force generated by another of said first pair of said AMAs.

16. The method of claim 13 further comprising providing a second pair of AMAs that are offset from said axis of rotation and that each generate a force in a direction that is parallel to a plane defined through said axis of rotation to induce said torque.