Method and apparatus to stabilize engine state selection using an energy based stabilization strategy for hybrid powertrain systems

Patent metadata

Field	Value
Publication number	US-2016208718-A1
Application number	US-201514820049-A
Country	US
Kind code	A1
Filing date	Aug 6, 2015
Priority date	Jan 16, 2015
Publication date	Jul 21, 2016
Grant date	—

Abstract

A method for controlling operation of a multi-mode powertrain system includes periodically determining a power cost difference between a first power cost and a second power cost. This includes determining the first power cost associated with operating the powertrain system with the engine operating in a presently commanded engine state in response to an operator torque request and determining the second power cost associated with an expected powertrain operation with the engine operating in a non-commanded engine state in response to the operator torque request. The first power cost is compared with the second power cost, and successive iterations of the periodically determined power cost difference between the first power cost and the second power cost are integrated to determine an integrated power cost difference. A transition to the non-commanded engine state is commanded when the integrated power cost difference is greater than a threshold.

First claim

1 . A method for operating a multi-mode powertrain system including an internal combustion engine operative in a plurality of engine states, the method comprising:
periodically determining a power cost difference between a first power cost and a second power cost, including:
determining the first power cost associated with operating the powertrain system with the engine operating in a presently commanded engine state in response to an operator torque request,
determining the second power cost associated with an expected powertrain operation with the engine operating in a non-commanded engine state in response to the operator torque request, and
comparing the first power cost with the second power cost;
integrating, by a controller, successive iterations of the periodically determined power cost difference between the first power cost and the second power cost to determine an integrated power cost difference; and commanding a transition to the non-commanded engine state when the integrated power cost difference is greater than a threshold.

2 . The method of claim 1 , wherein the engine states include a full cylinder state, a cylinder-deactivation state, a full cylinder-zero fuel state, and a cylinder-deactivation/zero fuel state.

3 . The method of claim 1 , further comprising resetting the integrated power cost difference to zero when the first power cost is greater than the second power cost.

4 . The method of claim 1 , wherein determining the first power cost associated with operating the powertrain system with the engine operating in a presently commanded engine state in response to an operator torque request comprises determining a power cost associated with fuel and electrical power consumption for operating the multi-mode powertrain system with the engine operating in the presently commanded engine state in response to the operator torque request.

5 . The method of claim 1 , further comprising commanding the transition to the non-commanded engine state only when the integrated power cost difference is greater than the threshold.

6 . The method of claim 1 , further comprising transitioning from an initial engine state including the presently commanded engine state to a final engine state including to the non-commanded engine state including executing an engine state transition logic process including a change of mind operation.

7 . The method of claim 6 , wherein executing the engine state transition logic process including the change of mind operation comprises transitioning from the initial engine state to an uncommitted engine state.

8 . The method of claim 7 , further comprising transitioning from the uncommitted engine state back to the initial engine state in response to a change in operating conditions when a transition during the uncommitted engine state is not far advanced.

9 . The method of claim 8 , wherein the change in operating conditions comprises a change in an operator input to an accelerator pedal.

10 . The method of claim 7 , further comprising transitioning from the uncommitted engine state to a stabilizing engine state when a transition during the uncommitted engine state is advanced.

11 . The method of claim 10 , wherein transitioning to the stabilizing engine state includes executing an engine manifold pump-down.

12 . The method of claim 10 , wherein transitioning to the stabilizing engine state includes discontinuing engine fueling prior to opening engine valves.

13 . The method of claim 10 , further comprising transitioning from the stabilizing engine state to the final engine state when the transition is advanced and there is no change in the operating conditions.

14 . A multi-mode powertrain system, comprising:
an internal combustion engine rotatably coupled to an electro-mechanical transmission and controlled by a controller; the internal combustion engine being operative in a plurality of engine states, the controller including executable code, said code operative to:
periodically determine a power cost difference between a first power cost and a second power cost, including code operative to:
determine the first power cost associated with operating the powertrain system with the engine operating in a presently commanded engine state in response to an operator torque request,
determine the second power cost associated with an expected powertrain operation with the engine operating in a non-commanded engine state in response to the operator torque request, and
compare the first power cost with the second power cost;

integrate successive iterations of the periodically determined power cost difference between the first power cost and the second power cost to determine an integrated power cost difference; and
command a transition to the non-commanded engine state when the integrated power cost difference is greater than a threshold.

15 . The multi-mode powertrain system of claim 14 , wherein the engine states include a full cylinder state, a cylinder-deactivation state, a full cylinder-zero fuel state, and a cylinder-deactivation/zero fuel state.

16 . The multi-mode powertrain system of claim 14 , further comprising the controller including executable code operative to reset the integrated power cost difference to zero when the first of the power costs is greater than the second of the power costs.

17 . The multi-mode powertrain system of claim 14 , wherein the controller including executable code operative to determine the power cost associated with operating the powertrain system with the engine operating in the commanded engine state in response to the operator torque request comprises the controller including executable code operative to determine a power cost associated with fuel and electrical power consumption for operating the multi-mode powertrain system with the engine operating in the commanded engine state in response to the operator torque request.

18 . The multi-mode powertrain system of claim 14 , further comprising the controller including executable code operative to command the transition to the non-commanded engine state only when the integrated power cost difference is greater than the threshold.

19 . The multi-mode powertrain system of claim 14 , further comprising the controller including executable code operative to transition from an initial engine state including the presently commanded engine state to a final engine state including the non-commanded engine state includes executable code operative to execute an engine state transition logic process including a change of mind operation.

Assignees

• Gm Global Tech Operations Inc

Inventors

• Kim Kee Yong
• Heap Anthony H
• Janczak John
• Lado Samantha Victoria
• Wei Yaoyao

Classifications

• B60W20/10

  Controlling the power contribution of each of the prime movers to meet required power demand · CPC title

• F02D41/0087

  Selective cylinder activation, i.e. partial cylinder operation (deceleration cut-off F02D41/123) · CPC title

• F02D29/02 Primary

  peculiar to engines driving vehicles; peculiar to engines driving variable pitch propellers · CPC title

• B60W2710/0666

  Engine torque · CPC title

• F02D41/1402

  Adaptive control · CPC title