Title of Invention

" A CONTROL SYSTEM FOR ENABLING AN ENGINE TO OPERATE IN A DECELERATION FUEL CUTOFF MODE "

Abstract A control system for enabling an engine to operate in a deceleration fuel cutoff (DFCO) mode is provided. The system includes; an enable module that selectively enables a DFCO mode based on an accelerator pedal position; and an engine speed module that regulates engine speed based on turbine speed during a predetermined time period after the DFCO mode is enabled.
Full Text GM Reference No. GP-308648-PTT-CD
Attorney Docket No. 8540P-000412
TURBINE OFFSET MATCHING CONTROL SYSTEM
FIELD
[0001] The present disclosure relates to methods and systems for
controlling an engine and more particularly to methods and systems for enabling
a deceleration fuel cutoff operating mode of the engine.
BACKGROUND
[0002] The statements In this section merely provide background
information related to the present disclosure and may not constitute prior art.
[0003] Automatic transmissions use a fluid clutch known as a torque
converter to transfer engine torque from the engine to the transmission. The
torque converter operates through hydraulic force provided by pressurized fluid
from the automatic transmission. The torque converter multiplies engine torque
and directs it through the transmission.
[0004] A conventional torque converter includes a sealed chamber
filled with hydraulic fluid. The chamber includes a pump (or impeller) driven by
the engine, a turbine connected to an output shaft, and a stator that provides
torque multiplication. A torque converter is said to "slip" when the impeller speed
and the turbine speed are not equivalent. Some converters incorporate a lockup
mechanism such as a mechanical clutch that engages at cruising speeds to
physically link the impeller with the turbine. The physical link causes the impeller
and the turbine to rotate at the same or near the same speed, thereby reducing
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Attorney Docket No. 8540P-000412
or eliminating slip. The dutch is applied and released via fluid supplied through a
hollow shaft at the center axis of the rotating converter assembly,
[0005] In some applications, the engine may employ a deceleration fuel
cutoff device that is capable of operating the engine in a deceleration fuel cutoff
(DFCO) mode. Operating in a DFCO mode Is desirable during overrun
conditions (i.e., going down a hill) or in city traffic, as well as for engine speed
limitation purposes. Operation in the DFCO mode contributes to improved fuel
economy.
[0006] in order to enter the DFCO mode, it is desirable for the torque
converter clutch to be applied. This reverses the transfer of torque. More
specifically, the applied clutch allows torque to be transferred from rotating drive
wheels back to the engine crankshaft when the vehicle coasts. If the slip across
the torque converter is too high or too low prior to entering the DFCO mode, the
application of the torque converter clutch may be delayed or may not occur at all.
Hence, delaying or preventing the engine from operating in the DFCO mode and
thus, impacting fuel economy.
SUMMARY
[0007] Accordingly, a control system for enabling an engine to operate
in a deceleration fuel cutoff (DFCO) mode is provided. The system includes: an
enable module that selectively enables a DFCO mode based on an accelerator
pedal position; and an engine speed module that regulates engine speed based
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Attorney Docket No. 8540P-0GQ412
on turbine speed during a predetermined time period after the DFCO mode is
enabled.
[0008] In other features, a method for enabling a deceleration fuel
cutoff mode of an internal combustion engine is provided. The method includes:
receiving a deceleration fuel cutoff (DFCO) request wherein the DFCO request is
initiated based on an accelerator pedal position; controlling engine speed based
on turbine speed after receiving the DFCO request; applying a torque converter
clutch when the engine speed is within a predetermined range of the turbine
speed; and enabling the DFCO mode after the clutch is applied.
[0009] Further areas of applicability will become apparent from the
description provided herein. It should be understood that the description and
specific examples are intended for purposes of illustration only and are not
intended to limit the scope of the present disclosure.
DRAWINGS
[0010] The drawings described herein are for illustration purposes only
and are not intended to limit the scope of the present disclosure in any way.
[0011] Figure 1 is a functional block diagram of a vehicle including a
conventional torque converter system.
[0012] Figure 2 is a dataflow diagram illustrating a turbine offset
matching control system.
[0013] Figure 3 is a flowchart illustrating a turbine offset matching
control method.
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Attorney Docket No. 8540P-000412
DETAILED DESCRIPTION
[0014] The following description is merely exemplary in nature and is
not intended to limit the present disclosure, application, or uses. It should be
understood that throughout the drawings, corresponding reference numerals
indicate like or corresponding parts and features. As used herein, the term
module refers to an application specific integrated circuit (ASIC), an electronic
circuit, a processor (shared, dedicated, or group) and memory that executes one
or more software or firmware programs, a combinational logic circuit, and/or
other suitable components that provide the described functionality.
t
[0015] Referring to Figure 1, a vehicle 10 includes an engine 12 that
drives a transmission 14. Air flows into the engine 12 through a throttle 16.
Fuel is combined with the air to be combusted within cylinders 18. The
combustion process reciprocally drives pistons (not shown) within the cylinders
18. The pistons rotatably drive a crankshaft 22 to produce drive torque. The
engine 12 includes N cylinders 18. Although Figure 1 depicts four cylinders (N =
4), it is appreciated that the engine 12 may include additional or fewer cylinders
18. For example, engines having 4, 5, 6, 8, 10, 12 and 16 cylinders are
contemplated.
[0016] Torque from the engine 12 is supplied to the transmission 14
through a torque converter (TC) 24. The torque converter 24 may be any known
lockup converter including a turbine, a stator, and a torque converter clutch
(TCC). The transmission 14 multiplies the drive torque generated by the engine
12 through one of a plurality of gear ratios to drive a vehicle driveline 26. The
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Attorney Docket No. 8540P-000412
transmission 14 includes a hydraulic pump 28 that regulates pressurized fluid
within the transmission 14 and controls fluid flow to and from the TC 24 via at
least one solenoid-operated valve 30.
[0017] An engine speed sensor 38 generates an engine speed signal
based on a rotational speed of the crankshaft 22. A turbine speed sensor 40
generates a turbine speed signal based on a rotational speed of the turbine
within the torque converter 24. The control module receives the signals and
commands a current and/or pulse width modulated signal to the solenoid 30 in
order to vary the supply of pressurized fluid to the torque converter 24. The
control module 32 controls a slip rate of the TC 24 by varying the pressurized
fluid.
[0018] A vehicle operator manipulates an accelerator pedal 34 to
regulate the throttle 16. A pedal position sensor 36 senses the position of the
accelerator pedal 34 and generates a pedal position signal that is communicated
to the control module 32. The control module 32 generates a throttle control
signal based on the pedal position signal. A throttle actuator (not shown) adjusts
the throttle 16 based on the throttle control signal to regulate air flow into the
engine 12. Such method of controlling the throttle 18 is referred to as electronic
throttle control (ETC). The control module 32 adjusts fuel quantity and generates
a fuel signal to the engine 12 based on the air flow.
[0019] When the pedal position signal indicates that the pedal 34 has
been released and the vehicle is operating in a coast mode, the control module
32 communicates with the engine 12 and various sensors and actuators to
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Attorney Docket No. 8540P-000412
control the activation of a deceleration fuel cutoff (DFCO) mode. In order to
smooth the transition into the DFCO mode, the control module 32 controls the
throttle 16 based on engine speed, turbine speed, and a turbine offset matching
method and system according to the present disclosure.
[0020] More particularly, the control module 32 determines when the
DFCO mode is desired and controls the throttle 16 and fuel such that the engine
speed is equal to the turbine speed plus a predetermined offset. Controlling the
engine speed to be within a predetermined range of the turbine speed allows for
the torque converter clutch to be applied. Once the torque converter clutch is
applied, the DFCO mode is enabled thereby disabling fuel to the engine 12.
Thereafter, the transmission 14 backdrives the unfueled engine 12 through the
torque converter 24 to maintain a default engine speed.
[0021] Referring to Figure 2, a dataflow diagram illustrates various
embodiments of a turbine offset matching system that may be embedded within
the control module 32. Various embodiments of turbine offset matching systems
according to the present disclosure may include any number of sub-modules
embedded within the control module 32. The sub-modules shown may be
combined and/or further partitioned to similarly control the engine during
activation of the DFCO mode. Inputs to the system may be sensed from the
vehicle 10, received from other control modules (not shown) within the vehicle
10, and/or determined from other sub-modules within the control module 32. In
various embodiments, the control module 32 of Figure 2 includes a DFCO enable
module 50 and an engine speed control module 52.
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Attorney Docket No. 8540P-000412
[0022] The DFCO enable module 50 receives as input the accelerator
pedal position 54. Based on the accelerator pedal position 54, the DFCO enable
module 50 selectively sets a DFCO enable flag 56. The DFCO enable flag 56 is
set to TRUE when the accelerator pedal position 54 indicates that an accelerator
pedal tip-out has occurred (e.g., the operator has released the pedal 34 (Figure
1}). Otherwise the DFCO enable FLAG 56 remains set to FALSE. The engine
speed control module 52 receives as input the DFCO enable flag 56, engine
speed 58, turbine speed 60, and gear 62. When the DFCO enable flag 56 is
TRUE, the engine speed control module 52 controls a desired engine speed to
be nearly the same as the turbine speed. In various embodiments the desired
engine speed is controlled to be near the turbine speed plus a predetermined
offset. More particularly, the engine control module 52 controls the throttle 16
(Figure 1) via a throttle control signal 64 as a function of gear 62 and engine
speed 58 such that the desired engine speed is achieved. The throttle 16 is
controlled for a predetermine time period. Once the time period expires, the
desired engine speed is gradually adjusted back to a default value and the
throttle is controlled via the throttle control signal 64 accordingly.
[0023] Referring now to Figure 3, a method of turbine offset matching
for deceleration fuel cutoff is shown. The method can be run continually during
engine operation. DFCO enable conditions are evaluated at 100. If the DFCO
mode is desired at 100, control evaluates a timer at 102. If a time since
accelerator pedal tip-out has not expired at 102, engine speed is controlled via
the ETC at 104. More particularly, the throttle is controlled based on gear and
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Attorney Docket No. 8540P-000412
current engine speed such that the ultimate engine speed is near the turbine
speed plus a predetermined offset (e.g., 100 RPM). Control continues to control
the engine speed via the throttle at 104 until the timer expires at 102. When the
timer expires at 102; the throttle is controlled back to a default value at 106.
[0024] Those skilled in the art can now appreciate from the foregoing •
description that the broad teachings of the present disclosure, can be
implemented in a variety of forms. Therefore, while this disclosure has been
described in connection with particular examples thereof, the true scope of the
disclosure should not be so limited since other modifications will become
apparent to the skilled practitioner upon a study of the drawings, specification,
and the following claims.
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Attorney Docket No. 8540P-000412
CLAIMS
What is claimed is:
1. A control system for enabling an engine to operate in a deceleration
fuel cutoff (DFCO) mode, comprising:
an enable module that selectively enables a DFCO mode based on
an accelerator pedal position; and
an engine speed module that regulates engine speed based on
turbine speed during a predetermined time period after the DFCO mode is
enabled.
2. The system of claim 1 wherein the engine speed module regulates
engine speed by commanding a throttle signal based on turbine speed.
3. The system of claim 1 wherein the engine speed module regulates
engine speed based on turbine speed and a predetermined offset.
4. The system of claim 1 wherein the enable module enables the
DFCO mode when the accelerator pedal position indicates the pedal is released.
5. The system of claim 1 wherein the engine speed module regulates
engine speed for the predetermined time period and thereafter, the engine speed
module gradually adjusts engine speed to a default speed.
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Attorney Docket No. 8540P-000412
6. The system of claim 5 wherein the predetermined time period is
based on the accelerator pedal position.
7. The system of claim 1 further comprising:
a torque converter clutch control module that controls pressurized
fluid to the clutch to apply the clutch when engine speed is within a
predetermined range of turbine speed; and
a fuel control module that disables fuel after the torque converter
clutch is applied.
8. The system of claim 1 wherein the engine cpntrol module controls
engine speed as a function of current engine speed and gear.
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Attorney Docket No. 8540P-000412
9. A method for enabling a deceleration fuel cutoff mode of an internal
combustion engine, comprising:
receiving a deceleration fuel cutoff (DFCO) request wherein the
DFCO request is initiated based on an accelerator pedal position;
controlling engine speed based on turbine speed after receiving the
DFCO request;
applying a torque converter clutch when the engine speed is within
a predetermined range of the turbine speed; and
enabling the DFCO mode after the clutch is applied.
10. The method of claim 9 further comprising stopping fuel injection
once the DFCO mode is enabled.
11. The method of claim 9 wherein the controlling comprises controlling
engine speed to be within a predetermined range defined by turbine speed and a
predetermined offset.
12. The method of claim 9 wherein the controlling comprises controlling
engine speed to be equal to turbine speed plus a predetermined offset.
13. The method of claim 9 wherein the controlling engine speed is
performed for a predetermined time period.
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Attorney Docket No. 8540P-000412
14. The method of claim 13 wherein the predetermined time period Is
initiated based on the accelerator pedal position,
15. The method of claim 13 further comprising adjusting engine speed
to a default speed after the predetermined time period expires.
16. The method of claim 9 wherein the controlling further comprises
controlling engine speed by commanding a throttle to adjust airflow to achieve an
engine speed within the predetermined range of turbine speed.
17. The method of claim 9 wherein the controlling further comprises
controlling engine speed by commanding a throttle to adjust airflow to achieve an
engine speed equal to turbine speed plus a predetermined offset
18. The method of claim 9 wherein the controlling further comprises
controlling engine speed as a function of current engine speed and gear.

12

A control system for enabling an engine to operate in a deceleration fuel
cutoff (DFCO) mode is provided. The system includes; an enable module that
selectively enables a DFCO mode based on an accelerator pedal position; and
an engine speed module that regulates engine speed based on turbine speed
during a predetermined time period after the DFCO mode is enabled.

Documents:

00712-kol-2007-abstract.pdf

00712-kol-2007-assignment.pdf

00712-kol-2007-claims.pdf

00712-kol-2007-correspondence others 1.1.pdf

00712-kol-2007-correspondence others 1.2.pdf

00712-kol-2007-correspondence others 1.3.pdf

00712-kol-2007-correspondence others.pdf

00712-kol-2007-description complete.pdf

00712-kol-2007-drawings.pdf

00712-kol-2007-form 1.pdf

00712-kol-2007-form 18.pdf

00712-kol-2007-form 2.pdf

00712-kol-2007-form 3.pdf

00712-kol-2007-form 5.pdf

00712-kol-2007-priority document.pdf

712-KOL-2007-(14-11-2011)-ABSTRACT.pdf

712-KOL-2007-(14-11-2011)-AMANDED CLAIMS.pdf

712-KOL-2007-(14-11-2011)-CORRESPONDENCE.pdf

712-KOL-2007-(14-11-2011)-DESCRIPTION (COMPLETE).pdf

712-KOL-2007-(14-11-2011)-DRAWINGS.pdf

712-KOL-2007-(14-11-2011)-EXAMINATION REPORT REPLY RECIEVED.pdf

712-KOL-2007-(14-11-2011)-FORM 1.pdf

712-KOL-2007-(14-11-2011)-FORM 2.pdf

712-KOL-2007-(14-11-2011)-FORM 3.pdf

712-KOL-2007-(14-11-2011)-FORM 5.pdf

712-KOL-2007-(14-11-2011)-OTHER PATENT DOCUMENT.pdf

712-KOL-2007-(14-11-2011)-OTHERS.pdf

712-KOL-2007-(14-11-2011)-PA.pdf

712-KOL-2007-(19-04-2012)-CORRESPONDENCE.pdf

712-KOL-2007-CORRESPONDENCE OTHERS 1.4.pdf

712-KOL-2007-CORRESPONDENCE.pdf

712-KOL-2007-PA.pdf


Patent Number 255018
Indian Patent Application Number 712/KOL/2007
PG Journal Number 03/2013
Publication Date 18-Jan-2013
Grant Date 15-Jan-2013
Date of Filing 08-May-2007
Name of Patentee GM GLOBAL TECHNOLOGY OPERATIONS, INC
Applicant Address 300 GM RENAISSANCE CENTER DETROIT, MICHIGAN
Inventors:
# Inventor's Name Inventor's Address
1 GORO TAMAI 7532 GLASCOTT, WEST BLOOMFIELD, MICHIGAN 48323
2 WILLIAM L. ALDRICH III 11375 EAGLE ROAD, DAVISBURG, MICHIGAN 48350
3 JAMES L. WORTHING 338, PORTAGE LAKE ROAD, MUNITH, MICHIGAN 49259
4 BIRENDRA P. BHATTARAI 47590 ABERDEEN DRIVE, NOVI, MICHIGAN 48374
PCT International Classification Number F03D11/04; F03D1/00
PCT International Application Number N/A
PCT International Filing date
PCT Conventions:
# PCT Application Number Date of Convention Priority Country
1 11/471,461 2006-06-20 U.S.A.