Patent Grant
6843229
The present invention relates to engine control systems, and more particularly to fault indication in displacement on demand engine control systems.
Some internal combustion engines include engine control systems that deactivate cylinders under low load situations. For example, an eight cylinder can be operated using four cylinders. Cylinder deactivation improves fuel economy by reducing pumping losses. To smoothly transition between activated and deactivated modes, the internal combustion engine should produce torque with a minimum of disturbances. Otherwise, the transition will not be transparent to the driver. Excess torque causes engine surge and insufficient torque causes engine sag, both of which degrade the driving experience.
For an eight-cylinder engine, intake manifold pressure is significantly lower during eight-cylinder operation than during four-cylinder operation. During the transition from eight to four cylinders, there is a noticeable torque reduction or sagging in four-cylinder operation until the intake manifold reaches a proper manifold pressure level. In other words, there is less engine torque when cylinders are deactivated than when the cylinders are activated for the same accelerator position. The driver of the vehicle would be required to manually modulate the accelerator to provide compensation for the torque reduction and to smooth torque.
In commonly-owned U.S. patent application entitled “Engine Control System With Throttle Preload During Cylinder Deactivation”, Ser. No. 10/150,522, filed May 17, 2002, which is hereby incorporated by reference in its entirety, the throttle limit is adjusted to an increased position prior to cylinder deactivation to provide compensation. In “Spark Retard Control During Cylinder Transitions in a Displacement on Demand Engine”, Ser. No. 10/150,879 filed May 17, 2002, which is hereby incorporated by reference in its entirety, the increased throttle position or preload is accompanied by spark retard to offset torque increase caused by the preload before the cylinders are deactivated.
The present invention provides an engine control system for monitoring torque increase during cylinder deactivation for a displacement, on demand (DOD) engine including activated and deactivated modes. The engine control system includes a throttle and a controller. The controller adjusts a preload of the throttle prior to a transition to the deactivated mode and determines whether a DOD fault is present during the cylinder deactivation event. The controller one of operates the engine without the preload in the deactivated mode and switches to the activated mode if the fault is present for a predetermined time.
In one feature, the controller cancels the preload if the DOD fault is present and resets the preload if the predetermined period has not expired.
In another feature, the controller retards spark based on the preload prior to the transition to the deactivated mode.
In another feature, an indicator receives a DOD fault signal from the controller after the predetermined time period expires to indicate the presence of the DOD fault.
In still another feature, the preload is based on a desired throttle position for the deactivated mode.
In yet another feature, the DOD fault is an engine speed fault. An engine speed sensor generates an engine speed signal that is processed by the controller to determine whether the engine speed fault is present.
In yet another feature, the DOD fault is a transmission gear fault. A transmission sensor generates a signal based on a current transmission gear that is processed by the controller to determine whether the transmission gear fault is present.
In yet another feature, the DOD fault is a fueled cylinder fault. A fuel supply sensor generates a fuel supply signal that is processed by the controller to determine whether the fueled cylinder fault is present.
Further areas of applicability of the present invention will become apparent from the detailed description provided hereinafter. It should be understood that the detailed description and specific examples, while indicating the preferred embodiment of the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention.
The present invention will become more fully understood from the detailed description and the accompanying drawings, wherein:
The following description of the preferred embodiment(s) is merely exemplary in nature and is in no way intended to limit the invention, its application, or uses. For purposes of clarity, the same reference numbers will be used in the drawings to identify similar elements.
As used herein, activated refers to engine operation using all of the engine cylinders. Deactivated refers to engine operation using less than all of the cylinders of the engine (one or more cylinders not active). Furthermore, the exemplary implementation describes an eight cylinder engine with cylinder deactivation to four cylinders. However, skilled artisans will appreciate that the disclosure herein applies to cylinder deactivation in engines having additional or fewer cylinders such as 4, 6, 10, 12 and 16.
Referring now to
A throttle position sensor generates a throttle position signal that is sent to the controller 12. A temperature sensor 34 generates an intake manifold temperature signal that is sent to the controller 12. An engine speed sensor 36 generates an engine speed signal that is sent to the controller 12. A transmission sensor 38 generates a gear signal that is sent to the controller 12. The gear signal indicates the current gear in which the transmission 17 is operating. The controller 12 receives a signal from the fuel injection system 20 indicating the number of cylinders 18 currently fueled.
The controller 12 monitors the various sensors described herein to determine whether cylinder deactivation is appropriate. This deactivation decision is based on engine load. If the engine load is sufficiently light, a select number of cylinders 18 are deactivated and the power output of the remaining or activated cylinders 18 is increased. The controller 12 determines a throttle preload prior to transitioning to the deactivated mode. The throttle preload is based on a desired throttle position during cylinder deactivation. That is to say, the throttle preload is based on the throttle position required to increase the power output of the activated cylinders.
Prior to transitioning into the deactivated mode, the controller 12 retards engine spark based on the throttle preload. The throttle preload is accompanied by the spark retard to offset torque increase caused by the preload before the cylinders are deactivated. Once transition to the deactivated mode is complete the spark retard is reduced. Smoothing of the transition to the deactivated mode is performed using spark retard with the throttle preload.
Prior to completing the transition to the deactivated mode, the controller 12 monitors the various sensors for the presence of a DOD fault. The DOD fault includes but is not limited to the following: torque increase, gear state and fueled cylinders. Torque increase can be determined in a number of manners including engine speed change. A detailed discussion of the manners in which torque increase can be determined is found in U.S. Ser. No. 10/368,895 filed Feb. 18, 2003 and entitled “Displacement On Demand with Throttle Preload Security Methodology”, the disclosure of which is expressly incorporated herein by reference in its entirety. With regard to engine speed change, the controller 12 monitors the engine speed sensor signal to determine whether the engine speed change is within a threshold. If the engine speed change is within the threshold, torque increase is not detected. If the engine speed change is above the threshold torque increase is detected and the controller signals a fault.
The gear state is determined by the transmission sensor 38. The controller 12 identifies the current transmission gear. If the gear is not one in which deactivation is allowed, the controller 12 signals a fault. Similarly, the controller 12 process the fuel injection system signal to determine the number of cylinders 18 that are fueled. If the number of cylinders 18 fueled is not equal to the number of cylinders 18 that are to be fueled in the deactivation mode, the controller 12 signals a fault.
If a fault has been signaled during transition to the deactivated mode, the controller 12 cancels the throttle preload and determines whether a predetermined number of transition attempts to the deactivated mode have occurred. If the result is false, the controller 12 cancels the present transition and determines the throttle preload. If the result is true, the controller 12 signals an engine error and finishes transition to the deactivated mode and operates the engine 16 without the throttle preload. The engine error can be indicated using audio and/or on a visual indicator 40 such as a check engine lamp. Additionally, the engine error sets a flag in the controller 12 that corresponds to the particular DOD fault. The flag can be read by maintenance personnel during inspection of the vehicle. As a result, the maintenance personnel can correct the fault.
Referring now to
Control monitors the signals of the various sensors to determine whether a DOD fault is present. In step 112, control monitors the engine speed change to determine if it is within the threshold. If step 112 is false, control signals a fault in step 114. If step 112 is true, control loops to step 116. In step 116, control determines whether the transmission gear is correct. If step 116 is false, control signals a fault in step 118. If step 116 is true, control loops to step 120. In step 120, control determines whether the number of fueled cylinders is correct for the deactivation mode. If step 120 is false, control signals a fault in step 122. If step 120 is true, control loops to step 124.
In step 124, control determines whether a DOD fault has been signaled. If step 124 is false, control completes transition into the deactivated mode in step 126. The engine operates in the deactivated mode with the throttle preload. If a DOD fault has been signaled, control cancels the throttle preload in step 128. In step 130, control determines whether the counter is greater than a threshold value. In other words, control determines whether a transition into the deactivated mode has been attempted at least a threshold number of times. If step 130 is false, control loops back to step 104, which cancels the transition into the deactivated mode and increments the counter in steps 132 and 134, respectively. If step 130 is true, control signals an error based on the particular DOD fault in step 136. The error signal enables the passenger or maintenance personnel to determine the nature of the DOD fault so remedial action can be taken. In step 126, control completes transition into the deactivated mode operating the engine without the throttle preload.
Operation of the engine 16 without the throttle preload may increase engine instability that may be felt by the vehicle occupant. When examining the vehicle for the cause of the engine instability, the error indicator or error flag informs the maintenance personnel of the source of the DOD fault. The maintenance personnel correct the error and reset the error indicator and error flag.
Referring now to
Those skilled in the art can now appreciate from the foregoing description that the broad teachings of the present invention can be implemented in a variety of forms. Therefore, while this invention has been described in connection with particular examples thereof, the true scope of the invention should not be so limited since other modifications will become apparent to the skilled practitioner: upon a study of the drawings, the specification and the following claims.
| Number | Name | Date | Kind |
|---|---|---|---|
| 6381953 | Glugla et al. | May 2002 | B1 |
| 6499449 | Michelini et al. | Dec 2002 | B2 |
| 6615804 | Matthews et al. | Sep 2003 | B2 |
| 6647947 | Boyer et al. | Nov 2003 | B2 |
| 6684151 | Ring | Jan 2004 | B1 |
| 20030213466 | Rayl | Nov 2003 | A1 |
| Number | Date | Country | |
|---|---|---|---|
| 20040255905 A1 | Dec 2004 | US |
