Background of the Invention
1. Field Of The Invention
This invention relates generally to a method and apparatus for controlling an internal combustion engine, and more particularly to a microprocessor-based electronic engine control system having a memory preprogrammed with various control laws and control schedules responsive to one or more sensed engine-operating parameters and generating signals for controlling fuel injection, ignition timing, EGR control, and the like.
2. Statement Of The Prior Art
Many of the patents of the prior art recognize the need for employing the enhanced accuracy of digital control systems for more accurately controlling one or more functions of an internal combustion engine.
U.S. Pat. No. 3,969,614 which issued to David F. Moyer, et al on July 13, 1976 is typical of such systems as are U.S. Pat. No. 3,835,819 which issued to Robert L. Anderson, Jr. on Sept. 17, 1974; U.S. Pat. No. 3,904,856 which issued to Louis Monptit on Sept. 9, 1975; and U.S. Pat. No. 3,906,207 which issued to Jean-Pierre Rivere, et al on Sept. 16, 1975. All of these Patents represent a break-away from the purely analog control systems of the past, but neither the accuracy, reliability, or number of functions controlled is sufficient to meet present day requirements.
Future internal combustion engines will require that emissions be tightly controlled due to ever-increasing governmental regulations, while fuel consumption is minimized and drivability improved over the entire operating range of the engine. None of the systems of the prior art provide a method and apparatus for controlling the operation of an internal combustion engine over even a portion of its operating range with sufficient accuracy to attain minimal emissions and minimal fuel consumption while simultaneously obtaining improved drivability.
The systems of the prior art attempt to control one or more of the engine-operating functions but none attempts to control the operation of the fuel pump, fuel injection, engine ignition timing, on-off and/or proportional EGR control, and the like while using feedback from such devices as oxygen sensors for emission control purposes or for effecting a closed loop fuel control mode of operations, yet including provisions for optimizing acceleration enrichment handling, and the like. Moreover, the systems of the prior art are extremely expensive, difficult to repair and maintain and are not commercially feasible at the present time.
These and other problems of the prior art are solved by the microprocessor-based electronic engine control system of the present invention which eliminates most or all of the problems of the prior arts and enables a commercially feasible implementation of a digital control system having a relatively low cost, and which is easy to repair and maintain. The system of the present invention is able to implement much more advanced and complex fuel control laws and expand on the number of control functions performed thereby to include the timing and duration of ignition, on-off and/or proportional EGR control and the like while at the same time reducing the cost and size of the unit and increasing reliability so as to render the system commercially feasible.
These and other objects and advantages of the present invention will be accomplished by the present method and apparatus for the microprocessor-based electronic engine control of nearly all engine functions over the entire operating range of the engine to minimize engine emissions and fuel consumption while simultaneously maintaining, if not improving, drivability and the like.
Summary of the Invention
The method and apparatus of the present invention includes means for detecting a need for acceleration enrichment and generating a reliable initial acceleration enrichment pulse, commonly called a Tip-In pulse, followed by an additional acceleration enrichment amount determined at least partially as a function of engine speed and the like to augment the main fuel pulse.
The additional acceleration enrichment amount is determined as a One Factoral enrichment of the primary main fuel pulse T.sub.p (N) computed for normal fuel injection purposes.
If T.sub.p (N) is the duration of the normal main or primary fuel pulse, T.sub.p (AE) is the duration of the total fuel pulse after an acceleration enrichment correction is factored in and "K" is the factoral enrichment factor, then T.sub.p (AE)=T.sub.p (N).times.(1+K).
The factoral enrichment factor "K" is a function of engine speed (RPM), air temperature and a decay factor where the decay factor is a modifier value addressed by the number of engine revolutions which have elapsed since the initiation of the acceleration enrichment enable sequence began. Therefore, K=K.sub.RPM +K.sub.AIR TEMP +K.sub.DECAY.
The present system ensures that if the acceleration enrichment Tip-In pulse is generated during the period of a previously-computed mean or primary fuel pulse, then the Tip-In pulse is delayed until the termination of the main fuel pulse and then immediately added to prolong the period of the fuel pulse to ensure that the one-time extra acceleration enrichment boost of fuel is not masked or lost during the main fuel pulse. Otherwise, the Tip-In pulse is immediately generated to provide an immediate one-time additional boost of fuel to compensate for acceleration enrichment.
A unity intercept concept is used for defining various breakpoints in the required look-up table of values stored in the memory so as to permit the use of a process for interpolating between two address values X1 and X2 to compute an overall modifier value or correction factor to be applied during fuel pulse calculation which corresponds to the actual input variable X, and at the end of the computed interpolation, the overall correction factor is compared with a level of "one" and the highest of the two, i.e., the computed correction factor or the value "1" is the only number used as the table output correction factor or value for computation purposes. With this approach, any threshhold level and any number of breakpoints between successive addressable values X1, X2 may be used regardless of limitations on the number of memory addresses available.
Brief Description of the Drawings
FIG. 2 is a block diagram of the microprocessor-based electronic engine control system.
Incorporation by Reference
This application is one of fourteen applications filed on Feb. 27, 1978, all commonly assigned and having substantially the same specification and drawings, the fourteen applications being identified below:
Application Ser. No. 881,321, has been printed in its entirety, including FIGS. 1 to 10.34 and the specification of that application is specifically incorporated by reference.