BACKGROUND AND OBJECTS
[0001] The inventor and his associates at A.E.A. have long been developing engine designs
for ultra-lean combustion. Much of the work is described as "High Swirl Very Low Pollution
Piston Engine Employing Optimizable Vorticity" U. S. Patent #4,344,394. The technology
described in this patent permits engines to be operated at exceptionally lean air/fuel
ratios with efficiency at or approaching that of small autonotive diesels and with
exceptionally low NO
x emissions. In an engine such as that described in Patent #4,344,394 the cylinder-to-cylinder,
cycle-to-cycle, and microscale volume mixing statistics on air/fuel ratio are much
tighter than in the prior art, and the statistical variation of mixture motion inside
the cylinder is also tightened. With such an engine, it has been found that the optimal
fuel economy air/fuel ratio, using the Schweitzer Procedure for determining the true
best economy mixture, occurs at very lean ratios. When the engine is operated richer
than this optimal point, the cyclic variation of flame speed and cyclic variation
of peak pressure observed in the engine is very much less than that characteristic
of prior art engines. It has been. found imperically that the point of optimal fuel
economy (which is nearly the point for minimum NO
x emissions) correlates over the speed load phase space with the onset of significant
statistical variation of flame speed and peak pressure. The statistical variations
of flame speed and peak pressure are not greater than the variations commonly encountered
with ordinary mixtures at stoichiometric or slightly lean ratios, but the statistical
variations can be measured and used as engine control inputs. It is highly desirable
that the engine operate (except at very high loads where rich mixtures are required
to make torque) at air/fuel ratios which are lean enough for a specific range of statistical
variation of flame speed (not misfire), If the air/fuel ratio is controlled to achieve
this borderline roughness, fuel conomy is nearly optimized and NO
x is nearly minimized. The adjustment of air/fuel ratio for borderline Toughness gives
the proper engine adjustment for efficiency and NO
x control regardless of fuel type (e. g. gasoline vs. methanol) or intake air density,
and efficiently compensates for variations in flame stability with internal or external
EGR as a function of speed and load. The roughness control can also compensate for
engine and embient temperature.
[0002] It is therefore a purpose of the present invention to produce a control which reads
a measure of flame speed or peak pressure, and adjusts air/fuel ratio so that the
statistical variation of flame speed (or a reliably correlated measure of flame speed)
achieves a specified degree of statistical variation. If the statistical variation
is smaller than a set value, the control shifcs the air/fuel ratio towards the lean
side where statistical variation of flane speed is increased. f statistical variation
of flame speed, or a measure of it, is excessive the mixture is shifted richer.
[0003] It is impossible to get the dynamic respouse of a roughness combustion cortrol to
be rapid enough to respond to the rapid load changes required for driveability if
the roughness sensor acts alone, However, the roughness sensitive control can input
a relatively slowly moving correction function for a faster automatic control system,
Specifically, the control can continuously update a viriable which multiplies the
air/fuel ratio selected by a more rapid autonomous fuel/air metering controllers.
The automomous fuel/air metering system can be built to respond to variations in speed,
load, etc, and can have very rapid resporse. Therefore the control system of the current
invention uses the roughhness control as a correct or function which adjusts the calibration
of a automatic programmed air/fuel matering system continuously.
[0004] The advantages of NO control and improved efficiency available with enleanment occur
because the leaner mixtures have lower peak flame temperatures and hence lower dissociation
losses and lower NO formation kinetic rates. These same effects can be obtained with
introduction of EGR for a richer air/fuel ratio rather than with enleanment of the
air/fuel ratio itself. It is, therefore, another purpose of the present invention
to produce a control which reads the measure of flame speed or peak pressure and adjusts
EGR input so that the statistical variation of flame speed achieves a specified degree
of statistical variation. Such an EGR control can achieve the same advantages as enleanment
with a super-homogeneous engine operated with in-cylinder flow control. The EGR control
can also be useful as a drivability control for more conventional engines, and can,
therefore, be applied to EGR controls on current vehicles as well as to EGR introduction
to better-mixed systems.
[0005] A number of measures of flame speed, and hence cyclic variation of flame speed, are
available. One can read the peak acoustic pressure at each exhaust blowdown since
this peak pressure correlates inversely with flame speed. Another convenient measure
of flame speed is the ionization resistance at the spark gap on refiring the plug
20 or 30 degrees after the initial ignition. Whichever combustion measure is chosen,
the control system functions by taking a running total of a flame speed measure and
controlling air/fuel ratio to adjust the flame speed measure variance to a set value.
[0006] Applied to an engine such as the ultra-homogenous variable restriction flap engine
of Patent #4,344,394 a roughness sensor control superimposed on a rapid response fuel/air
metering system or EGR introduction system serves to optimize NO
X and other emissions, maximize fuel efficiency, and compensate for variations in fuel,
altitude, temperature and other variables.
IN THE DRAWINGS
[0007]
Figure 1 illustrates the variation of efficiency versus fuel/air ratio for the constant
volume fuel/air cycle. (Source: Figure 0-2, The Internal Combustion Engine in Theory
and Practice, Volume 2, C. F. Taylor, MIT Press, 1969.)
Figures 2a and 2b illustrate the variation in peak pressure and flame speed which
is characteristic of spark-fired engines under different conditions. Figure 2a illustrates
combustion in an engine with typical mixing and lean combusion. Figure 2b shows operation
of the engine under similar conditions but with rich combustion. (Source: The Internal
Combustion Engine in Theory and Practice, Volume 2, op cit, Figure 1-18 taken in turn
from Soltan, "Cylinder Pressure Variations in Petrol Engines," Institution of Mechanical
Engineers [London Proceedings of the Automobile Division, 1960-1961, #2, Page 99].)
Figure 2c sketches the very small variation in flame speed typical of the fluidic
port ultra-homogeneous engine under conditions richer than optimal conditions.
Figure 3 illustrates by analogy the reason statistical variation of flame speed penalizes
efficiency. (Source: The Internal Combustion Engine in Theory and Practice, Volume
1, op -cit, Figures 12-14.)
Figure 4 shows the dependence of NOX emissions in grams per indicated horsepower hour on equivalence ratio (fuel/air ratio)
for the variable restriction port ultra-homogeneous engine.
Figures 5, 6 and 7 show schematically a fuel/air metering system intended to supply
an ultra-lean engine, and shows the manner in which the roughness control enters into
the overall fuel/air control scheme.
Figure 8 is an illustration of an internal combustion engine, shown schematically
with a microphone pickup which inputs an exhaust pressure signal to the controller.
Figure 9a shows pressure in an exhaust manifold under conditions where the engine
is operating smoothly and the variation in peak blowdown pressure is small (flame
speed variation is small). Figure 9b shows the pressure curve which occurs when blowdown
pressure varies (flame speed varies).
Figure 10 is a schematic showing the algorithm whereby the signal from the sensor
exhaust microphone is used for combustion control.
Figure lla is a schematic of an engine and ignition system with the ignition system
adapted to fire the spark again 30° after the ignition firing to provide an ionization
probe signal to measure flame speed. Breakdown voltage at the second firing correlates
reliably with flame speed.
Figure llb is a sketch of the ignition wire voltage curve which is characteristic
of low statistical variation of flame speed. Figure lie is a sketch of the wire ignition
voltage which is characteristic of relatively rough combustion.
Figure 12 is a schematic analogous to the schematic of Figure 10 where the input is
ionization breakdown voltage measured as shown above.
Figure 13a and 13b are schematics of an engine with an EGR control system where EGR
supply is a function of an automatic programming with engine variables, with a continuously
updated bias controlled by a roughness control.
Figure 14 is a schematic analogous to the schematic of Figure 12 wherein the roughness
controller adjusts the setting of an electronically controlled EGR system rather than
adjusting air/fuel ratio.
DETAILED DISCUSSION
[0008] Figure 1 illustrates the variation of efficiency versus equivalence ratio (fuel/air
ratio at stoichemetric ÷ fuel/air ratio actual) for the constant volume fuel/air cycle.
(Source: Figure 0-2 The Internal Combustion Engine in Theory and Practice, Volume
II, C. F. Taylor, MIT Press, 1968.) Figure 1 illustrates the thermodynamic advantages
of lean combustion so long as the constant volume cycle can be approximated. The constant
volume cycle assume instantaneous combustion at top dead center, but can be adequately
approximated even for combustion durations of 40 or 50 crank degrees so long as the
combustion process is timed so that the bulk of the combustion happen: near top dead
center. The indicated efficiency of an engine with excellent mixing and complete combustion
can be reasonably close to that of the fuel/ai cycle so long as flame speeds are adequate
and variations of flame speed fron cycle to cycle are relatively small.
[0009] Figures 2a and 2b illustrate the variation in peak pressure and flame speed which
is characteristic of typical current art spark-fired engines unde different mixture
conditions. Figure 2a illustrates combustion in an engine with typical mixing at 2000
rpm with a compression ratio of 9 at an equivalence ratio of .82, which is considered
a relatively lean ratio for typical engine combustion. It can be seen that there are
rather substantial variations in peak pressure characteristic of these lean mixtures.
These pea combustion variations produce significant efficiency decrements and perceptible
engine vibration. (Source for both Figure 2a and 2b: The Internal Combustion Engine
in Theory and Practice, Volume 2, op cit, Figure 1 18 taken in turn from Soltan, "Cylinder
Pressure Variations in Petrol Engines," Institution of Mechanical Engineers [London
Proceedings of the Automobile Division, 1960-1961, #2, Page 99].) Figure. 2b shows
operation of the same engine at the same rpm but with a rich equivalence ratio of
1.25 showing the cyclic variation which is characteristic of typical art engines when
operated rich. The degree of cyclic variation of flame speed characteristic of the
ultra-homogeneous engine when operated under optimal conditions is approximately equal
to the statistical variation in peak pressure shown in Figure 2b. Figure 2c sketches
the very small variation in flame speed typical of the fluidic port ultra-homogeneous
engine under conditions richer than optimal conditons. Under these relatively rich
conditions (which may be as lean as an equivalence ratio of .6) cyclic variation of
peak pressure is barely perceptible. Invariably it is found that the optimal efficiency
point occurs at a point where statistical variation of peak pressure and flame speed
has become significant. This is the point where the losses due to heat release away
from top dead center due to statistical variation about the mean optimal spark timing
balance the additional thermodynamic advantages of enleanment which were illustrated
with respect to Figure 1.
[0010] Figure 3 illustrates by analogy the reasons statistical variation of flame speed
penalizes efficiency. The figure plots the correlation of brake mean effective pressure
(a normalized torque measure) versus spark-advance deviation from the best torque
spark advance. (Source: The Internal Combustion Engine in Theory and Practice, Volume
I, op cit, Figure 12-14.) Investigation of the curve of Figure 3 shows that the decline
in efficiency is approximately proportional to the 1.8 power of spark timing deviation
from its optimal value. It happens that the great bulk of the statistical variation
in flame speed occurs in the first two percent of combustion pressure rise, so that
statistical variation of flame speed is, in effect, a random variation in spark timing
from cycle to cycle on a hypothetical engine where flame speed is otherwise constant.
The efficiency penalty for flame speed variance is therefore roughly proportional
to the 1.8 power of the variance. A small degree of flame speed and peak pressure
variation consequently does relatively little harm but the efficiency penalty with
flame speed variance increases almost as the square of the variance. With this in
mind, it should be easy t understand why the optimal efficiency point for a very homogeneous
and fluid- mechanically reproducible engine will occur at a very lean point where
the trade-off between statistical variation of flame speed and the inherent thermodynamic
advantage of further enleanment balances.
[0011] Figure 4 shows the dependence of NO emissions in grams per indicated horsepower hour
on equivalence ratio for a variable restriction port ultra-homogeneous engine described
in Patent #4,344,394. Much of the data from Figure 4 is also shown in Figure 60 of
Patent #4,344,394, but the figure also includes data from a 2.3 litre Ford engine
operated with a vortex and fluidic ports on gasoline. The performance of both the
single cylinder engine and th< Ford engine was such that the optimal efficiency occurred
at equivalence ratios in the range of .6 stoichemtric and leaner. This result was
typical over a wide range of speeds and loads. At the optimum fuel economy ratios,
NO
x is quite low. By controlling the equivalence ratio to achieve a specifiec level of
cyclic variation it is possible to approximate closely the optimal fuel economy and
minimum NO for the entire engine phase space of speeds and loads.
[0012] Figures 5, 6, and 7 show schematically a fuel/air metering system intended to meter
fuel and air to an ultra-lean engine such as that described in Patent #4,344,394 and
shows the manner in which the roughness control enters in to the overall fuel/air
control scheme. Figure 5 shows schematically fuel flow across the slotted valve 3
controlled by a solenoid servo valve 8, 9 which supplies the engine. The pressure
differential across the slotted valve is called ΔP fuel. Figure 6 shows an air throttle
linked mechanically and with coefficients of discharge matched to the slotted fuel
valve of Figure 5 and shows an air pressure transducer to pressure ΔP air across the
air throttle. Figure 7 shows the fuel/air control system schematically. A measured
A P air inputs into a computer which computes a ΔP fuel desired as the product of
an automatically programmed function (in terms of ΔP
air' r
pm, etc.) times a servo correction coefficient which is adjusted to bias the control
system to the proper degree of cyclic variation in flame speed. Once the computer
specifies the Δ P fuel desired, an analog servo controls the voltage on the servo
solenoid valve of Figure 4 until ΔP fuel measured = A P fuel desired. This equilibrium
process occurs in about ten milliseconds. The cyclic time of the computation process
shown in Figure 7 can vary, but it can be made very fast. The fuel/air metering system
of Figures 5, 6 and 7 is automatic and has very rapid response, but has its fuel/air
metering calibration adjusted continuously by the roughness sensor servo control.
This roughness sensor servo control can update the servo correction coefficient once
every exhaust blowdown or once every combustion event.
[0013] Figure 8 is an illustration of an internal combustion engine, shown schematically
with a microphone pickup which inputs an exhaust pressure signal to the controller.
Peak exhaust blowdown pressure is a useful measure of flame speed and variation in
peak blowdown pressures measures flame speed variation. It is not necessary that the
exhaust pressure microphone be located in the position shown in Figure 8, and indeed
it may be desirable to place the microphone in a much cooler passage (for example,
in the exhaust passage downstream of a mixing vortex, in a position where the exhaust
gas has been much'cooled).
[0014] Figure 9a shows pressure in an exhaust manifold under conditions where the engine
is operating smoothly and the variation in peak blowdown pressure is small (flame
speed variation is small). An engine with the ultra-homogeneous characteristics of
the engine of Patent #4,344,394 would be operating too rich if it had an exhaust pressure
pulse wave form such as this (unless the engine was operated at such a high torque
demand that enrichment of the mixture was inescapable because of engine airflow limits).
Figure 9b shows the pressure curve which occurs when blowdown pressure varies (flame
speed varies).
[0015] Figure 10 is a schematic showing the algorithm whereby the signal from the exhaust
microphone is used for combustion control. The drawing is largely self-explanatory.
The exhaust pressure signal from the sensor microphone is compressed by a logarithmic
compression circuit for electronic convenience and an electrical circuit is arranged
to hold the peak voltages which correspond to the exhaust blowdown pressure. These
peak voltages are read with an analog to digital converter and thereby converted to
numbers. The computer keeps a running total of the last 16 blowdown peak pressure
numbers in the normal way, where the last blowdown number enters the summation and
the 17th is dropped out on a continous update basis. After each blowdown the computer
compares the last blowdown number with the running total blowdown average, and makes
the following decisions. If the last blowdown number varies by more than a specified
value from the average of the previous 16 values, the roughness control adjusts the
roughness coefficient in Figure 7 to enrich the mixture. If the blowdown pressure
number falls within the specified limits, the circuit adjusts the control coefficient
in Figure 7 to enlean the mixture. The slew rate lean should typically be much slower
than the slew rate rich (perhaps a tenth as fast) since the penalty for excessive
enleanment may be misfire, whereas the penalty for excessive richness is only an NO
emission penalty in an engine characterized by low NO emissions. It should be clear
to those skilled in the servo mechanical arts that the slew rates lean and rich and
the numerical values of A and B are variables which may be adjusted by the designer
as he optimizes the system.
[0016] The system is also subject to a number of overrides, as follows: 1) Cranking override
- if blowdown frequency is less than 6 cycles per second and greater than 0 cycles
per seconds, slew rich for starting. 2) Deceleration fuel shut-off override - if rpm
is greater than 600 and there is neglible blowdown pressure (engine not firing) no
slew rate either rich or lean and no slew for the first 10 to 20 blowdowns after firing
resumes. 3) Cold enrichment override - once slew rate rich to increase with decreasing
sensor temperature below approximately 10°C (slew may double every 10°C thereafter).
[0017] Those skilled in the servo-mechanical arts will recognize that a number of the variables
set out above can be changed if this is convenient. A and B, the upper and lower percentage
variation threshholds for enrichening, are variable. The number of entries in the
running total can be varied. The slew rates lean and rich can be varied and the variation
of slew rate with temperature is also variable.
[0018] The roughness combustion control system can be very similar if its input is another
measure of flame speed. An extremely convenient measure of flame speed is the ionization
resistance of the combustion gases measured a specified time or specified number of
crank degrees after ignition. This may be measured by firing the spark plug a second
time a set number of crank degrees (say 30 crank degrees) after the ignition firing.
The spark plug gap will at this time be inside a cloud of post-flame combustion gases,
and the ionization breakdown voltage will be less than a hundredth that required for
ignition itself. This ionization breakdown voltage is a strong function of temperature
and pressure. Therefore variation of this breakdown voltage can serve as the input
for the combustion roughness control. To illustrate this Figure lla is a schematic
of an engine and ignition system with the ignitior system adapted to fire the spark
plug a second time 30 degrees after the ignition firing to provide an ionization probe
signal to measure flame speed
[0019] Figures llb and lie sketch the wire voltage traces from a system such a that of Figure
11a. Only the ionization breakdown voltages are shown. When the spark fires 30° after
ignition, the breakdown voltage is very much less than that required of the ignition
spark. This breakdown voltage is a function of the ionization temperature and pressure
in the spark gap, and varies sensitively with flame speed. Because the bulk of the
flame speed variation occurs in the first 10°-20° after the spark, the temperature
and pressure in the spark gap at the time of ionization signal sparking 30° afte ignition
will vary sensitively with variations in flame speed and the breakdown voltage signal
will therefore be a convenient measure of flame spe and variation. Figure llb is a
sketch of the wire voltage curve which is characteristic of low statistical variation
of flame speed. Figure llc is a sketch of the wire voltage curve trace which is characteristic
of relatively rougher combustion. In both cases, the ionization measuring voltages
can easily be distinguished from the much higher ignition spark voltages.
[0020] Referring again to Figure lla, the schematic shows two potential pick-u for the plug
(the plug is the signal fed into the controller). In the one case, the central distributor
wire to the coil is used for the pick-up. In this case, an ionization voltage signal
is obtained from each spark plug in each cylinder. Alternatively, the voltage pick-up
can occur on only one spark plug, as is also illustrated in lla. If the plug signal
comes directly from the coil, an ionization breakdown signal will go the controller
with every combustion event in the engine. However, it will be necessary for the controller
to compensate for the variations in ionization breakdown voltage which are functions
of plug gap geometry from plug to plug. If voltage breakdown is only taken from a
single plug, this additional statistical complexity need not be handled, but the slew
rate of the controller must be slower for stability, and the controller only reads
variation from a small sequential sample of combustion events.
[0021] Figure 12 is a schematic analogous to the schematic of Figure 10 where the input
is ionization breakdown voltage measured as shown above. The comments applicable to
discussion of Figure 10 are applicable to Figure 12. The ignition breakdown method
has some conveniences, and is particularly adaptable to the transistorized ignitions
which are coming to dominate much of the automotive market. The spark plug itself
is an available sensor, and breakdown voltage on each spark plug can be measured.
However, breakdown voltage will be proportional to the square of the spark gap, and
if the system is used to adapt to each of the cylinders, a slow moving running total
coefficient for breakdown voltage on each of the spark gaps must be built into the
computer so that breakdown variations accountable from spark gap variations from cylinder
to cylinder are not counted as variance of flame speed within the algorithm. Those
skilled in the computer arts should find it clear how to do this.
[0022] In an engine intended to run with complete homogeneity, tightly controlled fluid
mechanics and ultra-lean combustion, the optimal fuel economy point at all speeds
and loads is the air/fuel ratio for a small but perceptible degree of combustion variance.
The combination of a combustion control which controls air/fuel ratio to this degree
of variance with an autonomous rapid response fuel/air metering system, as illustrated
in Figures 5, 6 and 7, produces optimization of economy and emission minimization
in combination with a system having extremely rapid dynamic response.
[0023] The arguments above for controlling charge dilution in a homogeneous engine via enleanment
are equally applicable under the same homogeneous conditions if the dilution of the
mixture which suppresses peak flame temperature is achieved via EGR introduction,
so long as the overall air/fuel ratio is lean enough to control carbon monoxide. There
are currently on the market a number of EGR controls where the EGR supply to the engine
is controlled in an automatic fashion as a function of air pressure drops, rpm, temperature
and other inputs. The roughness control logic described above can be adapted straightforwardly
to serve as a continuously updated biasing correction function for such EGR systems.
Figure 13a shows schematically an engine with an EGR control. Figure 13b illustrates
in block diagram form the application of the combustion roughness servo logic to such
an EGR control system. The EGR valve position is controlled as a function of automatic
inputs, including Pair,
rp
m, etc., and is varied by a slowly-moving correction function from the combustion servo,
which is continuously updated as before. The combined effect of the automota fast
response programming and the slowly-moving combustioned servo correction function
produces the actuator position which controls EGR flow. Figure 14 blocks out the control
algorithm for such an EGR controller, utilizing spark plug firing as the input measure
of combustion variability. Comments applicable to Figure 12 and Figure 10 are applicable
here. A similar algorithm utilizing an exhaust pressure microphone as the combustion
variability signal can be produced.
Claim 1: Control apparatus for obtaining a measure of flame speed in the combustion
chamber of an internal combustion engine and based on said measure adjusting air/fuel
ratio apparatus so that the variation of flame speed falls within a specified degree
of statistical variation, said apparatus comprising means for obtaining said measure
of flame speed on each burn cycle of the engine and producing an electric signal representative
thereof, means for storing in succession the peaks of said electric signals, means
for converting the signal peaks to a plurality of numbers corresponding respectively
to said signal peaks, computer means for averaging the said numbers for a given quantity
of successive cycles and comparing said average with the last received signal peak
number and means for comparing the number average and that of the last received signal
peak to produce a difference and acting on the air/fuel ratio apparatus to enlean
the mixture if the difference is within designated limits and acting to enrich the
mixture if the difference is outside the designated limits whereby the air/fuel mixture
is adjusted so that the flame speeds of the burn cycles will fall within a specified
degree of statistical variation.
Claim 2: The invention as set forth in Claim 1 and wherein the measure of flame speed
of each burn cycle comprises means for sensing peak exhaust blowdown pressure.
Claim 3: The invention as set forth in Claim 1 and wherein the measure of flame speed
of each burn cycle comprises means for measuring the ionization resistance of the
combustion gases at a specified time after ignition by refiring the spark plug.
Claim 4: The invention as set forth in Claim 1 and wherein the measure of flame speed
is not obtained for each burn cycle, but only for a selected sequence of burn cycles.
Claim 5: ' A method of adjusting air/fuel ratio apparatus so that the statistical
variation of flame speed in an internal combustion engine from cycle-to-cycle will
fall within a specified degree of statistical variation, said method comprising the
steps of:
1. Obtaining a measure of flame speed of each successive burn cycle in the combustion
chamber of the engine,
2. Producing an electric signal representative of this measure of flame speed of each
cycle.
3. Storing in'succession the peak of the electric signals,
4. Converting the signal peaks to numbers corresponding respectively to said signal
peaks,
5. Averaging the numbers representing the signal peaks for a specified number of successive
cycles,
6. Comparing said average number with that of the last received signal peak number
to determine a difference,
7. Enleaning the air/fuel mixture if the difference is within specified limits and
enriching the air/fuel mixture if the difference is outside specified limits whereby
the air/fuel mixture is adjusted so that the statistical variation in cycle-to-cycle
burn rates falls within a specified range.
Claim 6: A method of adjusting an engine EGR control apparatus so that the statistical
variation of flame speed in an internal combustion engine from cycle-to-cycle will
fall within a specified degree of statistical variation, said method comprising the
steps of:
1. Obtaining a measure of flame speed of each successive burn cycle in the combustion
chamber of the engine,
2. Producing an electric signal representative of this measure of flame speed of each
cycle.
3. Storing in succession the peak of the electric signals,
4. Converting the signal peaks to numbers corresponding respectively to said signal
peaks,
5. Averaging the numbers representing the signal peaks for a specified number of successive
cycles,
6. Comparing said average number with that of the last received signal peak number
to determine a difference,
7. Increasing the EGR supply rate if the difference is within specified limits and
decreasing the EGR supply rate if the difference is outside specified limits whereby
the air-fuel-EGR mixture is adjusted so that the statistical variation in cycle-to-cycle
burn rates falls within a specified range.
Claim 7: The invention as set forth in Claim 1 and wherein the measure of flame speed
of each burn cycle comprises means for sensing peak exhaust blowdown pressure.
Claim 8: The invention as set forth in Claim 1 and wherein the measure of flame speed
of each burn cycle comprises means for measuring the ionization resistance of the
combustion gases at a specified time after ignition by refiring the spark plug.
Claim 9: The invention as set forth in Claim 1 and wherein the measure of flame speed
is not obtained for each burn cycle, but only for a selected sequence of burn cycles.