Field of the Invention
[0001] This disclosure concerns an invention relating generally to combustion methodologies
for internal combustion engines, and more specifically to combustion methodologies
resulting in decreased pollutant emissions.
Background of the Invention
[0002] For better understanding of the invention described in this document, it is initially
useful to review basic principles of internal combustion engine structure and operation.
FIG.1 depicts a cylinder in a simple idealized internal combustion engine
100, including a combustion chamber
102 defined between a piston
104 and a cylinder head
106. The cylinder head
106 includes a fuel injector
108 and a pair of combustion chamber valves, an intake valve
110 for intake of air from an intake manifold
112, and an exhaust valve
114 for exhaust of combustion products to an exhaust manifold
116 and exhaust system. As is well known, the engine
100 operates by engaging in a combustion cycle, wherein fuel is burned in the combustion
chamber
102 to expand the gases (primarily air) therein and drive the piston
104. The piston
104 in turn drives a crank
118 associated with the piston
104, with the crank
118 in turn driving the crankshaft (not shown) which provides power output for a vehicle
drive train or to other structures for transmitting mechanical power. The classical
four-stroke combustion cycle for both SI (spark ignition or gasoline) engines and
CI (compression ignition or diesel) engines involves the following steps:
- (1) An intake stroke, wherein the intake valve 110 is opened while piston 104 retreats from cylinder head 106 to draw air into the combustion chamber 102 from the intake manifold 112.
- (2) A compression stroke, wherein the piston 104 approaches cylinder head 106 with the combustion chamber valves 110 and 114 closed (at least during the latter portion of the stroke).
- (3) A power or expansion stroke, wherein fuel injected into the combustion chamber
102 is ignited and the expanding gases within the combustion chamber 102 push the piston 104 outwardly (as during the intake stroke). Again, the combustion chamber valves 110 and 114 usually remain closed (at least during the early portion of the stroke).
- (4) An exhaust stroke, wherein the combustion products within the combustion chamber
102 are expelled to the exhaust manifold 116 by advancing the piston 104 towards the cylinder head 106 with the exhaust valve 114 open.
[0003] Each stroke occurs over 180 degrees of crankshaft rotation, with the entire cycle
thereby occurring over 720 degrees (two full crankshaft revolutions). The combustion
chamber valves
110 and
114 are usually opened and closed at the desired times by valve actuators such as cams
or other structures, which are in turn driven by the crankshaft (not shown). Since
such arrangements couple the timing and extent of valve opening and closing to the
positioning of the crankshaft, and since it may be desirable to have a greater degree
of control over valve actuation to achieve desired combustion chamber conditions,
there has been a recent trend towards the use of variable valve timing technologies.
These technologies wholly or partially decouple the timing and/or extent of valve
actuation from the crankshaft position, and allow the valves
110 and
114 to be opened and/or closed when desired (and may also allow the degree of opening
to be varied as desired). Examples of variable valve actuation (VVA) schemes may be
found, for example, in
U.S. Patents 4, 777, 915;
4,829,947; and
5,515,818.
[0004] The foregoing combustion cycle steps/strokes differ between classical SI and CI engines
in that SI engines tend to inject fuel during the intake stroke, whereas CI engines
tend to inject fuel late in the compression stroke or early in the power stroke, close
to "top dead center" (TDC), the piston
104's point of closest approach to the cylinder head
106. Additionally, in SI engines, ignition of the fuel/air mixture occurs by introduction
of a spark (with no spark plug being illustrated in
FIG. 1). In contrast, classical CI engines rely on the compression stroke to increase the
heat and pressure in the combustion chamber
102 to such a degree that ignition results. There are also various types of "hybrid"
engines which operate using a combination of SI and CI principles, or example, engines
which run primarily on CI principles but which use a spark or "glow plug" to assist
with ignition. (Also note that the engine of
FIG. 1 is described as a "simple idealized" one since real-world engines may have a wide
variety of combustion chamber configurations other than those shown at
102 in
FIG. 1, and may have varying numbers, locations, and configurations of combustion chamber
valves
110 and
114 and/or injectors
108.)
[0005] In the field of engine development and manufacture, two concerns of critical importance
are engine efficiency (e.g., power output per fuel consumption) and engine emissions.
Diesel engines tend to operate more efficiently than SI engines, but they unfortunately
also tend to have much greater pollutant emissions than SI engines. Common pollutants
arising from the use of internal combustion engines are nitrogen oxides (commonly
denoted NO
x) and particulates (also known simply as "soot"). NO
x is generally associated with high-temperature engine conditions, and may be reduced
by use of measures such as exhaust gas recirculation (EGR), wherein the engine intake
air is diluted with relatively inert exhaust gas (generally after cooling the exhaust
gas). This reduces the oxygen in the combustion chamber and obtains a reduction in
maximum combustion temperature, thereby deterring NO
x formation. Particulates (soot) include a variety of matter such as elemental carbon,
heavy hydrocarbons, hydrated sulfuric acid, and other large molecules, and are generally
associated with incomplete combustion. Particulates can be reduced by increasing combustion
and/or exhaust temperatures, or by providing more oxygen to promote oxidation of the
soot particles. Unfortunately, measures which reduce NO
x tend to increase particulate emissions, and measures which reduce particulates tend
to increase NO
x emissions, resulting in what is often termed the "soot-NO
x tradeoff".
[0006] At the time of this writing, the diesel engine industry is facing stringent emissions
legislation in the United States, and is struggling to find methods to meet government-imposed
NO
x and soot targets for the years 2002-2004 and even more strict standards to be phased
in starting in 2007. One measure under consideration is use of exhaust after-treatment
(e.g., particulate traps) for soot emissions control in both heavy-duty truck and
automotive diesel engines. However, in order to meet mandated durability standards
(e.g., 50,000 to 100,000 miles), the soot trap must be periodically regenerated (the
trapped soot must be periodically re-burned). This requires considerable expense and
complexity, since typically additional fuel must be mixed and ignited in the exhaust
stream in order to oxidize the accumulated particulate deposits.
[0007] Apart from studies directed to after-treatment, there has also been intense interest
in the more fundamental issue of how to reduce NO
x and particulates generation from the combustion process and thereby obtain cleaner
"engine out" emissions (i.e., emissions directly exiting the engine, prior to exhaust
after-treatment or similar measures). Studies in this area relate to shaping combustion
chambers, timing the fuel injection, tailoring the injection rate during injection
so as to meet desired emissions standards, or modifying the mode of injection (e.g,
modifying the injection spray pattern). One field of study relates to premixing methodologies,
wherein the object is to attain more complete mixing of fuel and air in order to simultaneously
reduce soot and NO
x emissions. In diesel engines, the object of premixing methodologies is to move away
from the diffusion burning mechanism which drives diesel combustion, and instead attempt
to attain premixed burning. In diffusion burning, the oxidant (fuel) is provided to
the oxidizer (air) with mixing and combustion occurring simultaneously. The fuel droplets
within an injected spray plume have an outer reaction zone surrounding a fuel core
which diminishes in size as it is consumed, and high soot production occurs at the
high-temperature, fuel-rich spray core. In contrast, premixed burning mixes fuel and
air prior to burning, and the more thorough mixing results in less soot production.
Premixing may be performed by a number of different measures, such as by use of fumigation
(injection of fuel into the intake airstream prior to its entry into the engine),
and/or direct injection of a fuel charge relatively far before top dead center (TDC)
so that motion of the piston 104, and convection within the cylinder, result in greater
mixing.
[0008] One promising diesel premixing technology is HCCI (Homogeneous Charge Compression
Ignition), which has the objective of causing initial ignition of a lean, highly premixed
air-fuel mixture at or near top dead center (TDC). An extensive discussion on HCCI
and similar premixing techniques is provided in
U.S. Patent 6,230,683 to zur Loye et al. , and
U.S. Patents 5,832,880 to Dickey and
6,213,086 to Chmela et al. also contain useful background information. The charge is said to be "homogeneous"
in HCCI because it is (at least theoretically) highly and evenly mixed with the air
in the cylinder. Ignition is then initiated by autoignition, i.e., thermodynamic ignition
via compression heating. The objective of HCCI is to use autoignition of the lean
and homogeneous mix to provide a uniform and relatively slow non-diffusion (or minimized
diffusion) burn, resulting in significantly lower combustion chamber temperatures
and diminished NO
x production (which thrives at high temperature), as well as lower soot production
owing to enhanced mixing. In contrast, a richer mixture (such as that necessary for
flame propagation from the spark in an SI engine) will burn more quickly at greater
temperature, and therefore may result in greater NO
x production.
[0010] As the foregoing references note, while HCCI-type premixing processes might be beneficially
implemented in CI engines to achieve their high efficiency without their customarily
high emissions, HCCI is also hard to accomplish owing to the difficulties in igniting
the lean mix and/or controlling the start of ignition. Combustion in an SI engine
is readily initiated by the spark, with premixed burning occurring afterward; similarly,
combustion in a conventional CI engine is initiated by fuel injection near top dead
center (at or slightly after the end of the compression stroke) when thermodynamic
conditions for autoignition are favorable, with diffusion burning occurring afterward.
However, HCCI does not utilize a spark, nor is it desirable for HCCI to use the rich
mixture needed for effective use of a spark. It is also difficult for HCCI to achieve
a homogeneous charge or premixed burning if injection near top dead center is used,
since there is less time for mixing to occur before ignition. Thus, a key area of
study in the HCCI field is how to efficiently initiate ignition, and more critically,
how to effect ignition at the desired time. While these issues are somewhat straightforward
where CI engines operate under a relatively rigid set of operating conditions (as
with diesel generators, which tend to operate at relatively constant speeds and loads),
these issues become exceedingly complex where CI engines must operate at varying speeds
and loads (as in automotive/vehicular operations). These ignition and timing problems
are the primary reason why HCCI methodologies have not attained widespread use outside
of generators and other constant speed/load applications.
[0011] In view of the foregoing discussion, there is a significant need for methods and
apparata which assist in obtaining premixed burning, particularly premixed burning
which achieves or approximates HCCI burning, so as to allow exploitation of the high
efficiency of CI engines without the detriment of their high pollutant emissions.
[0012] Other prior patents which are usefully considered include
U.S. Patents 3,714,932;
4,974,566;
5,201,907;
5,224,460;
5,228,422;
5,353,763;
6,286,482;
6,397,813;
6,439,210;
6,439,211;
6,460,337; and
6,571,765; and particularly
U.S. Patent 5,862,790 to Dai et al. and
U.S. Patent 6,405,706 to Hammoud et al. as well as
EP-A-0 473 258 and
FR-A -2 476 741.
Detailed Description of Preferred Versions of the Invention
[0013] The invention, which is defined by the claims set forth at the end of this document,
is directed to methods which at least partially alleviate the aforementioned problems.
To allow a reader to better compare the invention to the preexisting technology described
above, preferred features of the invention will now be more specifically described
with reference to
FIG. 1. Thus, it should be understood that while
FIG. 1 bears the label "prior art" to denote that the exemplary structure shown therein
is well known, the following description describes how the invention might be implemented
in previously-known engines of the type shown in
FIG. 1 or of other types (though it should also be understood that the invention might be
implemented in other types of engines which are yet to be developed).
[0014] A particularly preferred version of the invention involves briefly opening at least
one of the combustion chamber valves
110 and
114 for at least one discrete period sometime during the compression and/or power strokes,
resulting in one or more of the following benefits:
- (1) Greater mixing may be obtained within the combustion chamber 102. If one of the combustion chamber valves 110 and 114 is opened for a brief period, the gases within the combustion chamber 102 will rapidly exit from the opened valve into its associated manifold 112 or 116 during this period. The escaping gases may generate mixing flows within the combustion
chamber 102, which may enhance burning of particulates and thereby result in lower emissions.
- (2) The conditions in combustion chamber 102 can be altered to effect a change in the time ignition is initiated, thereby allowing
the ignition timing to be varied as desired to achieve HCCI. Since ignition timing
is largely dependent on the pressure (and temperature) of the gases within the combustion
chamber 102, releasing the combustion chamber 102 gases by briefly opening one or more of the combustion chamber valves 110 and/or 114 will introduce an ignition delay depending on the resulting drop in pressure (and
temperature). Thus, by opening one or more combustion valves 110 and/or 114 (and opening them simultaneously or sequentially, where multiple valves are opened),
one can tailor combustion chamber pressures (and to some degree temperatures) so that
peak values can be precisely timed, allowing control over ignition timing.
[0015] Since the pressure generated within the combustion chamber
102 is used to generate the power output from the engine
100, it might be regarded as contrary to the purposes of the engine
100 to open one or more of the combustion chamber valve(s) 110 and/or
114 for a discrete period sometime during the compression and/or power strokes: the release
of pressure from the combustion chamber
102 results in a power loss. However, the power loss may be acceptable if emissions reduction
and other objectives are met. The pressure loss within the combustion chamber
102 will depend on the length of the period during which the combustion chamber valve(s)
110 and/or
114 is/are opened, and the degree to which they are opened. It is believed that the benefits
of the invention would best be achieved if the period and extent of valve opening
be limited such that no more than 20% of the mass of the combustion chamber
102 contents (as measured after fuel injection) be released during all discrete openings
of the valves
110 and
114 during the compression and/or power strokes, since computerized engine simulations
appear to indicate that more substantial power losses occur if more than approximately
15% of the combustion chamber
102 mass is released.
[0016] It follows from the foregoing that it will usually be desirable to implement the
invention in such a manner that any mixing and/or ignition timing objectives are met
while releasing as little of the combustion chamber mass (and thus pressure) as possible.
Thus, it is expected that when the invention is implemented in most diesel engines
by a single opening of a single one of the combustion chamber valves
110 and
114 to its fully open position (or nearly so), it will usually be desirable to open the
valve for no more than 5 degrees of crankshaft revolution, since computerized engine
simulations indicate that more substantial power losses occur above approximately
7 degrees. More preferably, the period will not exceed approximately 3 degrees. Where
the invention is implemented by opening more than one combustion chamber valve (e.g.,
by opening both an intake valve
110 and an exhaust valve
114, or by opening more than one intake and/or exhaust valve
114 where multiple intake valves
110 and/or exhaust valves
114 are present), it is expected that the foregoing parameters would apply to the cumulative
openings of the valves
110 and
114. The same principle applies where a combustion chamber valve is opened more than
once during compression and/or power strokes.
[0017] The timing of the valve opening may also vary depending on which of the two aforementioned
benefits is to be achieved, and the degree to which it is to be achieved. It is expected
that the objective of greater mixing is best accomplished if one or more of the combustion
chamber valves
110 and
114 is opened during the first half of the power stroke, most preferably within about
50 degrees after TDC (i.e., approximately the first quarter of the power stroke).
At this time, ignition has usually started and combustion is underway.
[0018] In contrast, to achieve the objective of ignition timing, it is expected that any
openings of the valves
110 and
114 are usually best implemented starting in the latter half of the compression stroke,
most preferably at 50 degrees before TDC or thereafter. Openings of the valves
110 and
114 could occur earlier, but since ignition delay occurs with each valve opening owing
to pressure release from the combustion chamber
102, and ignition is usually desired late in the compression stroke or early in the expansion
stroke, openings of the valves
110 and
114 during the latter half of the compression stroke (particularly at about 30 degrees
before TDC and thereafter) should afford more precise control of ignition timing.
[0019] The foregoing discussion suggests that where ordinary engine speed/load conditions
are presumed, the mixing objective is generally better achieved with openings of the
valves
110 and
114 after TDC, whereas the ignition timing objective is generally better achieved with
openings of the valves
110 and
114 before TDC. However, openings of the valves
110 and
114 before TDC will have an impact on mixing as well. Similarly, openings of the valves
110 and
114 after TDC may also have an impact on ignition timing provided ignition has not already
begun. To illustrate, some combustion schemes - such as the Modified Kinetics (MK)
combustion methodology, where ignition is often desired after the power stroke has
begun - may benefit from valve openings after TDC to control ignition timing.
[0020] As noted above, the invention may be accomplished by opening more than one of the
intake and/or exhaust valves
110 and
114, and/or by opening one or more of these valves more than once during a combustion
cycle. It is expected that it will generally be most beneficial to open one or more
intake valves
110, since any unburned fuel and/or particulates ejected from the combustion chamber
102 will then be retained in the intake manifold
112 for later readmission into the combustion chamber
102 during the next intake stroke. The unburned fuel and particulates (if any) ejected
from the intake valve(s)
110 during one combustion cycle will therefore be taken up for consumption in the following
cycle. In contrast, if the invention is implemented by alternatively or additionally
opening one or more exhaust valves
114, any unburned fuel and/or particulates escaping the combustion chamber
102 will exit to the exhaust manifold
116 to exit as pollutant emissions (unless some form of after-treatment is applied to
the exhaust gases). Owing to these emissions, it is expected that implementation of
the invention by opening one or more exhaust valves
114 will generally be undesirable, unless any resulting emissions are outweighed by any
corresponding mixing and/or ignition timing benefits.
[0021] In some instances, opening of exhaust valves
114 warrants serious consideration despite any emissions drawbacks. To illustrate, since
exhaust valves
114 are often spaced at opposite ends of the combustion chamber
102 from any intake valves
110, it may in some cases be beneficial to first open an exhaust valve
114 and then an intake valve
110, or conversely first open an intake valve
110 followed by opening of an exhaust valve
114, to better achieve thorough mixing throughout the entirety of the combustion chamber
102. By opening the valves
110 and
114 at different times, a sort of back-and-forth "sloshing" effect is achieved in the
contents of the combustion chamber
102, resulting in thorough mixing. However, the same effect might be accomplished by only
opening intake valves
110 if multiple spaced intake valves
110 are present.
[0022] Since most standard valve actuation schemes couple valve actuation to crankshaft
motion, and it would often be difficult and expensive to modify any cams or other
intervening structure to effectively actuate the valves to implement the invention,
it is expected that the invention would make beneficial use of variable valve actuation
(VVA) technologies. Since variable valve actuators (VVAs) allow precise control of
valve opening and closing times, and/or to the degree of valve opening/closing, they
allow a readily available means for implementing the invention.
[0023] At various points in the foregoing discussion, preferred operating parameters were
noted for the invention, with such parameters being determined in view of computerized
engine simulations. These simulations were performed using WAVE simulation software
(Ricardo PLC, Shoreham-by-Sea, West Sussex, England) with a Caterpillar 3401E SCOTE
engine (Caterpillar Inc., Peoria, IL, USA) running at 821 rpm, 25% load, with 61.2
mg of fuel being injected per cycle starting at 20 degrees before TDC. It should be
understood that different preferred operating parameters might be derived if engines
having different configurations and/or operating conditions are tested.
[0024] Note that various preferred versions of the invention are shown and described above
to illustrate different possible options for the invention and the varying ways in
which these options may be combined. Apart from combining the different options of
the foregoing versions of the invention in varying ways, other modifications are also
considered to be within the scope of the invention. Following is an exemplary list
of such modifications.
[0025] First, any variable valve actuators (VVAs) used to implement the invention may make
use of regeneration methodologies, i.e., recovery of energy which would otherwise
be lost by the engine or by associated components, to better decrease energy demands
from valve actuation. Exemplary regeneration methodologies may be seen in
U.S. Patent 6,315,265 (recovery of energy captured from valve during valve deceleration), as well as in
U.S. Patents 6,082,328 and
6,012,424 (recovery of energy from vehicle braking systems).
[0026] Second, the invention might be implemented by opening a combustion chamber valve
other than an intake valve (or valves) and/or an exhaust valve (or valves). For example,
a combustion chamber might be separated from an adjacent supplemental chamber (provided
outside the cylinder) by a supplemental combustion chamber valve which serves neither
intake nor exhaust purposes. The combustion chamber contents might be "vented" into
this supplemental chamber at appropriate times to serve the mixing and/or ignition
timing functions of the invention.
[0027] Third, while the invention is believed to have most beneficial application to CI
engines, it might be utilized in SI engines as well (particularly in SI engines implementing
HCCI-type or similar combustion schemes). In this case, the primary benefit of the
invention would likely result from the enhanced mixing that the invention can provide,
rather than from ignition timing modification (which is more readily controlled in
an SI engine via spark timing).
[0028] The invention is not intended to be limited to the preferred versions of the invention
described above, but rather is intended to be limited only by the claims set out below.
Thus, the invention encompasses all different versions that fall literally or equivalently
within the scope of these claims.
1. A method of modifying combustion in a combustion chamber of a 4-stroke internal combustion
engine running under standard warm (non-starting) engine temperatures, the method
comprising the step of briefly opening a combustion chamber intake valve sometime
during a period spanning:
a. the latter half of the compression stroke, and
b. the first half of the power stroke,
such opening being subsequent to the closing of the same intake valve during the intake
stroke, and solely allowing the escape of combustion chamber gases.
2. A method as claimed in claim 1, wherein the briefly opening of the combustion chamber
intake valve effects an escape of no greater than approximately 15% of the mass of
the combustion chamber content.
3. A method as claimed in any of the foregoing claims wherein the combustion chamber
intake valve is briefly opened two or more times during the period.
4. A method as claimed in any of the foregoing claims wherein the combustion chamber
intake valve is briefly opened during the period of crankshaft rotation between:
a. 50 degrees before top dead center, and
b. 50 degrees after top dead center.
5. A method as claimed in any of the foregoing claims wherein the combustion chamber
intake valve is briefly opened during the period of crankshaft rotation between:
a. 30 degrees before top dead center, and
b. 30 degrees after top dead center.
6. A method as claimed in any of the foregoing claims wherein the combustion chamber
intake valve is briefly opened for no greater than approximately 7 degrees of crankshaft
rotation.
7. A method as claimed in any of the foregoing claims wherein the combustion chamber
intake valve is briefly opened for no greater than approximately 5 degrees of crankshaft
rotation.
8. A method as claimed in any of the foregoing claims wherein the combustion chamber
intake valve is briefly opened for no greater than approximately 3 degrees of crankshaft
rotation.
9. A method as claimed in any of the foregoing claims wherein the combustion chamber
intake valve which is briefly opened is an intake valve.
10. A method as claimed in any of the foregoing claims wherein the combustion chamber
intake valve is briefly opened at or substantially near the time of ignition.
11. A method as claimed in any of the foregoing claims wherein multiple combustion chamber
intake valves are briefly opened during the period.
12. A method as claimed in claim 11 wherein at least some of the multiple combustion chamber
intake valves are briefly opened during the period starting at different times.
13. A method as claimed in claim 12 or 13 including a combustion chamber exhaust valve.
1. Verfahren zum Modifizieren der Verbrennung in einer Verbrennungskammer einer Viertaktverbrennungskraftmaschine
mit innerer Verbrennung, welche unter warmen Standard-(Nicht-Start-)Motortemperaturen
läuft, wobei das Verfahren den Schritt umfasst: kurzes Öffnen eines Verbrennungskammer-Einlassventils
irgendwann während einer Periode, umspannend:
a. die letzte Hälfte des Verdichtungstaktes und
b. die erste Hälfte des Arbeitstaktes,
wobei ein derartiges Öffnen dem Schließen desselben Einlassventils während des Ansaugtaktes
folgt und allein das Entweichen von Verbrennungskammergasen erlaubt.
2. Verfahren nach Anspruch 1, wobei das kurze Öffnen des Verbrennungskammer-Einlassventils
ein Entweichen von nicht mehr als ca. 15 % der Masse des Verbrennungskammerinhalts
bewirkt.
3. Verfahren nach einem der voranstehenden Ansprüche, wobei das Verbrennungskammer-Einlassventil
zwei oder mehr Male während der Periode kurz geöffnet wird.
4. Verfahren nach einem der voranstehenden Ansprüche, wobei das Verbrennungskammer-Einlassventil
während der Periode der Kurbelwellendrehung zwischen:
a. 50 Grad vor dem oberen Totpunkt und
b. 50 Grad nach dem oberen Totpunkt
kurz geöffnet wird.
5. Verfahren nach einem der voranstehenden Ansprüche, wobei das Verbrennungskammer-Einlassventil
während der Periode der Kurbelwellendrehung zwischen:
a. 30 Grad vor dem oberen Totpunkt und
b. 30 Grad nach dem oberen Totpunkt
kurz geöffnet wird.
6. Verfahren nach einem der voranstehenden Ansprüche, wobei das Verbrennungskammer-Einlassventil
über nicht mehr als ca. 7 Grad Kurbelwellendrehung kurz geöffnet wird.
7. Verfahren nach einem der voranstehenden Ansprüche, wobei das Verbrennungskammer-Einlassventil
über nicht mehr als ca. 5 Grad Kurbelwellendrehung kurz geöffnet wird.
8. Verfahren nach einem der voranstehenden Ansprüche, wobei das Verbrennungskammer-Einlassventil
über nicht mehr als ca. 3 Grad Kurbelwellendrehung kurz geöffnet wird.
9. Verfahren nach einem der voranstehenden Ansprüche, wobei das Verbrennungskammer-Einlassventil,
welches kurz geöffnet wird, ein Einlassventil ist.
10. Verfahren nach einem der voranstehenden Ansprüche, wobei das Verbrennungskammer-Einlassventil
zu oder im Wesentlichen nahe der Zündzeit kurz geöffnet wird.
11. Verfahren nach einem der voranstehenden Ansprüche, wobei mehrere Verbrennungskammer-Einlassventile
während der Periode kurz geöffnet werden.
12. Verfahren nach Anspruch 11, wobei mindestens einige der mehreren Verbrennungskammer-Einlassventile
während der Periode zu verschiedenen Zeiten kurz geöffnet werden.
13. Verfahren nach Anspruch 12 oder 13, umfassend ein Verbrennungskammer-Auslassventil.
1. Procédé de modification de la combustion dans une chambre de combustion d'un moteur
à combustion interne à 4 temps fonctionnant à des températures de moteur chaudes standard
(hors démarrage), le procédé comprend l'étape d'ouverture brève d'une soupape d'admission
de la chambre de combustion parfois au cours d'une période recouvrant :
a. la dernière moitié du temps de compression, et
b. la première moitié du temps de combustion,
une telle ouverture étant ultérieure à la fermeture de cette même soupape d'admission
lors du temps d'admission, et permettant uniquement le dégagement des gaz de la chambre
de combustion.
2. Procédé selon la revendication 1, dans lequel l'ouverture brève de la soupape d'admission
de la chambre de combustion réalise un dégagement inférieur à approximativement 15
% de la masse du contenu de la chambre de combustion.
3. Procédé selon l'une quelconque des revendications précédentes, dans lequel la soupape
d'admission de la chambre de combustion est ouverte brièvement au moins deux fois
lors de cette période.
4. Procédé selon l'une quelconque des revendications précédentes, dans lequel la soupape
d'admission de la chambre de combustion est ouverte brièvement lors de la période
de rotation du vilebrequin entre :
a. 50 degrés avant le point mort haut, et
b. 50 degrés après le point mort haut.
5. Procédé selon l'une quelconque des revendications précédentes, dans lequel la soupape
d'admission de la chambre de combustion est ouverte brièvement lors de la période
de rotation du vilebrequin entre :
a. 30 degrés avant le point mort haut, et
b. 30 degrés après point mort haut.
6. Procédé selon l'une quelconque des revendications précédentes, dans lequel la soupape
d'admission de la chambre de combustion est ouverte brièvement sur moins d'approximativement
7 degrés de la rotation du vilebrequin.
7. Procédé selon l'une quelconque des revendications précédentes, dans lequel la soupape
d'admission de la chambre de combustion est brièvement ouverte sur moins d'approximativement
5 degrés de la rotation du vilebrequin.
8. Procédé selon l'une quelconque des revendications précédentes, dans lequel la soupape
d'admission de la chambre de combustion est brièvement ouverte sur moins d'approximativement
3 degrés de la rotation du vilebrequin.
9. Procédé selon l'une quelconque des revendications précédentes, dans lequel la soupape
d'admission de la chambre de combustion qui est ouverte brièvement est une soupape
d'admission.
10. Procédé selon l'une quelconque des revendications précédentes, dans lequel la soupape
d'admission de la chambre de combustion est ouverte brièvement au temps d'allumage
ou à un moment sensiblement proche du temps d'allumage.
11. Procédé selon l'une quelconque des revendications précédentes, dans lequel de multiples
soupapes d'admission de la chambre de combustion sont ouvertes brièvement lors de
la période.
12. Procédé selon la revendication 11, dans lequel au moins certaines des multiples soupapes
d'admission de la chambre de combustion sont ouvertes brièvement lors de la période
commençant à différents moments.
13. Procédé selon la revendication 12 ou 13, incluant une soupape d'échappement de la
chambre de combustion.