TECHNICAL FIELD OF THE INVENTION
[0001] The present invention relates generally to engine crankcase gas blow-by sensors and
to a method of evaluating performance of an internal combustion engine. More particularly,
this invention relates to an engine crankcase gas blow-by sensor using a venturi and
a differential pressure transducer to measure volumetric flow of blow-by gases.
BACKGROUND OF THE INVENTION
[0002] Ideally, the pressure within an internal combustion engine crankcase should be maintained
at a level equal to or slightly less than atmospheric pressure to prevent external
oil leakage through the various gasketed joints, such as that between the valve cover
and the cylinder head. As is well known, in an internal combustion engine, a so-called
blow-by gas is emitted in the crankcase as a result of leaks of intake air-fuel mixture
and combustion gases through the clearances around piston rings, during the compression,
combustion and/or exhaust cycles. Because of these blow-by gases, the crankcase pressure
will inherently rise, promoting leakage of oil from the crankcase. Originally, the
crankcase pressure was vented to the atmosphere through a breather in order to solve
this problem.
More recently, environmental considerations have dictated that the blow-by gases in
the crankcase be vented back to the combustion chamber rather than being released
to the atmosphere. Such closed crankcase ventilation (CCV) systems recycle the blow-by
gas by burning these gases together with the intake air-fuel mixture.
[0003] Heavy duty and high horsepower internal combustion engines run under severe and sometimes
adverse conditions, where engine downtime is expensive and service is not always available.
A good method of checking an engine's "health" is to periodically, or preferably continuously,
monitor the flow of crankcase blow-by gases. The greater the quantity of blow-by gases
escaping around the pistons, the poorer the condition of the engine. Therefore, sensing
of the amount of blow-by gas in an engine can detect catastrophic failures (i.e. an
instantaneous increase in the amount of blow-by gas) or monitor engine wear over time
in order to predict when the engine will require an overhaul (i.e. a slowly increasing
amount of blow-by gas).
[0004] A good way to measure the volume of blow-by gas entering the crankcase is to measure
the pressure of such gases in the crankcase. However, closed crankcase ventilation
systems do not allow any of the crankcase gases to be vented through an orifice, which
would be required in order to measure the crankcase pressure. There is therefore a
need for an alternative way to measure the amount of blow-by gas entering the engine
crankcase and to collect this data for making determinations of engine health. The
present invention is directed toward meeting this need.
[0005] US-A-3,862,624 discloses an engine which uses oxygen and an excess of hydrogen as
fuel and which has a substantially closed exhaust system which recirculates the gaseous
part of the exhaust and mixes it with fresh gaseous feed and recirculated blow-by
gas. A flow meter is provided for the mixture of recirculated exhaust gas, fresh gaseous
fuel and blow-by gas.
SUMMARY OF THE INVENTION
[0006] According to one aspect of this invention there is provided an engine with a crankcase
gas blow-by sensor as claimed in claim 1. Preferred features are claimed in the sub
claims 2 to 7.
[0007] In a closed crankcase ventilation system, crankcase gases are allowed to flow through
a venturi which includes high pressure and low pressure taps. The high and low pressure
taps are coupled to a differential pressure transducer which produces an output that
is proportional to the volumetric flow of crankcase gases through the venturi. The
use of a venturi in conjunction with a differential pressure sensor offers a low resistance
path for the flow of crankcase gases and allows continuous monitoring of blow-by without
exceeding the operating pressure limitations of various oil seals. Such a sensor is
particularly suited for closed crankcase ventilation (ccv) systems, as it doesn't
require venting of crankcase gases to the atmosphere (but will also work well on open
systems).
[0008] According to another aspect of this invention there is provided a method of evaluating
performance of an internal combustion engine as claimed in claim 8.
[0009] Preferred features of the method are claimed in the sub-claims 9 to 11.
BRIEF DESCRIPTION OF THE DRAWINGS
[0010] FIG. la is a cross-sectional view of a preferred embodiment of the venturi of the
present invention.
[0011] FIG. lb is an end view of the venturi of FIG. 1.
[0012] FIG. 2 is a top plan view of the venturi of FIG. 1 with the differential pressure
transducer mounted thereon.
[0013] FIG. 3 is a cross-sectional view of the venturi and differential pressure sensor
of FIG. 2.
[0014] FIG. 4 is an end view of the venturi and differential pressure sensor of FIG. 2.
[0015] FIG. 5 is a graph of differential pressure as a function of the flow transfer function
of the venturi of FIG. 2.
[0016] FIG. 6 is a graph of the voltage output signal of the differential pressure sensor
of FIG. 2 as a function of air flow through the venturi.
DESCRIPTION OF THE PREFERRED EMBODIMENT
[0017] For the purposes of promoting an understanding of the principles of the invention,
reference will now be made to the embodiment illustrated in the drawings and specific
language will be used to describe the same. It will nevertheless be understood that
no limitation of the protection claimed by the claims is thereby intended, such alterations
and further modifications in the illustrated device, and such further applications
of the principles of the invention as illustrated therein and as claimed by the claims,
being contemplated as would normally occur to one skilled in the art to which the
invention relates.
[0018] Hereinafter, when expressions such as "above" and "below" are used, it will be assumed
that the piston is so oriented that its axis is vertical and the crankcase is positioned
below the piston. This hypothesis is merely intended to simplify the description and
therefore does not imply that the piston is in fact oriented in this way when it is
mounted in an internal combustion engine.
[0019] The present invention involves the sensing of crankcase blow-by gases by measuring
the volumetric flow of such gases rather than the prior art method of measuring the
pressure of these gases. Volumetric flow of the blow-by gases is accomplished by routing
a portion of these gases through a venturi which has high pressure and low pressure
taps therein. A differential pressure sensor is then attached to the high and low
pressure taps in order to measure the pressure differential between the taps. This
differential pressure is related to the volumetric flow of blow-by gases through the
venturi, and hence the volumetric flow of blow-by gases around the engine pistons.
Both instantaneous measurement of this volumetric flow, as well as historical trend
analysis, provide useful information in determining the health of the engine as well
as to predict future needs for service. The sensor will therefore yield data suitable
for trend analysis to aid diagnostics and prognostics, and can be used to avoid catastrophic
failure.
[0020] Referring to FIG. la, a cross-sectional view of a preferred embodiment venturi of
the present invention is illustrated and indicated generally at 10. The venturi 10
includes a generally cylindrical venturi body 12 having an inlet port 14 and an outlet
port 16 attached thereto. The inlet port 14 includes a hose connection nipple 18 while
the outlet port 16 includes a hose connection nipple 20. Crankcase gases may thus
be routed to the venturi 10 via a suitable hose (not shown), and crankcase gases exiting
the venturi 10 may be routed back to the crankcase via a second suitable hose (not
shown). The venturi 10 is preferably formed from aluminum, steel or an injection molded
engineering thermoplastic, or any other suitable material.
[0021] The dimensions of the venturi 10 will vary depending upon the engine size with which
the venturi is associated. The dimensions given for the venturi 10 of FIG. la are
preferred for use with a K50 diesel engine manufactured by the Cummins Engine Company
of Columbus, Indiana. Because the venturi effectively amplifies the flow rate of crankcase
gases through the venturi, different venturi sizes will be appropriate for different
size engines.
[0022] In the preferred embodiment of FIG. la, the venturi 10 has an inlet port 14 internal
diameter of 1 inch (25.4mm). The outlet port 16 also has an internal diameter of 1
inch (25.4). The venturi throat 22 has an internal diameter of 0.425 inches (10.795mm.)
Dimensions for the other portions of the venturi 10 are illustrated in FIG. la. A
high pressure tap 24 is formed from the exterior surface of the venturi body 12 to
the inlet bore 26 which extends through the inlet port 14. Similarly, a low pressure
tap 28 is formed from the exterior surface of the venturi body 12 to the venturi throat
22.
[0023] Referring to FIG. 2, a differential pressure sensor 30 is coupled to the venturi
body 12 by means of four screws 32 which bore into the body 12. The differential pressure
sensor 30 is preferably a variable capacitive on ceramic differential pressure sensor
such as a model P604 manufactured by Kavlico of Moorepark, California, but any type
of differential pressure sensor may be utilized in the present invention.
[0024] As illustrated in the cross-sectional view of FIG. 3, the differential pressure sensor
30 is mounted to the venturi body 12 such that the high pressure tap 24 is aligned
with the inlet 34 to the high pressure side of the differential pressure sensor 30.
Similarly, the low pressure tap 28 communicates with the inlet 36 of the low pressure
side of the differential pressure sensor 30. The differential pressure sensor 30 is
preferably of the wet-dry type, therefore the low pressure side of the sensor includes
a filter element 38 in order to prevent liquid, such as uncombusted fuel and oil,
to enter the low pressure side of the differential pressure sensor 30. The output
of the differential pressure sensor 30 is a voltage which is proportional to the differential
pressure across the high pressure tap 24 and the low pressure tap 28. This output
voltage is supplied to a multi-pin electrical connector 40. The connector 40 additionally
accepts the input voltage which is used to power the differential pressure sensor
30.
[0025] The venturi 10 of FIG. la is capable of flowing in excess of 50 actual cubic feet
per minute (ACFM) (1.4 cubic metres per minute) air or crankcase gas, although the
flow rate will be approximately 26 ACFM (0.728 cubic metres per minute) maximum for
the model K50 engine for which the venturi 10 was designed. A flow rate of 26 ACFM
(0.728 cubic metres per minute) results in approximately 30 inches (760 mm) of water
pressure differential developed across the pressure taps 24 and 28. This is illustrated
in the graph of FIG. 5 which illustrates the differential pressure developed across
the pressure taps 24 and 28 of the venturi 10 as a function of gas flow through the
venturi 10. This graph illustrates that the transfer function of gas flow vs. differential
pressure for the venturi 10 is not linear.
[0026] The combination venturi body 12 and differential pressure sensor 30 is preferably
mounted in a substantially vertical orientation in order to allow gas to run out of
the venturi in order to prevent build-up and contamination within the differential
pressure sensor 30. Such build-up will change the measured pressure and result in
inaccuracies in the measurement of crankcase gas flow. The differential pressure sensor
30 is mounted to the venturi body 12 by means of an appropriate sealing gasket which
forms an airtight seal between the differential pressure sensor 30 and the high pressure
tap 24 and low pressure tap 28.
[0027] Referring to FIG. 6, it can be seen that the output voltage of the differential pressure
sensor 30 is a non-linear function of media volumetric flow, which tracks the actual
differential pressure developed across the high and low pressure taps of the venturi.
The input voltage to the differential pressure sensor 30 is 5.0+/-5% VDC. Because
the sensor 30 is ratiometric to the input voltage, the output voltage illustrated
in FIG. 6 assumes a 5.0 VDC input voltage. It will be appreciated by those skilled
in the art that the transfer function of FIG. 6 allows an engine monitoring system
to determine the flow-rate of crankcase gases through the venturi by monitoring the
output voltage of the differential pressure sensor 30. This information may be used
in different ways by the engine monitoring system. For instance, the output voltage
of the differential pressure sensor 30 may be monitored for an instantaneous increase
of blow-by gas flow, indicative of a catastrophic failure within the engine. The amount
of instantaneous increase necessary to signal a catastrophic failure may be made a
calibratable threshold point within the engine monitoring system and is dependent
upon engine size. Upon the sensing of such an instantaneous increase in blow-by gas
flow, an indicator light may be used to alert the driver of the situation. The output
voltage of the differential pressure sensor 30 may also be used to record crankcase
gas flow rate over time in order to chart the wear of the engine and hence predict
when the engine will require an overhaul. The engine monitoring system may use a filtered
linear projection in order to determine at what time the engine blow-by gases have
increased to the point where maximum performance is no longer available from the engine.
Appropriate servicing can then be scheduled for the vehicle prior to that time.
[0028] It will therefore be appreciated by those skilled in the art that the present invention
allows useful measurement of engine crankcase blow-by which was previously unavailable
in closed crankcase ventilation systems. Measurement of such blow-by gases can provide
information to signal catastrophic failures within the engine as well as to predict
when major engine servicing will be required in the future. Such information may be
used to minimize downtime of the engine and to prevent expensive catastrophic engine
failure.
[0029] While the invention has been illustrated and described in detail in the drawings
and foregoing description, the same is to be considered as illustrative and not restrictive
in character, it being understood that only the preferred embodiment has been shown
and described and that all changes and modifications that come within the scope of
the protection claimed by the claims are desired to be protected.
1. An engine comprising a crankcase gas blow-by sensor and an engine crankcase operative
to receive blow-by gases via a gas flow path;
characterised by:
a venturi (10) positioned within the gas flow path such that the blow-by gases in
use flow through the venturi (10) and are routed back from the venturi (10) to the
crankcase;
a high pressure tap (24) extending from an exterior of the venturi (10) to an interior
(26) of the venturi (10);
a low pressure tap (28) extending from the venturi exterior to the venturi interior
(22); and
a sensor (30) coupled to the venturi (10) and operative to measure a differential
pressure between the high pressure tap (24) and the low pressure tap (28).
2. An engine crankcase gas blow-by sensor, according to claim 1 in an internal combustion
engine, comprising:
at least one cylinder;
at least one piston slidingly disposed within the at least one cylinder in order define
a combustion chamber above the piston;
the crankcase being coupled to the at least one cylinder, wherein an interior of the
crankcase is in fluid communication with an interior of the at least one cylinder
below the at least one piston via at least the gas flow path, wherein combustion blow-by
gases which blow-by the at least one piston may enter the crankcase.
3. Apparatus according to claim 1 or claim 2, wherein the high pressure tap (24) extends
from the venturi exterior to an interior of an inlet bore (26) of the venturi (10).
4. Apparatus according to claim 1 or claim 2, wherein the low pressure tap (28) extends
from the venturi exterior to an interior of a venturi throat (22) of the venturi (10).
5. Apparatus according to claim 1 or claim 2, wherein the sensor (30) comprises a wet-dry
differential pressure sensor.
6. Apparatus according to claim 1 or claim 2, wherein the sensor (30) comprises a variable
capacitive on ceramic pressure sensor.
7. Apparatus according to claim 1 or claim 2, wherein the venturi (10) is mounted substantially
vertically in order to allow gas to run out of the venturi (10).
8. A method of evaluating performance of an internal combustion engine,
characterised by the steps of:
(a) routing at least a portion of blow-by gases entering a crankcase of the engine
through a venturi (10) and back to the crankcase, the venturi (10) having a high pressure
tap (24) and a low pressure tap (28);
(b) measuring a pressure differential between the high pressure tap (24) and the low
pressure tap (28); and
(c) outputting a signal that is proportional to the measured pressure differential.
9. A method according to claim 8, wherein step (b) is performed by a wet-dry differential
pressure sensor (30).
10. A method according to claim 8, wherein step (b) is performed by a variable capacitive
on ceramic pressure sensor (30).
11. A method according to claim 8, wherein the signal is a voltage signal.
1. Motor mit einem Sensor für ins Kurbelgehäuse durchblasendes Gas und einem Motorkurbelgehäuse,
das Durchblasgase über einen Gasströmungsweg empfangen kann;
gekennzeichnet durch
ein Venturi (10), das in dem Gasströmungsweg derart angeordnet ist, daß die Durchblasgase
in Betrieb durch das Venturi (10) strömen und von dem Venturi (10) aus zu dem Kurbelgehäuse zurückgeleitet
werden;
eine Hochdruckzapfstelle (24), die sich von außerhalb des Venturis (10) bis zu einem
Innenraum (26) des Venturis (10) erstreckt;
eine Niederdruckzapfstelle (28), die sich von außerhalb des Venturis bis zu dem Innenraum
(22) des Venturis erstreckt; und
einen Sensor (30), der mit dem Venturi (10) verbunden und wirksam ist, um einen Differenzdruck
zwischen der Hochdruckzapfstelle (24) und der Niederdruckzapfstelle (28) zu messen.
2. Sensor für ins Motorkurbelgehäuse durchgeblasenes Gas gemäß Anspruch 1 in einer Brennkraftmaschine,
mit
mindestens einem Zylinder;
mindestens einem Kolben, der verschiebbar in dem mindestens einen Zylinder angeordnet
ist, um eine Brennkammer über dem Kolben zu begrenzen;
wobei das Kurbelgehäuse mit dem mindestens einen Zylinder verbunden ist, wobei ein
Innenraum des Kurbelgehäuses in Strömungsverbindung mit einem Innenraum des mindestens
einen Zylinders unter dem mindestens einen Kolben über mindestens dem Gasströmungsweg
steht, wobei Verbrennungsdurchblasgase, die an dem mindestens einen Kolben vorbeiströmen,
in das Kurbelgehäuse eintreten können.
3. Vorrichtung nach Anspruch 1 oder Anspruch 2, bei der sich die Hochdruckzapfstelle
(24) von außerhalb des Venturis bis zum Innern einer Einlaßbohrung (26) des Venturis
(10) erstreckt.
4. Vorrichtung nach Anspruch 1 oder Anspruch 2, bei der sich die Niederdruckzapfstelle
(24) von außerhalb des Venturis bis zum Innern einer Venturiengstelle (22) des Venturis
(10) erstreckt.
5. Vorrichtung nach Anspruch 1 oder Anspruch 2, bei der der Sensor (30) einen Naß-Trocken-Differenzdrucksensor
aufweist.
6. Vorrichtung nach Anspruch 1 oder Anspruch 2, bei der der Sensor (30) einen regelbaren
kapazitiven Auf-Keramik-Drucksensor aufweist.
7. Vorrichtung nach Anspruch 1 oder Anspruch 2, bei der das Venturi (10) im wesentlichen
vertikal angeordnet ist, so daß Gas aus dem Venturi (10) ausströmen kann.
8. Verfahren zum Bewerten der Leistung einer Brennkraftmaschine,
gekennzeichnet durch die Schritte:
(a) Leiten von mindestens einem Teil der in ein Kurbelgehäuse der Brennkraftmaschine
eintretenden Durchblasgase durch ein Venturi (10) und zurück zu dem Kurbelgehäuse, wobei das Venturi (10) eine Hochdruckzapfstelle
(24) und eine Niederdruckzapfstelle (28) hat;
(b) Messen einer Druckdifferenz zwischen der Hochdruckzapfstelle (24) und der Niederdruckzapfstelle
(28); und
(c) Ausgeben eines Signals, das zu der gemessenen Druckdifferenz proportional ist.
9. Verfahren nach Anspruch 8, bei dem Schritt (b) durch einen Naß-Trocken-Differenzdrucksensor
(30) ausgeführt wird.
10. Verfahren nach Anspruch 8, bei dem Schritt (b) durch einen regelbaren kapazitiven
Auf-Keramik-Drucksensor (30) ausgeführt wird.
11. Verfahren nach Anspruch 8, bei dem das Signal ein Spannungssignal ist.
1. Moteur comprenant un détecteur de gaz de carter et un carter de moteur permettant
de recevoir les gaz de carter par l'intermédiaire d'un passage d'écoulement gazeux
;
caractérisé par :
une buse (10) placée dans le passage d'écoulement gazeux de sorte que les gaz de carter
s'écoulent, en utilisation, dans la buse (10) et qu'il sont renvoyés de la buse (10)
au carter ;
un robinet haute pression (24) s'étendant d'une partie extérieure de la buse (10)
à une partie intérieure (26) de la buse (10) ;
un robinet basse pression (28) s'étendant de l'extérieur de la buse à l'intérieur
de la buse (22) ; et
un détecteur (30) couplé à la buse (10) et permettant de mesurer une différence de
pression entre le robinet haute pression (24) et le robinet basse pression (28).
2. Détecteur de gaz de carter de moteur selon la revendication 1 d'un moteur à combustion
interne, comprenant :
au moins un cylindre ;
au moins un piston placé, de façon à pouvoir coulisser, dans l'au moins un cylindre
afin de définir une chambre de combustion au-dessus du piston ;
le carter étant couplé à au moins un cylindre, dans lequel une partie intérieure du
carter est en communication fluidique avec une partie intérieure d'au moins un piston
situé au-dessous d'au moins un piston par l'intermédiaire d'au moins le passage d'écoulement
gazeux, dans lequel les gaz de carter de combustion qui se trouvent au niveau de l'au
moins un piston peuvent entrer dans le carter.
3. Appareil selon la revendication 1 ou la revendication 2, dans lequel le robinet haute
pression (24) s'étend de l'extérieur de la buse à une partie intérieure d'un alésage
d'entrée (26) de la buse (10).
4. Appareil selon la revendication 1 ou la revendication 2, dans lequel le robinet basse
pression (28) s'étend de l'extérieur de la buse à une partie intérieure d'un col (22)
de la buse (10).
5. Appareil selon la revendication 1 ou la revendication 2, dans lequel le détecteur
(30) comprend un détecteur de pression différentielle de type sec ou humide.
6. Appareil selon la revendication 1 ou la revendication 2, dans lequel le détecteur
(30) comprend une capacité variable sur un détecteur de pression en céramique.
7. Appareil selon la revendication 1 ou la revendication 2, dans lequel la buse (10)
est montée sensiblement verticalement afin de permettre au gaz de sortir de la buse
(10).
8. Procédé permettant d'évaluer les performances d'un moteur à combustion interne,
caractérisé par les étapes consistant à :
(a) diriger au moins une partie des gaz de carter entrant dans un carter du moteur
dans une buse (10) puis de nouveau dans le carter, la buse (10) présentant un robinet
haute pression (24) et un robinet basse pression (28) ;
(b) mesurer une différence de pression entre le robinet haute pression (24) et le
robinet basse pression (28) ; et
(c) émettre un signal proportionnel à la différence de pression mesurée.
9. Procédé selon la revendication 8, dans lequel l'étape (b) est exécutée par un détecteur
de pression différentielle de type sec-humide (30).
10. Procédé selon la revendication 8, dans lequel l'étape (b) est exécutée par une capacité
variable sur un détecteur de pression en céramique (30).
11. Procédé selon la revendication 8, dans lequel le signal est un signal de tension.