U.S. patent number 3,754,538 [Application Number 05/194,930] was granted by the patent office on 1973-08-28 for engine crankcase ventilation.
This patent grant is currently assigned to General Motors Corporation. Invention is credited to Max Ephraim, Jr., Ludvik F. Koci.
United States Patent |
3,754,538 |
Ephraim, Jr. , et
al. |
August 28, 1973 |
ENGINE CRANKCASE VENTILATION
Abstract
In a preferred embodiment, a crankcase ventilation system
utilizes the combination of a fixed orifice and a pressure actuated
regulating valve downstream of the orifice to control vapor flow
from the engine crankcase into its induction system. The
arrangement provides controlled vacuum in the engine crankcase
during normal operation but permits the development of pressure
during abnormal conditions of excessive blowby or the like so as to
permit actuation of a crankcase pressure actuated shutdown device
associated with the engine.
Inventors: |
Ephraim, Jr.; Max (Evergreen
Park, IL), Koci; Ludvik F. (LaGrange Park, IL) |
Assignee: |
General Motors Corporation
(Detroit, MI)
|
Family
ID: |
22719427 |
Appl.
No.: |
05/194,930 |
Filed: |
November 2, 1971 |
Current U.S.
Class: |
123/41.86;
55/DIG.19; 123/574; 123/198D |
Current CPC
Class: |
F01M
13/04 (20130101); F01M 13/0011 (20130101); F01M
2013/0083 (20130101); Y10S 55/19 (20130101) |
Current International
Class: |
F01M
13/04 (20060101); F01M 13/00 (20060101); F02f
009/02 () |
Field of
Search: |
;123/119B,41.86 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Smith; Al Lawrence
Assistant Examiner: Toth; Dennis
Claims
We claim:
1. The combination with an internal combustion engine having a
crankcase and a combustion air inlet of
engine shutdown means connected to the engine crankcase and
responsive to a predetermined positive pressure therein to stop the
engine,
crankcase ventilation means communicating said crankcase with said
air inlet for drawing crankcase vapors into the combustion air
stream,
orifice means in said communicating means and providing a fixed
restriction to fluid flow therethrough, and
regulating valve means in said communicating means downstream of
said orifice means, said valve means providing a variable
restriction to fluid flow and being operative to limit the negative
control pressures upstream thereof to a predetermined value
regardless of greater negative pressures in the air inlet,
said control pressure limit being chosen and said orifice means
being sized to permit passage of a sufficient flow of crankcase
vapors during normal engine operation to maintain a predetermined
maximum vacuum in the engine crankcase but to provide a sufficient
flow restriction to cause development of positive pressure in the
crankcase sufficient to actuate said shutdown means to stop the
engine when there occurs an abnormally high flow of blowby into the
crankcase indicative of engine malfunction.
2. A crankcase ventilation system in combination with an internal
combustion engine having a combustion air inlet, a crankcase and
engine shutdown means connected with said crankcase and adapted to
be actuated by a predetermined positive pressure therein to
terminate engine operation, said crankcase ventilation means
comprising
means communicating said crankcase with said air inlet for drawing
a flow of crankcase vapors into the combustion air stream,
regulating valve means in said communicating means and providing a
variable restriction to fluid flow therethrough, said valve means
being responsive to system pressures upstream thereof to vary said
restriction in a manner to maintain a predetermined maximum vacuum
upstream thereof, and
fixed orifice means in said communicating means between said
regulating valve means and said crankcase, said orifice means being
sized to restrict fluid flow sufficiently to cause development of a
positive pressure in the crankcase to actuate said shutdown means
under predetermined conditions of excess engine blowby but to allow
the passage of sufficient ventilation flow to permit the
establishment of a predetermined maximum crankcase vacuum under
normal engine operating conditions.
3. The combination of claim 2 and further including an oil
separator in said communicating means, upstream of said orifice
means, said oil separator being adapted to separate and return to
the engine crankcase excess oil passing into the ventilation system
with the crankcase vapors.
4. An internal combustion engine having in combination
an exhaust-driven turbocharger operable to supply varying amounts
of combustion air to the engine under various engine operating
conditions,
a combustion air inlet to the turbocharger subject to substantial
variations in sub-ambient air pressure under the varying air flows
drawn into said turbocharger,
an enclosed crankcase into which engine blowby gases are received
in varying amounts during engine operation,
pressure responsive means connected with said crankcase and
responsive to a predetermined, positive pressure therein to stop
said engine,
crankcase ventilation means communicating said crankcase with said
air inlet for drawing crankcase vapors into the combustion air
stream,
a regulating valve in said communicating means and providing a
variable restriction to fluid flow therethrough, said valve being
operable to vary said restriction so as to limit the vacuum
immediately upstream thereof to a predetermined maximum, and
a fixed orifice in said communicating means between said regulating
valve and said crankcase and sized to permit a sufficient flow of
crankcase vapors through said communicating means to establish a
substantial crankcase vacuum under normal engine operating
conditions but to restrict flow sufficiently to cause development
of a positive pressure in the crankcase sufficient to actuate said
pressure responsive means under predetermined conditions to excess
engine blowby.
Description
BACKGROUND OF THE INVENTION
This invention relates to crankcase ventilation systems for
internal combustion engines and, more particularly, to a crankcase
ventilation system having the capability of maintaining a
predetermined vacuum in the engine crankcase under normal operating
conditions, including varying inlet pressures while permitting the
development of pressure in the crankcase under abnormal engine
conditions of high blowby or the like.
In the operation of internal combustion engines and, specifically,
large diesel engines used, for example, as power plants for diesel
electric locomotives and the like, it is desirable to maintain a
small vacuum in the crankcase under normal operating conditions.
This has the advantage of reducing the amount of vapors maintained
in the crankcase so that the possibility of a crankcase explosion
is minimized. In addition, it provides a pressure differential
which acts at the various seals and other openings in the crankcase
to reduce the possibility of oil escaping from the interior of the
engine. There are, however, abnormal operating circumstances for
such engines which may result in excessive amounts of blowby
escaping into the crankcase and indicate the possible or potential
failure of certain engine parts. Continued operation under such
conditions may cause serious engine damage and might lead to a
crankcase explosion. Under such conditions, it is desired that the
excess flow of blowby into the crankcase will create a positive
pressure that will be detected by a crankcase-connected pressure
detector that is provided to actuate an engine shutdown
mechanism.
To maintain the desired crankcase vacuum, it has been known to
provide means to exhaust the crankcase vapors, including the blowby
gases which escape past the piston rings into the crankcase,
through suitable conduit means into either the engine inlet or
exhaust systems or, in some cases, to a separate exhaust
device.
A typical system for recirculation of the crankcase gases into the
engine inlet which is used on certain two-cycle diesel engines
includes an engine-mounted oil separator that communicates with the
crankcase and a conduit connecting the oil separator with the
engine combustion air inlet, at a point between the air filtration
means and the charging air blower. A similar system is shown, for
example, in U.S. Pat. No. 2,688,316 Brill. In such systems it is
known to include a restrictive orifice in the conduit to prevent an
excessive flow of vapors through the system with the resultant
carryover of oil from the oil separator. The orifice limits normal
flow and provides for the development of positive pressure in the
crankcase under abnormal conditions of high blowby. A pressure
actuated protective device may be provided to actuate engine
stopping means in response to the crankcase pressure, thus
preventing continued abnormal operation of the engine. An example
of such a protective device is shown in U.S. Pat. No. 3,246,641
Goehring.
Generally, the application of fixed orifices in the above-indicated
manner has been limited to systems where the variation in inlet
depression (negative pressure or vacuum) upstream of the blower is
relatively small. Where significant variations in inlet depression
exist, as in engines having the charging air supplied by a
turbocharger, the above-described system is not especially suitable
due to the excessive variations in flow through the system which
would be encountered under normal operating conditions. A number of
crankcase ventilation systems are knwon in the prior art which
provide for the maintenance of a suitable vacuum in the engine
crankcase under the control of a regulating valve. See, for
example, U.S. Pat. Nos. 3,263,660 Hyde and 3,380,441 Lewis. While
such systems might be suitable for the control of crankcase
ventilation flow in large locomotive engines and the like under
their normal operating conditions, this would not be true under the
abnormal conditions caused by excessive blowby indicative of an
engine malfunction and the possible occurrence of a crankcase
explosion. Under such conditions, the regulating valves of the
prior art systems would respond to the increased crankcase pressure
by opening completely. This action would permit the flow through
the ventilation conduit to become excessive and deter the buildup
of pressure in the crankcase which is necessary to actuate the
crankcase pressure detector of the protective device and shut down
the engine so as to prevent or minimize damage due to the abnormal
conditions.
SUMMARY OF THE INVENTION
The present invention provides a crankcase ventilation system which
meets the requirements of large locomotive engines and the like
where it is desired to ventilate the crankcase into the engine
induction system upstream of the charging air blower or
turbocharger. The system is particularly adapted for conditions
where a significant variation in inlet depressions exists and it is
desired to maintain a suitable vacuum in the crankcase under normal
operating conditions but to permit the buildup of a crankcase
pressure to actuate the engine shutdown mechanism under conditions
of abnormally high engine blowby or other similar indication of
actual or potential engine failure.
In essence, the system of the present invention involves the
combination of both fixed restriction means and a regulating valve
in series in the crankcase ventilation conduit with the fixed
restriction located upstream of the regulating valve. Preferably,
an orifice plate is used as the fixed restriction and the
regulating valve is arranged to normally maintain a relatively
constant vacuum in the space between the orifice plate and
regulating valve. To provide flexibility of the system for
application to various engine sizes and types, provision may be
made for the alternative use of various sizes of fixed orifices.
Additionally, the regulating valve may be made adjustable to permit
varying the controlled pressure upstream thereof. The combination
of the present invention provides for maintenance of crankcase
vacuum in a desired range under normal engine operating conditions
as controlled primarily by movement of the regulating valve while
permitting a buildup of pressure in the crankcase to actuate the
engine protector under conditions of excessive blowby or a
crankcase explosion.
These and other advantages of the present invention will be more
clearly understood from the following description of a preferred
embodiment taken together with the accompanying drawing.
BRIEF DESCRIPTION OF THE DRAWING
In the drawing:
FIG. 1 is a side view of an internal combustion engine having a
crankcase ventilation system according to the invention; and
FIG. 2 is a diagrammatic illustration of the crankcase ventilation
system as applied to the engine of FIG. 1.
DESCRIPTION OF THE PREFERRED EMBODIMENT
In the drawing, numeral 10 generally indicates an internal
combustion engine which may be of any suitable type, but in the
present instance is shown as a large two-cycle diesel engine of a
type commonly used to power diesel locomotives and for other
purposes. Engine 10 includes a crankcase 12 which in known manner
provides an enclosure for the engine cylinders and operating
components. Within the crankcase, blowby gases from the engine
cylinders mix with oil vapors and other gases to form a mixture of
crankcase vapors which it is desirable to draw from the
crankcase.
Mounted on the engine crankcase is a turbocharger 14 which is
driven by the engine exhaust supplemented by an internal gear
train, not shown, to supply combustion air to the interior of the
engine for delivery to the cylinders. Turbocharger 14 includes an
air inlet 16 which connects through suitable conduit means 18 with
an air cleaner housing 20. The engine crankcase further carries a
protective device including a pressure detector 22 which is
arranged to be actuated by a predetermined positive pressure in the
crankcase to operate means for shutting down the engine in known
manner. The crankcase pressure detector may, for example, be of the
type shown in U. S. Pat. No. 3,246,641 Goehring.
Engine 10 is further provided with a crankcase ventilation system
which will give the desired crankcase pressure characteristics. The
crankcase ventilation system is generally indicated by numeral 24
and is shown schematically in FIG. 2. System 24 includes an oil
separator 26 which is preferably mounted directly on the engine
crankcase to return thereto excess oil separated from the crankcase
vapors. If desired, the oil separator 26 may be spacedly mounted
from the crankcase and connected thereto by a conduit. Oil
separator 26 is connected with the turbine inlet 16 through
suitable conduit means 28 that also communicate, through the oil
separator, with the engine crankcase 12. A fixed orifice plate 30
is mounted within conduit 28 downstream of the oil separator to
provide a resistance to excessive fluid flow through the system. A
suitable regulating valve 32 is also mounted within the conduit 28
intermediate orifice plate 30 and the turbine inlet.
Regulating valve 32 may be of any suitable type which is adapted to
be responsive to pressure upstream of the valve so as to control
fluid flow as a function of such pressure. The valve is arranged so
that during engine operation it controls the flow of fluids through
the ventilation conduit to provide during normal operation a
predetermined maximum vacuum in the conduit 28 between the orifice
plate and the regulating valve. One type of valve which might be
usable for this purpose is shown in the previously mentioned U. S.
Pat. No. 3,263,660 Hyde, although any other suitable valve
arrangement may be utilized.
In a specific example, the engine involved is such that vacuum in
the turbocharger air inlet may vary between almost zero to 50
inches of water under various operating conditions. The valve 32 is
arranged to control the upstream vacuum between the valve and the
orifice plate at a maximum of about 10 inches of water. The orifice
in plate 30 is then sized so that in the normal range of flow the
pressure drop therethrough will result in a maximum vacuum of about
four to 5 inches of water in the engine crankcase under normal
blowby flow conditions.
In operation, vacuum created in the turbocharger air inlet by the
drawing of inlet air through the air filters causes a pressure
differential that establishes a flow of crankcase vapors through
the ventilation system and into the turbocharger air inlet. When
inlet vacuum is low, as at engine idle, regulating valve 32 remains
fully open, permitting free flow of vapors therethrough and the
pressure drop through orifice plate 30 is small.
As engine speed and load are increased, the vacuum between the
valve 32 and orifice plate 30 increases until the predetermined
control pressure is reached, after which the valve closes as
necessary to limit the maximum vacuum between the valve and orifice
plate to the desired control pressure (e.g. 10 inches of water) no
matter how high the vacuum in the turbocharger air inlet becomes.
Pressure drop through the orifice plate 30 remains relatively low
(maximum of about 5 inches of water) under blowby conditions
encountered during normal operation, since the orifice is sized not
to greatly restrict normal vapor flow.
However, in the case of abnormal engine operation, such as might be
caused by a cracked piston or a scored liner allowing excessive
blowby to escape from the engine cylinders into the engine
crankcase, the resulting increased flow will be increasingly
restricted by the orifice plate 30 until a positive pressure is
developed in the engine crankcase. This pressure will, at a
predetermined value, actuate the crankcase pressure detector 22
which will in turn shut down the engine so that it may be inspected
to determine the cause of the faulty operation.
The limitation of the maximum downstream vacuum acting on the
orifice plate through the action of the regulating valve is
important since it permits the use of a sufficiently large orifice
to have only a small effect on normal blowby flows. The arrangement
reduces the pressure differential required across the orifice to
develop a pressure in the crankcase under abnormal high blowby
conditions which thus allows the use of a larger, less restrictive,
orifice than would be possible if the turbocharger air inlet vacuum
was allowed to act directly on the orifice plate.
The function of the orifice plate in the system could, if desired,
be performed by some other type of fixed resistance suitably
arranged to provide the proper restriction to flow in relation to
the normal and abnormal engine operating conditions which might be
encountered. Such resistance might be provided merely by sizing the
connections to the regulating valve to adequately restrict the
passage of excessive flow for the particular engine arrangement.
Preferably, where the devices making up the crankcase ventilating
system are intended to be used on a line of engines of differing
sizes and blowby characteristics, an arrangement will be utilized
with provision being made for the system to accept any one of a
number of different orifice plates with various sized orifices,
depending on the engine application. In this way a single
regulating valve can be made to serve for application to any of a
number of different engines, with the system being properly
balanced by the use of an orifice sized for the particular
application. Also, if desired, the regulating valve may be made
adjustable to provide for selection of the upstream controlled
pressure best suited for a particular application.
It should be apparent that numerous other variations and changes
could be made in the crankcase ventilation system disclosed herein
without departing from the inventive concepts involved.
Accordingly, it is intended that the invention be limited only by
the language of the following claims.
* * * * *