U.S. patent number 3,730,149 [Application Number 05/108,265] was granted by the patent office on 1973-05-01 for drain return for engine.
This patent grant is currently assigned to Outboard Marine Corporation. Invention is credited to Peter W. Brown.
United States Patent |
3,730,149 |
Brown |
May 1, 1973 |
DRAIN RETURN FOR ENGINE
Abstract
Disclosed herein is a two-stroke internal combustion engine with
a drain return system comprising a drain return line which is
supported by wall means defining a fuel supply passage and which
extends from a crankcase and includes an end part terminating in
adjacently spaced opposing relation to one portion of the wall
means, whereby drains exiting from the drain return line splash
against the wall portion and are broken into droplets for delivery
to the engine cylinder.
Inventors: |
Brown; Peter W. (Zion, IL) |
Assignee: |
Outboard Marine Corporation
(Waukegan, IL)
|
Family
ID: |
22321187 |
Appl.
No.: |
05/108,265 |
Filed: |
January 21, 1971 |
Current U.S.
Class: |
123/73R;
123/DIG.2; 123/73PP; 123/73A; 123/73B; 123/572 |
Current CPC
Class: |
F02M
33/04 (20130101); F02B 61/045 (20130101); Y10S
123/02 (20130101); F02B 2075/025 (20130101) |
Current International
Class: |
F02M
33/00 (20060101); F02M 33/04 (20060101); F02B
61/00 (20060101); F02B 61/04 (20060101); F02B
75/02 (20060101); F02b 033/04 () |
Field of
Search: |
;123/73R,73A,73B,73SC,73PP,DIG.2,119B,136 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Burns; Wendell E.
Claims
What is claimed is:
1. A two-stroke internal combustion engine including a cylinder,
wall means defining a fuel supply passage communicating with said
cylinder, and a drain return line communicating with a source of
fuel drains and supported by said wall means and including an end
part having a bore with a diameter less than about one-eighth of an
inch and terminating in spaced opposing relation to one portion of
said wall means at a distance less than about one-eighth of an
inch, whereby drains exiting from said return line splash against
said wall portion and are broken into droplets for delivery to said
cylinder.
2. An engine in accordance with claim 1 wherein said engine also
includes a crankcase, wherein said fuel supply passage comprises a
transfer passage communicating with said cylinder and said
crankcase, and wherein said drain return line communicates with
said crankcase during periods of positive pressure in said
crankcase.
3. An engine in accordance with claim 2 wherein said drain return
line has a bore with an internal diameter of approximately
one-sixteenth of an inch extending substantially from said
crankcase to said transfer passage.
4. An engine in accordance with claim 1 wherein said end part is
spaced at about one-sixteenth of an inch from said wall
portion.
5. An engine in accordance with claim 1 wherein said drain return
line comprises a tube including said end part and having a bore
with a diameter of about one-sixteenth of an inch.
6. An engine in accordance with claim 1 wherein said drain return
line includes a conduit and a fitting comprising a bolt which
includes a head and an axial bore and which is threaded into one
section of said wall means and a tube fixed in said bore and
including, at the end opposite from said head, said end part and,
at the end thereof adjacent said head, a nipple connected to said
conduit.
7. A two-stroke internal combustion engine including a cylinder, a
crankcase, wall means defining a fuel transfer passage
communicating between said crankcase and said cylinder and a drain
return line supported by said wall means and extending from and
communicating with said crankcase, said drain return line including
a conduit having an axial bore communicating with said crankcase
and a fitting comprising a bolt which includes a head and an axial
aperture and which is threaded into one section of said wall means,
and a tube which is fixed in said bolt aperture, which includes at
the end thereof adjacent said head, a nipple connected to said
conduit, which includes, at the other end, an end part terminating
in opposed relation to one portion of said wall mans at a distance
therefrom of about 1/16 of an inch, and which has an axial bore
communicating with said conduit axial bore, said axial bores having
a diameter of about 1/16 of an inch.
Description
BACKGROUND OF THE INVENTION
Two stroke engines commonly experience an accumulation of fuel and
lubrication "drains" in the low point or sump of the engine
crankcase. The desirability of recycling or returning such drains
to the engine cylinder for ultimate combustion has been known for
some time. Such recycling is especially important in avoiding
pollution associated with outboard motors as, in the past, such
drains have commonly been wasted overboard into the body of water
in which the outboard motor was operating.
Prior arrangements for returning or recycling drains are disclosed
in the U.S. Pat. No. 2,717,584 to Upton issued Sept. 13, 1955, the
U.S. Pat. No. 3,128,748 to Goggi issued Apr. 14, 1964, and in the
U.S. Pat. No. 3,132,635 to Heidner issued May 12, 1964.
The above identified disclosures all rely in some part on the
incoming charge to carry the drains into the cylinder for
combustion. However, when the drains are supplied to the charge in
the form of a stream, less than maximum conditions are presented
for effective transportation of the drains by the incoming charge
into the cylinder for combustion.
SUMMARY OF THE INVENTION
The invention provides an arrangement for breaking up a stream of
drains into droplets so as to facilitate transportation of the
drains into an engine cylinder for ultimate combustion, either by
way of direct transportation of the droplets by the incoming charge
or by increasing the amount of vaporization of the drains, thereby
to facilitate delivery of such vaporized drains to the engine
cylinder.
In accordance with the invention, there is provided a drain return
line which, in part, is supported by a fuel feeding passage, such
as the transfer passage of a two-stroke engine, and which includes
an end part terminating in closely spaced relation from an opposing
portion of the wall defining the fuel feeding passage.
Also in accordance with the invention, the drain return line
communicates with the crankcase of a two-stroke engine and has, for
substantially the entire length of the return line, a relatively
small diameter. As a consequence, the drains exiting from the end
part of the drain return line are particularly responsive to the
pressure pulses supplied to the return line by the crankcase and,
as a result, drains exit from the end part of the drain return line
in a stream having sufficient velocity to cause splashing when the
stream strikes the closely spaced opposed wall portion. Such
splashing is effective to break the stream up into droplets which
are more readily vaporized and which can be more readily
transported into the cylinder by an incoming fuel charge.
One of the principal objects of the invention is the provision of
an arrangement for more effectively transporting return drains into
an engine cylinder by an incoming fuel-air charge.
Another principal object of the invention is the provision of an
arrangement for causing a returning stream of drains to splash into
a charge of fuel-air traveling toward an engine cylinder, whereby
to break the stream of drains into droplets which can be more
effectively borne to the engine cylinder by the incoming
charge.
Still another principal object of the invention is the provision of
a drain return system including a drain return line which
communicates with the engine crankcase, which has a relatively
small internal bore, and which terminates in closely adjacent
relation to a wall portion defining a fuel feeding passage, whereby
the pressure applied to the drains by the crankcase will cause the
drains to exit from the return line in a stream which splashes
against the wall portion.
Another important object of the invention is the provision of a
drain return system which is economical to construct and to install
and which will provide a long and useful life.
Other objects and advantages of the invention will become known by
reference to the following description and accompanying
drawings.
DRAWING
FIG. 1 is a partially schematic fragmentary sectional view of an
engine embodying various of the features of the invention.
GENERAL DESCRIPTION
Shown in the drawings is a two-stroke engine 11 including an engine
block 13 defining a cylinder 17 having an exhaust port 19 and an
inlet port 21. Reciprocably movable in the cylinder 17 is a piston
23 which is joined to a connecting rod 27. The intake port 21
comprises the terminus of a transfer passage 29 which is defined by
suitable wall means 30 and which constitutes a fuel supply or
feeding passage.
In the particularly disclosed construction, the transfer passage 29
communicates with a crankcase 31 which, in turn, is connected
through reed valves (not shown) with a carburetor (not shown) so as
to periodically pump a fuel-air mixture through the transfer
passage 29 to the cylinder 17. As above described, the construction
is conventional.
As shown, for instance, in the Heidner U.S. Pat. No. 3,132,635
issued May 12, 1964, which is hereby incorporated by reference,
drains which accumulate in the crankcase can be pumped, by reason
of the cyclical pressure pulses occurring in the crankcase, for
return to the engine cylinder and ultimate combustion. Thus, as
shown in FIG. 1, there is provided for the purpose of feeding
drains into the cylinder 17 for ultimate combustion, a drain return
line or duct 41 which communicates with the crankcase 21. In
accordance with the invention, the drain return line 41 includes a
drain fitting 43 comprising a threaded bolt 47 which is secured
into one section 49 of the wall means 30 and which includes an
axial bore or aperture fixedly carrying an axially extending tube
51. At the end of the tube 51 adjacent to the head 53 of the bolt
47, the tube 51 is provided with a nipple 57 which is connected to
a tubular conduit 59 which, in turn, connects with the crankcase
31. The other end of the tube 51 includes an end 61 which
terminates in spaced closely adjacent relation to and in opposing
relation to a portion 63 of the wall means 30. Means such as shims
or washers 67 between the wall section 49 and the bolt head 53, or
other known mechanical arrangements, can be provided for adjustably
locating the end 61 of the tube 51 relative to the wall portion 63
so as to obtain optimum results. In the specifically disclosed
arrangement, the end 61 is spaced from the wall portion 63 by about
one-sixteenth of an inch. At least some of the advantages of the
invention are believed to be obtainable with spacings of up to
about approximately one-eighth of an inch.
In order to minimize the internal volume of the drain return line
41 and thereby to maximize the responsiveness of the drains in the
tube 51 to the pressure pulses supplied to the drain line 41 from
the crankcase 31, and thereby also to maximize the delivery
velocity of the drains from the drain tube 51, in accordance with
the invention, the respective bores 71 and 73 of the tube 51 and
the conduit 59 are relatively small for substantially the entire
distance from the crankcase 31 to the transfer passage 29. In the
particularly disclosed construction, the bores 71 and 73 have a
diameter of approximately one-sixteenth of an inch. At least some
of the advantages of the invention are believed to be obtainable
with bores having diameters of up to about one-eighth of an
inch.
In operation, the discharge velocity of the drains provided as a
result of crankcase pressure and the relatively small diameter of
the bores 71 and 73, as well as the closely adjacent relation of
the end 61 of the tube 51 relative to the wall portion 63, cause
the returning stream of drains to splash when the stream hits the
wall portion 63 and thereby to break up into many small droplets
which can be readily carried, either as particles or as vapor, into
the cylinder 17 by the incoming charge of fuel-air mixture.
Thus, in the disclosed construction, the nozzle length is designed
so as to spray the liquid fuel drainings directly against a
non-water cooled portion of the cylinder wall and directly into the
high velocity gaseous mixture just outside of the cylinder intake
port. The fuel is thereby vaporized and carried into the cylinder
where it is burned with the rest of the mixture.
Various of the features of the invention are set forth in the
following claims.
* * * * *