U.S. patent number 3,893,436 [Application Number 05/469,474] was granted by the patent office on 1975-07-08 for fuel supply system, carburetor for use in the same and method.
Invention is credited to William H. Beekhuis, Jr..
United States Patent |
3,893,436 |
Beekhuis, Jr. |
July 8, 1975 |
**Please see images for:
( Certificate of Correction ) ** |
Fuel supply system, carburetor for use in the same and method
Abstract
Fuel supply system for an internal combustion engine having at
least one cylinder with a moving piston therein to provide a
combustion chamber within the cylinder which is adapted to be
placed in communication with an intake opening by operation of an
intake valve. A carburetor and means for supplying fuel to the
carburetor are provided as a part of the system. The carburetor
includes means forming a wave tube of substantially constant
cross-sectional area with one end open to the atmosphere and with
the other end adapted to be placed in communication with the intake
opening. Means forming an orifice is disposed in the wave tube for
supplying fuel to the interior of the wave tube. Throttle means is
disposed in the wave tube between the region in which the fuel is
introduced and the intake opening. The means for supplying a liquid
fuel to the carburetor includes means for supplying fuel to a level
which approximately just covers the orifice.
Inventors: |
Beekhuis, Jr.; William H. (Los
Altos Hills, CA) |
Family
ID: |
26953293 |
Appl.
No.: |
05/469,474 |
Filed: |
May 13, 1974 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
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268736 |
Jul 3, 1972 |
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Current U.S.
Class: |
123/586; 123/531;
261/44.3; 261/36.2 |
Current CPC
Class: |
F02M
17/02 (20130101); F02B 27/006 (20130101); F02B
27/00 (20130101); F02M 13/02 (20130101); F02M
9/02 (20130101); Y02T 10/12 (20130101) |
Current International
Class: |
F02M
17/02 (20060101); F02B 27/00 (20060101); F02M
9/00 (20060101); F02M 13/00 (20060101); F02M
9/02 (20060101); F02M 13/02 (20060101); F02M
17/00 (20060101); F02m 007/10 () |
Field of
Search: |
;123/119R,119DB,139AW,139AV,52M,52MV ;261/36A,44R |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Other References
Acoustic Vibrations, P. M. Morse et al., Journal of Applied
Physics, Jan. 1938..
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Primary Examiner: Burns; Wendell E.
Assistant Examiner: Reynolds; D.
Attorney, Agent or Firm: Flehr, Hohbach, Test
Parent Case Text
This is a continuation of application Ser. No. 268,736 filed July
3, 1972, now abandoned.
Claims
I claim:
1. A fuel supply system for an internal combustion engine having at
least one combustion chamber which is adapted to be placed in
communication with an intake opening during each intake event,
comprising wall means forming a wave tube having a substantially
unimpeded flow passage with one end open to the atmosphere and with
the other end adapted to be placed in communication with the intake
opening of the internal combustion engine, means forming an orifice
disposed in the wall means forming the wave tube and opening into
the flow passage of the wave tube, means for supplying fuel to the
orifice so that the fuel has a level which will reach the orifice
but will not flow through the orifice solely because of the level
of the fuel with respect to the orifice, and throttle valve means
disposed in the wave tube between the region in which the fuel is
introduced into the wave tube and the intake opening, said throttle
valve means being formed so that a shock wave from the engine can
be propagated down the wave tube to cause fuel to be drawn into the
wave tube through the orifice substantially solely during
propagation of the pressure shock wave along the wave tube and to
atomize the fuel so that the atomized fuel can be carried into the
combustion chamber by the incoming air stream flowing in the wave
tube, the pressure effect of said wave serving as substantially the
sole means for metering fuel from the orifice, said wall means
forming a wave tube including a body, said body being formed with
shock wave terminating means for preventing a shock wave from
traveling substantially more than one round trip in the flow
passage in the wave tube for each intake event.
2. A system as in claim 1 wherein said means for supplying fuel
includes a fuel supply bowl, means for supplying liquid fuel to the
fuel bowl, control means for preventing liquid fuel from being
introduced into the fuel bowl to a level which is significantly
above the orifice and a drain tube connected to the fuel bowl for
draining off excess liquid fuel from the fuel bowl.
3. A system as in claim 2 wherein said drain tube is connected to
the fuel bowl at a position which is above the orifice.
4. A system as in claim 2 wherein said control means for preventing
fuel from being introduced into the fuel bowl to a level which is
significantly above the orifice includes said drain tube.
5. A system as in claim 1 wherein said body has an elongate recess
formed therein with a bore opening into the recess and wherein said
throttle valve is in the form of a throttle plate slidably mounted
in said recess in said body, for movement between throttle open and
throttle closed positions, said throttle plate having an opening
therein adapted to be moved into registration with said bore in
said body so that it is in alignment with and forms a part of the
wave tube when the throttle plate is in the throttle open position
and is out of registration with said bore in said body in the
throttle closed position.
6. A system as in claim 5 together with yieldable means for urging
said throttle plate into a position so that the bore in said body
is occluded by said throttle plate.
7. A system as in claim 6 together with means for moving said
throttle plate so that the opening in said throttle plate is in
registration with said bore in said body against the force of said
yieldable means.
8. A system as in claim 1 wherein said terminating means is in the
form of at least one opening located in the body and establishes
communication between the atmosphere and the flow passage.
9. A system as in claim 5 together with supplemental air bleed
means formed in the body in communication with the flow passage
under the control of the throttle valve.
10. A system as in claim 9 wherein said supplemental air bleed
means is provided by a slot in the body open to the recess in the
body and a hole in the body in communication with the slot and
being open to the atmosphere.
11. In a carburetor, a body having a bore therein, said body being
formed with a recess and a throttle plate slidably mounted in said
body, said throttle plate having a hole therein adapted to be moved
into and out of registration with said bore in said body by
movement of the throttle plate, said bore in said body and said
hole in said throttle plate being adapted to form a substantially
unimpeded flow passage, said body being formed with terminating
means extending substantially transversely to the major axis of the
flow passage and establishing communication between the bore in
said body and the atmosphere for preventing a shock wave in the
flow passage from traveling substantially more than one round trip
in the flow passage in the wave tube for each intake event.
12. A carburetor as in claim 11 wherein said terminating means is
downstream the throttle plate.
13. A carburetor as in claim 11 together with means for yieldably
urging said throttle plate into a position in which said throttle
plate occludes said bore in said body.
14. A carburetor as in claim 13 together with means for moving said
throttle plate into a position in which said hole is in alignment
with said bore against the force of said yieldable means.
15. A carburetor as in claim 11 together with means forming an
orifice in the body for admitting liquid fuel into said bore in
said body.
16. A carburetor as in claim 15 together with a fuel bowl having a
chamber in communication with said means forming the orifice.
17. A carburetor as in claim 16 together with means for controlling
the level of the liquid fuel in said chamber so that it is
generally at the same level as the orifice.
18. In a fuel supply system for an internal combustion engine of a
type having a plurality of combustion chambers and having intake
openings adapted to be placed into communication with the
combustion chambers during intake events, the system comprising
separate carburetor means for each of said intake openings, each of
said carburetor means including means forming a wave tube having a
flow passage therein with one end open to the atmosphere and the
other end in communication with an intake opening, means forming an
orifice disposed in the wave tube for supplying fuel to the
interior of the wave tube, throttle valve means disposed in the
wave tube between the region in which the fuel is introduced and
the intake opening, means for supplying liquid fuel to the orifice
at a level so that fuel will not flow through the orifice solely
under the force of gravity and terminating means in the means
forming a wave tube for preventing a shock wave in the flow passage
from traveling substantially more than one round trip in the flow
passage for each intake event.
19. A system as in claim 18, together with air cleaner means for
filtering the air prior to the time it is supplied to the wave
tubes.
20. A system as in claim 18 wherein as a part of said throttle
valve means certain of said carburetors are provided with a common
throttle plate, said throttle plate having an opening therein for
each of said certain carburetors.
21. In a method for introducing a fuel and air mixture into the
combustion chamber of an internal combustion engine, in which shock
waves are formed and in which a column of air flows into the
combustion chamber during each intake event, providing a supply of
liquid fuel adjacent the column of air propagating a shock wave
created in the engine outwardly through the column of air to cause
fuel to be drawn into the column of air and to be atomized so that
the atomized fuel can travel with the column of air, providing a
reflected shock wave which travels inwardly through the column of
air, and substantially attentuating the reflected shock wave so
that there is substantially only one round trip travel of the shock
wave from and back to the engine during each intake event.
22. A method as in claim 21 together with the step of confining the
moving column of air in a wave tube having a substantially
unimpeded flow passage.
23. A method as in claim 22 together with the step of controlling
the time delay between the reflected shock wave and the outgoing
propagated shock wave by controlling the length of the wave
tube.
24. A method as in claim 22 together with the step of controlling
the pressure amplitude of the outgoing and reflected shock waves by
controlling the cross-sectional area of the wave tube.
25. A system as in claim 1 wherein said means for maintaining the
level of liquid fuel with respect to said orifice comprises a fuel
bowl having fuel therein at a predetermined level with an air space
above the fuel, a sealed fuel supply vessel located at a level
above said fuel bowl, means forming a fuel feed passage connecting
said fuel bowl and said fuel supply vessel, means forming a control
passage between the air space above the fuel in said fuel supply
vessel and down to the predetermined level in the fuel bowl, and
means forming a vent passage in the fuel bowl between the air space
above the fuel in said fuel bowl and the atmosphere.
26. A system as in claim 1 wherein said means for maintaining the
level of liquid fuel with respect to said orifice comprises a fuel
bowl having fuel therein at a predetermined level with an air space
above the fuel, a fuel supply vessel located at a level below said
fuel bowl, means forming a fuel feed passage between said fuel bowl
and said fuel supply vessel, fuel pump means connected in said
means forming a fuel passage for supplying fuel from said vessel to
said bowl, means forming a fuel drain passage connected between
said fuel bowl and said fuel supply vessel, said means forming the
drain passage being positioned in the bowl so that a predetermined
fuel level is maintained in the bowl, and means in the fuel bowl
forming a vent passage between the air space above the fuel in said
fuel bowl and the atmosphere.
27. A system as in claim 26 together with a fuel flow regulator
connected into said means forming said fuel feed passage and which
is responsive to engine fuel demand whereby said regulator prevents
excess fuel recirculation.
28. A fuel supply system for an internal combustion engine having
at least one combustion chamber which is adapted to be placed in
communication with an intake opening during each intake event,
comprising wall means forming a wave tube having a flow passage for
a medium therein with one end open to the atmosphere and with the
other end adapted to be placed in communication with the intake
opening of the internal combustion engine, means forming an orifice
disposed in the wall means forming the wave tube and opening into
the flow passage therein, said flow passage being formed so that
the maximum pressure effect at the orifice due to a shock wave
generated by the engine in said medium in the flow passage is
substantially greater than the maximum pressure effect at the
orifice due to the velocity of said medium in the flow passage,
said wall means forming a wave tube including a body, said body
being formed with shock wave terminating means for preventing a
shock wave from traveling substantially more than one round trip
along the flow passage in the wave tube for each intake event,
means for supplying fuel to the orifice so that the fuel will be
introduced into the flow passage in the wave tube through the
orifice substantially only in response to said pressure effects at
the orifice, and throttle valve means disposed in the wave tube
between the region in which the fuel is introduced into the flow
passage in the wave tube and the intake opening of the internal
combustion engine.
29. In a method for introducing a fuel and air mixture into a
combustion chamber of an internal combustion engine, in which a
shock wave is generated during an intake event in a medium confined
by wall means defining an intake passage, the improvement of
substantially terminating the progress of the shock wave after one
round trip travel from and back to the engine of the shock wave in
said medium for each intake event.
30. A method as in claim 29 together with the step of introducing
fuel into said medium substantially solely in a region adjacent the
wall means defining an intake passage.
Description
BACKGROUND OF THE INVENTION
This invention relates to fuel supply systems, carburetor for use
therein and a method for metering and atomizing liquid fuel for use
with internal combustion engines.
Heretofore, many different types of fuel supply systems and
carburetors have been provided. However, such systems and
carburetors for use therein have suffered from a lack of wide
operating ranges. In addition, such systems and carburetors have
suffered from inadequate performance often caused gy inefficient
atomization of the fuel and with undesirable pressure drops. There
is, therefore, need for a new and improved fuel supply system,
carburetor for use therein and a method which overcomes these
disadvantages.
SUMMARY OF THE INVENTION AND OBJECTS
The fuel supply system is for use with an internal combustion
engine having at least one cylinder with a moving piston therein to
provide a combustion chamber within the cylinder which is adapted
to be placed in communication with an intake opening by operation
of an intake valve. Means is provided which forms a wave tube of
substantially constant cross-sectional area with one end open to
the atmosphere and with the other end adapted to be placed in
communication with the intake opening. Means forming an orifice is
disposed in the wave tube for supplying fuel to the interior of the
wave tube. Fuel supply means supplies fuel at a level which covers
the orifice. The cross-sectional area of the wave tube is
sufficiently small to permit shock wave metering and atomization of
fuel supplied to the wave tube. Throttle means is disposed in the
wave tube between the region in which the fuel is introduced and
the intake opening. The throttle valve is formed so that when it is
in the fully open position, there is substantially no restriction
to the airflow through the wave tube.
In general, it is an object of the present invention to provide a
fuel supply system, carburetor for use therein and method which
makes possible a wide range of operation.
Another object of the invention is to provide a system, carburetor
and method of the above character in which marked pressure drops
are eliminated.
Another object of the invention is to provide a system, carburetor
and method of the above character in which emission of unburned
hydrocarbons and carbon monoxide is substantially reduced.
Another object of the invention is to provide a system, carburetor
and method of the above character in which the air-to-fuel ratios
can be varied through wide ranges if desired.
Another object of the invention is to provide a system, carburetor
and method of the above character which are applicable to internal
combustion engines whether reciprocating or rotary and whether
two-stroke or four-stroke cycle.
Another object of the invention is to provide a system, carburetor
and method of the above character in which the correct amount of
fuel and the highest possible degree of atomization is
provided.
Another object of the invention is to provide a system, carburetor
and method of the above character which are applicable to
multi-cylinder engines.
Another object of the invention is to provide a system, carburetor
and method of the above character which are relatively simple.
Another object of the invention is to provide a system, carburetor
and method of the above character which make possible improved
throttle response.
Another object of the invention is to provide a system, carburetor
and method of the above character which make possible the efficient
use of fuel.
Another object of the invention is to provide a system, carburetor
and method which can be implemented relatively inexpensively.
Another object of the invention is to provide a system, carburetor
and method of the above character in which shock waves are used for
causing intake of fuel and atomizing the same.
Additional objects and features of the invention will appear from
the following description in which the preferred embodiments are
set forth in detail in conjunction with the accompanying
drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a side elevational view of the carburetor utilized in the
fuel supply system incorporating the present invention.
FIG. 2 is a top plan view looking along the line 2--2 of FIG.
1.
FIG. 3 is a side elevational view looking along the line 3--3 of
FIG. 1.
FIG. 4 is a cross-sectional view taken along the line 4--4 of FIG.
3.
FIG. 5 is a cross-sectional view taken along the line 5--5 of FIG.
1.
FIG. 6 is a cross-sectional view taken along the line 6--6 of FIG.
4.
FIG. 7 is a top plan view of the carburetor similar to FIG. 2 but
showing additional details.
FIG. 8 is a crosS-sectional view taken along the line 8--8 of FIG.
7.
FIG. 9 is a schematic illustration of a fuel bowl with which air
control is utilized.
FIG. 10 is a schematic illustration showing a fuel supply system
incorporating the present invention utilizing air control.
FIG. 11 is a schematic illustration showing a fuel bowl with which
pump control is utilized.
FIG. 12 is a schematic illustration of a fuel supply system
incorporating the present invention utilizing pump control.
FIG. 13 is a front elevational view partly in cross section of a
multi-cylinder internal combustion engine of a four-stroke cycle
having a fuel supply system mounted thereon incorporating the
present invention.
FIG. 14 is a cross-sectional view taken along the line 14--14 of
FIG. 13.
FIG. 15 is a cross-sectional view showing an internal combustion
engine of the two-stroke cycle and having a fuel supply system
mounted thereon incorporating the present invention.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
In FIGS. 1 through 8 there is shown a carburetor 21 for use in a
fuel supply system incorporating the present invention. This
carburetor 21 has the principal novelty in the system and consists
of a body or housing 22 and a base 23 which can be formed of a
suitable material such as an aluminum alloy sand casting. If
desired, die cast aluminum can be utilized for high volume
production. Alignment pins 24 are provided either in the body or
the base 23 and are provided for aligning the base 23 on the body
22. The base and the body are fastened together in a suitable
manner such as by the use of Allen head screws 26. They extend
through the body 22 and are threaded into the base 23 as shown.
The body 22 is provided with a cylindrical bore 28 which is of
uniform or constant cross-sectional area. The bore 28 opens into a
generally planar oval-shaped recess 29 (see FIG. 5) which receives
a throttle plate or a slide valve 31. The slide valve 31 is formed
of a suitable material such as a phenolic laminate, Nema grade LE.
The slide valve 31 is provided with a bore 32 which has
substantially the same diameter as the bore 28 provided in the body
or housing 22. The base 23 is also provided with a bore 33 which is
in axial alignment with the bore 28 and is of substantially the
same size as the bore 23. As can be seen from the drawing, the
slide valve 31 is adapted to be moved between a throttle-full open
position in which the bore 32 is in axial alignment or registration
with the bores 28 and 33 and a throttle-closed position in which
the slide valve 31 occludes communication between bores 28 and
33.
Means is provided for retaining the slide valve 31 in the
throttle-closed position and consists of a coil spring 36 which has
one end seated in a well 37 provided in the slide valve 31 and
having the other end engaging the wall forming the recess 29 and
encircling a tube 38 mounted in the body (see FIG. 4). Means is
provided for causing movement of the slide valve 31 between the
throttle-closed position and the throttle-open position and
consists of a cable 41 which extends through the sleeve 38, through
the coil spring 36 and is fastened into a counterbore 42 in the
slide valve 31 by a screw 43.
A tube 45 of a substantially constant or uniform cross section is
provided which has an outer flared end portion 46a. As shown in
FIG. 4, the tube 46 is secured within a bore 47 provided in the
body 22. As shown in the drawings, the tube 46 is cylindrical and
has a flow passage 48 extending therethrough which has a diameter
which is substantially identical to the diameter of the bore 28 in
the body 22 and the bore 33 provide what may be called a "wave
tube" of a substantially constant or uniform cross-sectional area
extending completely through the carburetor and which is sized as
hereinafter described.
Means is provided which forms a fuel supply orifice in the vicinity
of the interior of the wave tube between the ends of the wave tube.
Thus as shown in FIG. 4, a fitting 51 is threaded into the body 22
and into the tube 46 as shown in FIG. 4. The fitting 51 is provided
with a conical inlet recess 52 which opens into a small centrally
disposed orifice 53. The orifice 53 opens into a downstream passage
or channel 54 in the fitting which opens into and is in
communication with the passage 48 in the tube 46. As can be seen
from FIG. 4, the exterior end of the fitting 51 and the outer end
of the passage or channel 54 are generally flush with the inner
cylindrical surface defining the passage 48. The channel 54 extends
in a direction at right angles to the axis of the passage 48. Also,
the downstream channel 54 is positioned ahead of the slide valve 31
and is spaced from the inlet end of the tube 46.
The inlet recess 52 of the fitting 51 opens into the interior
chamber 56 of a fuel bowl 57. The bowl 57 is formed of a suitable
material such as an aluminum sand casting. It is provided with a
pair of ears 58 (see FIG. 3) which are secured to the main body 22
by Allen head screws 59. A cap 61 closes the open end 62 of the
bowl 57. The cap 61 is provided with a small vent hole 63 for
venting the interior of the chamber 56 to the atmosphere. Means is
provided for introducing a liquid fuel such as gasoline into the
chamber 56 of the bowl 57 and includes a fill tube 66 which is
mounted in the side wall of the bore 57. The fill tube 66 has an
inner conically-shaped end which has a small inlet opening 67
formed therein. A control tube 68 is mounted in the cap 61 and also
has an inner tapered conical end which has a small opening 69
formed therein. A drain tube 71 is mounted in the side wall of the
bowl and has its inlet end open to the interior of the bowl. The
fill tube 66 is normally positioned at a level which would be below
the level of the fuel within the chamber 56. The control tube 68 is
positioned in such a manner so that the opening 69 is only a slight
distance above the axis of the orifice 53 so that the fuel level is
just slightly above the orifice. The drain tube 71 is normally
positioned in such a manner so that it would be above the normal
liquid fuel level within the bowl 57.
The carburetor 21 is adapted to be mounted on an internal
combustion engine 76 of a conventional type as shown in FIG. 3. As
is well known to those skilled in the art, such internal combustion
engine is provided with an engine block 77 having a piston (not
shown) which reciprocates or moves therein. The engine block 77 is
provided with an inlet passage 78 which is in controlled
communication through an inlet valve 79 with the combustion chamber
provided above the piston. The carburetor 21 is mounted in a
suitable manner such as by a pair of screws 81 which extend through
the base 23 and are threaded into the engine block 77. As will be
noted from FIG. 8, the passage 78 has substantially the same size
as the wave tube for a purpose hereinafter described.
A schematic illustration of the fuel bowl 57 provided in the
carburetor 21 utilizing air control is shown in FIG. 9. A schematic
illustration of the manner in which fuel is supplied to the bowl 57
is shown in FIG. 10. As shown in FIG. 10, the fuel is carried in a
tank 86 formed of a suitable material such as steel or fiberglass.
The tank 86 is thermally insulated in a suitable manner such as by
a layer 87 of rigid polyurethane foam which may be provided with an
epoxy overcoat. The tank 86 is provided with an air tight filler
cap 88. Fuel 89 is provided in the tank which flows through an
outlet pipe 91 and through a shut-off valve 92 through a pipe 93 to
a hose 94 which is connected to the fill tube 66. Fuel 89 flows
into the chamber 56 from the fill tube 66 by force of gravity until
the opening 69 in the control tube 68 is occluded by the liquid
fuel 89. The control tube 68 is connected by a hose 96 which is
connected to a tube 97 mounted on the tank 86 and which enters the
tank near the fill cap 86 and is in communication with the space 98
in the upper portion of the tank as shown in FIG. 10.
As soon as the opening 69 in the control tube 68 is occluded, air
can no longer pass into the space 98 above the liquid fuel 89 so
that within a very short time, a partial vacuum or a below
atmospheric condition is created in the space 98 which prevents
further flow of fuel from the tank 86. In the event there is
overfilling of the chamber 56, the excess fuel will pass through
the drain tube 71 after which it can be returned to the tank 86 if
so desired. Fuel 89 from the chamber 56 is metered through the
orifice 53 into the carburetor as hereinafter described.
As pointed out previously, the fuel flows into the bowl until the
tip of the control tube is covered and a partial vacuum is
generated in the air space 98 above the fuel in the tank. The
pressure difference between atmospheric and the air space in the
tank is determined by the density of the fuel in the tank times the
acceleration of gravity times the difference in height between the
fuel level in the tank and the fuel level in the bowl.
In connection with the fuel supply bowl, it is always important
that the fuel level be at a level which is just slightly above the
orifice 53 so that fuel can be readily drawn into the orifice 53
when the shock wave passes the orifice.
It has been found that the fill and control orifices or openings 67
and 69 should be approximately the same diameter when gasoline is
being utilized as a fuel. By establishing a relationship between
the orifice sizes and the surface area of fuel in the bowl,
overshooting is prevented and maximum accuracy is provided with a
predetermined fuel feed rate requirement.
In providing the fitting 51, it has been found that it is desirable
to provide a conical entry for the inlet recess 52 and a
length-to-diameter ratio of approximately 0.7 for the orifice 53.
The downstream channel or bore 54 preferably has an area which is
approximately 10 times the cross-sectional area of the orifice
53.
In mounting the careburetor on the engine, it is important that the
carburetor 21 be mounted in such a manner that the bowl with its
fitting 51 have the inlet orifice 53 of the fitting point in a
forward direction or in the direction of movement of the vehicle in
which the engine is mounted so that when the vehicle accelerates, a
change in fuel level will be in a positive direction so that the
orifice 53 will not be starved of fuel.
A phenolic has been chosen for the slide valve because it has a
temperature coefficient of expansion which is very similar to that
of aluminum alloy castings. In addition, since gasoline is a very
poor lubricant, it is desirable to utilize a material for the slide
valve which will not bind or stick in its movement in the
carburetor. Therefore, preferably, the material should be
non-metallic.
Operation and use of the carburetor 21 with a fuel system of the
type herein described in conjunction with an internal combustion
engine may now be briefly described. Let it be assumed that the
slide valve or throttle plate 31 has been moved to a full open
position or throttle-open position so that the bore 32 provided
therein is in alignment with the bores 33 and 28 whereby there is
provided a wave tube of substantially constant cross section
extending from the inlet port 78 of the internal combustion engine
to which the carburetor is connected to the atmosphere. As is well
known to those skilled in the art, a shock wave is created by the
combination of piston motion and sudden opening of the inlet valve
79. It has been found that the specific form of the inlet valve or
the specific form of the cylinder has relatively little effect on
the generation of the shock wave other than to slightly modify the
shape of the same. This shock wave is created by these two features
of engine operation and is propagated down the intake passage 78
and down the wave tube formed by the bore 33,, the bore 32, the
bore 28 and the passage 48 at the velocity of sound in air. The
shock wave pressure does not differ markedly in pressure from
atmospheric pressure to which the outlet end of the tube 46 is
exposed. As hereinafter pointed out, the design parameters for the
wave tube are chosen such that the shock wave pressure will not be
in excess of 10% from that of atmospheric pressure.
During the time that the shock wave is being propagated, it should
be appreciated that there is a relatively steady state airflow
entering the wave tube from the inlet end of the wave tube which
passes thrugh the wave tube as a moving column of air of generally
uniform cross section and then passes into the inlet passage 78
past the inlet valve 79 into the combustion chamber above the
piston. During the time this is occurring, the shock wave is being
propagated outwardly from the tube through the column of air and as
it passes the flow channel 54, it will pump fuel through the
orifice 53 and will atomize the same into very fine droplets so
that it will be carried by the moving column of air into the
combustion chamber above the piston. The amount of fuel which is
atomized is dependent upon the time that the shock wave is
effective and is directly determined by the length of the wave
tube. The outgoing shock wave is of the correct sign of pressure to
meter fuel from the orifice 53 and to atomize the same so that it
can be carried to the engine by the steady state air stream. The
outgoing shock wave propagates outwardly until it reaches the end
of the tube at which time a reflected wave is created which is of
the opposite sign of pressure which propagates as an ingoing wave.
Since this shock wave has a pressure of the incorrect sign, no fuel
will be metered from the orifice 53 when this wave passes the
orifice 53. This ingoing wave will not have any effect on the fuel
which has already been metered out of the orifice 53 by the
outgoing wave because the atomized fuel has already been carried
inwardly toward the engine combustion chamber. This will always be
true because the outgoing and ingoing waves are opposite in sign
and will be delayed in time with respect to each other.
The length of time required for the incoming wave to reach the flow
channel 54 is determined by the length of the tube and the speed of
sound in air. As is hereinafter explained, it has been found
desirable to select the length of the wave tube such that the round
trip time for sound to travel in the wave tube in air corresponds
to approximately 40.degree. of crankshaft travel at the maximum
useful engine speed.
In considering the design of the wave tube, it should be considered
that the degree of atomization of a liquid fuel in air is dependent
upon the relative velocity between the liquid fuel and the air. As
this velocity becomes an appreciable fraction of the velocity of
sound, both the mean drop size and the variation in drop size
decrease to small values, dependent upon the surface tension of the
fuel. For this reason, it is desirable to atomize fuel at a sonic
velocity if possible to thereby insure the maximum degree of
atomization of the liquid fuel.
In considering the wave tube utilized in the present carburetor as
one having a constrant or uniform cross-sectional area and having a
steady volume air flow rate q, certain determinations can be made.
Neglecting friction, the steady-state pressure
p = q.sup.2 d/2A.sup.2
where
d is the density of air in the tube, and
A is the cross-sectional area of the tube.
If it is shown that there is a demand for this volume air flow rate
through the tube immediately after the sudden opening of the intake
valve, a shock wave will be propagated down the intake tube
generating an acoustic pressure
p' = cqd/A
where
c is the velocity of propagation, which for a weak shock wave is
equal to the velocity of sound in air.
The ratio of acoustic pressure to steady state pressure is 2cA/q
and since q/A = v, where v is the steady state air velocity, then
p'/p = 2c/v. Thus, it will be seen at low steady state air
velocities, the steady state pressure is negligible compared to the
acoustic pressure. This acoustic pressure will persist until the
shock wave, traveling at the speed of sound, makes the round trip
from the intake valve to the open end of the wave tube and back
again.
The length and diameter of the intake wave tube determine the range
of engine operation over which sonic atomization, fuel metering
linearity and minimum steady state pressure loss may be achieved.
For example, if the maximum pressure loss at peak engine speed is
chosen not to exceed 5% and the maximum metering non-linearity is
chosen not to exceed 5%., the optimum diameter of the intake wave
tube is determined by
D = 2.58 .times. 10.sub.-.sup.3 x.sqroot. VNe (cm),
where
V is the displacement volume of the cylinder in cm.sup.3,
N is the maximum engine speed in rpm, and
e is the fractional volumetric efficiency at maximum engine
speed.
The length of the intake wave tube is determined by
L = 1.15 .times. 10.sup.5 /N (cm).
Increasing the diameter of the intake wave tube above this value
increases the minimum engine speed at which sufficient atomization
energy is avaiable, since p' is proportional to the square of the
ratio of engine speed to tube area, while decreasing the diameter
of the intake tube below this value increases the steady state
pressure loss at peak engine speed approximately inversely as the
4th power of the tube diameter. The length of the intake tube is
less critical. Decreasing the length of the tube raises the minimum
engine speed only inversely as the length, while increasing the
length of the wave tube introduces some metering non-linearity and
friction loss.
The location of the slide valve or sliding throttle plate 31
relative to its longitudial position with respect to the axis of
the wave tube is selected so that at part throttle openings, an
increase in air/fuel ratio occurs consistent with the nominal
requirements of the engine under part load conditions. This results
in better fuel economy and lower carbon monoxide and unburned
hydrocarbon emissions. This occurs because the effective length of
the intake tube, which directly determines the metering pressure
from a given fuel jet size, is reduced. Optimum placement of the
slide valve depends on the parameters of the engine on which the
carburetor is mounted and the desired operating conditions.
If desired, the physical spacing and the angular orientation of the
axis of the fuel jet with respect to the axis of the throttle plate
may be varied to tailor the part-throttle air/fuel ratio because
the steady state air flow, which carries atomized fuel droplets
into the combustion chamber, has a much smaller angle of
convergence approaching the throttle plate than the shock wave.
Therefore, the air/fuel ratio may be increased at low throttle
settings by "hiding" the fuel jet behind the throttle plate by
rotation of the jet axis in a plane parallel to the throttle plate
and/or increasing the distance between the jet axis and the
throttle plate. In this connection, it should be noted that the
increase in air/fuel ratio is more strongly controlled by a
function of rotation than the distance at very low throttle
settings.
It should be appreciated that full throttle or open throttle is
when the passage or bore 32 in the slide valve is in complete
registration with the bores or passages 28 and 33 and that this
throttle opening can be gradually decreased by releasing the cable
41 and permitting the spring 36 to move the slide valve or throttle
plate 31 to the right as viewed in FIG. 4 to progressively close
off the wave tube.
The flared outer end of the wave tube minimizes entrance
losses.
It should be noted that the fitting 51 is placed in the wall of the
wave tube 46 because the axial position of the orifice 53, for the
purposes of metering fuel into the wave passages, is relatively
immaterial. This is true because the shock wave, after it passes
through the slide valve or throttle plate, expands almost
immediately so that it will effectively atomize any fuel which it
draws into the wave tube.
In connection with the design of the carburetor and the fuel system
incorporated in the present invention, it has been found desirable
to terminate the returning or incoming shock wave so that no
further shock waves are produced. For this purpose a viscous
acoustical resistance has been provided in the form of a slot 101
(see FIGS. 2 and 4) formed in the base 23. The slot 101 extends the
width of the base 23 and is open to the atmosphere on both sides.
The slot has a width which is only slightly greater than the
interior diameter of the wave tube. The slot 101 serves as a
terminating slot and in effect absorbs the incoming shock wave so
that there are no further reflections from the shock tube. Thus,
each shock wave can only make one round trip through the wave tube.
Further reflections of the shock wave are eliminated to prevent
such reflections from causing perturbations in the metering
linearity over the operating range of the internal combustion
engine on which the carburetor is mounted. As can be seen, the slot
101 is positioned immediately adjacent to and opens into the bore
33.
It is possible under certain conditions of engine operations where
a very high air/fuel ratio, that is, a very lean mixture, is
desired, as under part throttle conditions, that supplemental means
be provided to increase the air/fuel ratio. Because of the form of
the throttle plate or slide valve, it is expedient to utilize the
movement of this throttle plate to admit supplemental acoustical
resistance which is effectively in parallel with the wave tube such
that the acoustical impedance looking into the tube becomes much
lower. This will lower the shock wave pressure, thus metering less
fuel for a given value of steady state airflow thrugh the wave tube
and thereby producing the desired increase in air/fuel ratio. For
this purpose a thin slot 102 is milled into the body 22 and is open
to the recess 29. A hole 103 is formed in the body 22 and is in
communication with the slot 102 and is open to the atmosphere. The
slot 102 and the hole 103 serve to provide a variable acoustical
impedance as the throttle valve is moved. Hole 103 serves merely to
expose slot 102 to the atmosphere. By placing this slot 102 close
to the longitudinal axis of the slide, a monotonically increasing
air/fuel ratio is obtained with a decrease in throttle opening. By
proper placement of slot 102, great latitude can be obtained in
mixture compensation. It should be appreciated, however, that the
depth of slot 102 should be relatively small to maintain the
desired ratio of acoustical resistance to inductive reactance of
slot 102. The acoustical resistance of the slot 102 varies as the
4th power of the depth of the slot 102 whereas the inductive
reactance varies directly as the depth of the slot. It is
preferable to maximize the ratio of the acoustical resistance
relative to the inductive reactance because it is the acoustical
resistance which is most effective in modifying the shock wave
pressure.
In operation of the carburetor 21 on an internal combustion engine,
the carburetor can be positioned in any desired position. Thus, for
example, the wave tube can be positioned so that it is a side draft
wave tube or a down draft wave tube. It is only important that the
fuel supply bowl and the orifice therein be positioned in such a
manner that the level of the fuel in the fuel bowl barely covers
the orifice.
Another embodiment of the fuel control system incorporating the
present invention is shown in FIGS. 11 and 12, utilizing a pump
control. For this purpose, a fuel supply bowl 111 similar to the
bowl 57 can be provided. It is provided with an inlet or fill tube
66 as well as a drain tube 71. The control tube 68 is omitted. The
fitting 51 and the drain tube 71 are positioned so that the
lower-most point of the drain tube is flush with the upper portion
of the orifice 53. In such a bowl, fuel is supplied by a pump to
the fill tube 66 continuously and the excess fuel which is not
utilized drains away through the drain tube 71. At all times the
fuel 89 is maintained at a level which just covers the orifice
53.
In FIG. 12, there is shown a fuel supply system utilizing a
plurality of fuel supply bowls 111 such as would be used in
connection with an eight-cylinder internal combustion engine. The
fuel 89 is supplied from the tank 113 through a pipe 114 to an
engine-driven pump 116. The pump 116 supplies fuel through a
throttle-actuated regulator 117 to a line 118 which is connected to
the fill tube 65 of each of the fuel supply bowls 111. A line 119
is connected to the drain tubes 71 and is connected into the space
121 overlying the fuel in the tank 113 so that it can be readily
drained into the tank by gravity flow. Thus, fuel will be
continuously supplied to each of the fuel supply bowls 111 so that
it can be supplied to the wave tube of the carburetor associated
therewith.
In FIGS. 13 and 14 there is shown how the present carburetor and
fuel supply system can be incorporated into an eight-cylinder
internal combustion engine having a 4-stroke cycle. Thus, as shown
in FIGS. 13 and 14, there has been provided an internal combustion
engine 131 of a conventional type. Such an engine includes a block
132 provided with cylinders 133 having reciprocating or moving
pistons 134 mounted therein. The combustion chamber 136 is provided
above the piston and is adapted to be placed in communication with
an intake passage 137 through an intake valve 138 operated by a cam
139. Similarly, the combustion chamber 136 is adapted to be placed
in communication with an exhaust passage 141 through an exhaust
valve 142 operated by a cam 143.
A carburetor 146 incorporating the present invention is provided
for each of the cylinders of the internal combustion engine. As can
be seen, the carburetors 146 are mounted upon the engine block. The
carburetors 146 are provided with wave tubes 148 of the type
hereinbefore described. In addition, the carburetors are also
provided with fuel supply bowls 149 similar to those hereinbefore
described. As can be seen from FIGS. 13 and 14, the wave tubes of
the carburetors are inclined upwardly at a suitable angle such that
the wave tubes 148 are coaxial with the intake passages 137. Means
is provided on the engine 131 for filtering the air entering the
carburetors 146 and consists of a box-like enclosure 151 which is
mounted on the engine and which is provided with a removable cover
152 to permit access to the carburetors 146. The housing or casing
151 is provided with louvered openings 153 through which air passes
into the housing 151 and thence through filters 154 mounted on the
sides of the container as shown in FIG. 13. In this way, all air
entering the carburetors 146 will be filtered.
As can be seen from FIG. 14, the four carburetors provided on each
side of the enginer are formed from a common body casting 161 which
extends substantially the entire length of the engine and a common
base casting 162 both of which are fastened together by the screws
147. The base casting is secured to the block 132 by screws 150
(FIG. 13). Similarly, a common throttle plate is therefore provided
with four holes or openings 167, one of which is associated with
each carburetor.
Means is provided for operating the throttle plate 166 and consists
of a linkage mechanism 169. The linkage mechanism consists of a
shaft 171 which is rotatively mounted in L-shaped arms 172 and
secured to the housing 151. A plate 173 is secured to the shaft 171
and has a linkage 174 connected thereto which extends downwardly
through a slot 176 in the housing 151. The linkage 174 is connected
to a conventional accelerator mechanism such as that utilized in an
automobile so that the shaft 171 can be rotated by operation of the
acceleration pedal. Two arms 176 are provided on opposite ends of
the shaft 171 and are connected. by ball and pivot assemblies 177
to threaded shafts 178 which are connected to ball and pivot
assemblies 179 secured to the throttle plates 166. Thus, it can be
seen that as the shaft 171 is rotated, the throttle plates 166 will
be moved simultaneously. Means is provided for returning the
throttle plates to positions in which the holes 167 are out of
registration with the wave tubes of the carburetor and consists of
springs 181 secured to posts 182 secured to the body castings 161
and posts 183 secured to the throttle plates 166.
The fuel supply system which is utilized in the embodiment of the
invention shown in FIGS. 13 and 14 is of the pump control type and
fuel is supplied under pressure from the pump through line 191 to a
regulator 192. The regulator 192 supplies its output to a pipe 193
which is connected by lateral extensions 194 through tubes 196 to
the filler tubes of the fuel supply bowls 149. The operation of the
regulator 192 is controlled through the accelerator linkage as is
shown in FIG. 14. The arm 173 is connected by a pivot and ball
assembly 201 to a threaded rod 202 which is connected by a pivot
and ball assembly 203 to an arm 204 mounted on the regulator.
The drain tubes of the fuel supply bowls 149 are connected to tubes
206 which are connected to two extensions 207 of a drain pipe 208.
As can be seen from FIG. 13, the drain pipe 203 is at the level
which is substantially below the level of the drain pipes from the
carburetors so that in the event the engine is tilted during
operation fuel from one carburetor will not flow into the
carburetor on the other side.
The operation of this embodiment of the invention is similar to
that hereinbefore describedd with the principal difference being
that there are a plurality of carburetors and cylinders provided
for the internal combustion engine. From the concentration shown it
can be seen that all of the carburetors will operate in unison with
the cylinders to supply the so-desired fuel/air mixture to the
cylinders. All of the advantages described in the preceding
embodiments are applicable to the present embodiment. The shock
wave is utilized for automization of the fuel. This fuel
atomization is accomplished in a very efficient manner without a
marked pressure drop which gives increased performance and
increased range of operation. The air/fuel ratio is carefully
controlled so that there is a reduction of unburned hydrocarbons
and carbon monoxide. Since the carburetor utilized is relatively
simple, manufacturing and maintenance costs are greatly reduced.
While obtaining the maximum degree of atomization and providing for
efficient use of fuel, there is excellent throttle response and a
60 : 1 range of efficient airflow rate handling capability.
Still another embodiment of the invention is shown in FIG. 15 which
shows the applicability of the invention to two-stroke cycle
engines. Thus, as shown in FIG. 15, there is provided a two cycle
engine 216 which is provided with a cylinder 217 which has a
reciprocating piston 218 therein. The engine block 219 is provided
with a transfer passage 221 which is controlled by the piston 218.
The block is also provided with an exhaust passage 222 also
controlled by the piston. The piston drives the crankshaft 223
which is rotatably mounted on the block. The crankshaft 223 drives
a rotary valve 224 which is provided with a bore or passage 226
which is adapted to be moved into registration with an intake port
227 provided in the block. This bore 227 is in registration with
the wave tube of a carburetor 231 incorporating the present
invention. As shown in FIG. 15, the carburetor 231 is mounted in a
side draft fashion and utilizes an air control tube 232 for
controlling the flow of fuel into the fuel bowl. The carburetor 231
operates in the manner hereinbefore described as with the other
embodiments of the invention. A shock wave is formed within the two
cycle engine similar to the four cycle engine and is propagated
down the wave tube to atomize the fuel as hereinbefore described. A
throttle plate 234 is provided for controlling the fuel supplied to
the engine to thereby regulate the speed of operation of the
engine.
It is apparent from the foregoing that there has been provided a
fuel supply system and carburetor incorporated in the same which
utilizes a unique method for atomizing fuel and introducing the
same into the combustion chamber of internal combustion engines. An
airflow without significant pressure drops is provided for movng
the atomized fuel into the combustion chamber. The emission of
unburned hydrocarbons and carbon monoxide is substantially reduced.
Very accurate control of air/fuel ratio can be obtained.
* * * * *