[0001] This invention relates to a fluid mixing device and in fuel metering particular,
though not exclusively, to a carburetor having a / system for supplying a homogeneous
mixture of fuel and air across the throttle opening of the carburetor while precisely
controlling fuel and air flow rates.
[0002] For so long as internal combustion engines have been in existence, various carburetors
have been developed to supply a required air-fuel mixture to the engine to promote
proper and efficient combustion. Although myriads of carburetion schemes and devices
have deen developed, a continuing problem has been metering of the air-fuel mixture
in a consistently homogeneous blend such that the air-fuel mixture received by each
cylinder of the internal combustion engine is the same as that supplied to each other
cylinder.
[0003] In addition, not only is it important to control the homogeneity of the fuel-air
mixture, it is also important to control the actual quantity of the fuel injected
into the air stream in relation to the density of the air passing through the carburetor.
Thus, when the air density decreases, it is important to also reduce the fuel flow
rate so that the air-fuel blend supplied to the internal combustion engine is not
fuel rich. This is particularly important in aircraft, where at high altitudes, the
air density is considerably reduced. A commensurate reduction in the flow rate of
the fuel must be made in order to properly lean the mixture to avoid fuel waste or
possible engine flooding.
[0004] In conventional carburetors or fuel injection systems, the velocity of the air passing
through a venturi portion is assumed to correspond directly to the air mass flow.
This assumption remains correct so long as there is no change in air density. If the
ambient air temperature or pressure does change, then the resultant change in density
invalidates this assumption and the carburetor or injection system experiences a change
in air-fuel ratio. If the air density increases, then the air-fuel ratio becomes leaner
and if the air density decreases, then the air-fuel ratio becomes richer. In most
carburetor applications except aircraft the recent low cost of fuel has made mixture
control not cost effective. In aircraft, where density-related mixture changes due
to altitude result in large power- reductions, mixture control has always been a necessary
feature.
[0005] The venturi system of measuring air flow and metering fuel is based upon the Bernoulli
principle as expressed by the Bernoulli equation as follows:

Where P = Pressure, V = airflow velocity, e = air density
[0006] As the Bernoulli equation applies to air flow in a venturi, it can be rewritten as
follows:

or,

with the subscripts 1 and 2 referring to different axial locations in the flow tube.
If the velocity at location 2 is high (such as occurs at the throat of a venturi)
the pressure is lower than the pressure at a location where the velocity is low. From
the Bernoulli equation, it is seen that the amount of pressure difference is much
greater than the velocity difference because the velocities in the equation are squared.
[0007] The pressure that is sensed in a direction perpendicular to the direction of local
flow in a venturi is the static pressure and is equal to that which would be sensed
by a pressure instrument moving with the air flow. The pressure that is sensed by
a probe inserted in the flow path and oriented with its opening facing the oncoming
air is defined as the total pressure. The difference between the total pressure and
the static pressure is the dynamic pressure and is related to the flow velocity by
Bernoulli's equation as follows:

[0008] In the absence of friction, the total pressure remains constant along the length
of a flow tube or venturi. In an area where the flow velocity increases due to a constriction
in flow area, the static pressure is commensurately low.
[0009] Slide-type carburetors consisting of an air passage and a throttle plate movable
to provide an adjustable throttle opening to alterably constrict the air passageway
have been in existence for some time, as evidenced by U.S. Patents No. 3,709,469 and
3,957,930. Such devices provide for throttling of the air flow in combination with
mechanical control of the fuel quantities added to the carburetor. However, because
fuel is injected into one side of -the throttle opening in either of these devices,
they suffer from an inability to supply a homogeneous air-fuel mixture across the
throttle opening and do not permit a full range of air-fuel mixture control.
[0010] Other devices are known for metering fuel flow across the throat of a carburetor,
as evidenced by U.S. Patents No. 1,142,763 and 4,205,024. While such devices do permit
fuel distribution effectively across the carburetor, it is difficult with such devices
to adjust the air-fuel mixture as the carburetor air passageway is throttled.
[0011] The present invention seeks to provide a fluid mixing device, preferably in the form
of a carburetor, which overcomes the above-delineated short comings of the prior art,and
others.
[0012] Accordingly the invention provides fluid mixing device comprising: a fluid passageway
for a first fluid, an adjustable throttle valve which has a throttle aperture which
is so arranged in relation to the passageway so as to form in the passageway a throttle
opening of controllable cross-sectional dimension, and a fluid metering system means
for supplying a second fluid to the passageway through a distribution outlet which
extends across the passageway and the effective length of which is determined by the
cross-sectional dimension of the throttle opening, and means for altering the proportionate
flow of the second fluid through the distribution outlet in relation to the flow of
the first fluid in the passageway.
[0013] Preferably the fuel metering system means incorporates a fuel metering tube which
extends across the throttle.opening. The distribution outlet is preferably located
in metering tube for metering of fuel across the entire width of the throttle opening,
not matter what size throttle opening is presented.
[0014] In one embodiment of the invention, the fuel metering system includes means to alter
the flow of fuel through the distribution outlet by changing the orientation of the
fuel metering tube from a maximum lean position, where fuel flow may be essentially
eliminated, to a full fuel flow position, thereby providing the richest possible air-fuel
mixture.
[0015] In this embodiment, in order to alter the flow of fuel through the fuel distribution
outlet, the fuel metering tube preferably is rotatable about its longitudinal axis
to change the circumferential location of the distribution outlet. The outlet is positionable
between a maximum lean condition facing upstream in the direction of air passage,
and a maximum rich condition 90 degrees therefrom in which the distribution outlet
faces across the path of air flow.
[0016] In another embodiment of the invention, the fuel supply comprises a fixed metering
tube having its distribution outlet extending along one side and oriented perpendicular
to air flow through the throat of the carburetor. In order to control the fuel flow,
a pressure detecting tube is located in communication with the air passageway to sense
a portion of the dynamic pressure of the air as it passes through the carburetor.
This detected pressure is then used to maintain the pressure of the fuel at the detected
pressure as the fuel is introduced into the fixed metering tube.
[0017] In this second embodiment of the invention, the detecting tube has an inlet in one
side and is very similar to the fuel metering tube of the first embodiment of the
invention. The detecting tube is rotatable to change the circumfernetial location
of the inlet and therefore change the amount of the dynamic air pressure that is sensed
Therefore, because of the rotatable nature of the detecting tube, the tube can be
made to sense any pressure between the total pressure and the static pressure of the
air flow.
[0018] In order to control the fuel flow in this embodiment of the invention, the invention
includes a balancing regulator which is regulated by the sensed pressure. The balancing
regulator has an inlet on one side for the fuel, and includes a control responsive
to the sensed pressure and operable to permit the flow of fuel through the fuel inlet
at such a rate so as to maintain equality between fuel pressure and the sensed pressure.
[0019] In another embodiment of the invention, the fuel metering tube is also fixed with
the distribution outlet extending perpendicular to the air flow. A pressure transmitting
tube having one end extending into the air flow is oriented to detect the total pressure
of the air. A second pressure transmitting tube has one end extending into the air
at the throttle passageway in order to detect the static pressure of the air passing
therethrough. The tubes are joined at their other ends and a third pressure transmitting
tube leads from this junction to a balancing regulator to control pressure of the
fuel. The second pressure transmitting tube has a valve operable to permit a portion
of the total pressure in the first pressure transmitting tube to bleed into the second
pressure transmitting tube,-'leaving a resultant differential pressure in the third
pressure transmitting tube. The resultant differential pressure is used to control
the pressure of the fuel as it is introduced into the fuel outlet.
[0020] In this embodiment of the invention, a balancing regulator is again used to control
the fuel flow. The balancing regulator senses the differential pressure and has an
inlet for the fuel. The regulator includes a fuel control responsive to the sensed
differential pressure and operable to permit flow of fuel through the fuel inlet at
such a rate so as to maintain equality of pressure between the fuel and the sensed
differential pressure.
[0021] In both latter embodiments of the invention, the fuel is delivered to the inlet of
the balancing regulator from some external source such as a fuel pump or elevated
fuel reservoir. The balancing regulator therefore is used to reduce the pressure of
the fuel to the required pressure before fuel is permitted to enter the fuel metering
tube.
[0022] In accordance with the invention, the fuel metering system comprises a normally axially
stationary fuel metering tube extending across the throttle opening. In one form,
the distribution outlet in the fuel metering tube comprises a plurality of apertures
spaced axially along one side of the metering tube. In another form, the distribution
outlet comprises an axial slot along one side of the metering tube. In all cases,
the metering tube preferrably is positioned in registration with the throttle valve
and extends through a complimentary lateral aperture in the throttle valve. The throttle
valve is slidable upon the metering tube to adjust the throttle opening and change
the effective length of thefuel distribution outlet; Therefore, no matter how large
the throttle opening, a uniform distribution of fuel is maintained across the throttle
opening.
[0023] The throttle valve is adjustable between limits to provide a maximum throttle opening
and a minimum throttle opening. In order to precisely control the fuel-air mixture
at the minimum throttle opening, the axial location of the fuel metering tube can
be adjusted. Thus, a greater or lesser portion of the distribution outlet can be presented
across the throttle opening at its minimum setting.
[0024] Often, in situations of increased acceleration, it is necessary to momentarily enrich
the fuel-air mixture. To do so, the invention includes a fuel reservoir in communication
with the air passageway. As the throttle opening is enlarged to increase the cross-sectional
dimension of the air passageway, the invention includes means to inject supplemental
fuel into the air passageway. Such injection occurs only when the throttle opening
is increased in dimension, and only when the rate of increase of the throttle opening
is such that an enriched fuel mixture is required.
BRIEF DESCRIPTION OF THE DRAWINGS
[0025] The above features of the invention, and others, are described in greater detail
in the following description of a number of preferred embodiments, where reference
is made to the accompanying drawings, in which:
Figure 1 is an exploded illustration of the invention, with some parts omitted and
other parts in cross-section to permit illustration of the primary components of the
invention.
Figure 2 is a cross-sectional illustration of the assembled invention, illustrating
the throttle valve closed to a minimal throttle opening.
Figure 3 is an illustration similar to Figure 2, but with the throttle valve translated
sufficiently to provide a partial throttle opening.
Figure 4 is a view similar to Figure 2 but with the throttle valve being withdrawn
sufficiently to provide a full throttle opening.
Figure 5 is an enlarged cross-sectional illustration taken along lines 5-5 of Figure
4.
Figure 6 is an enlarged cross-sectional illustration taken along lines 6-6 of Figure
2.
Figure 7 is an enlarged cross-sectional illustration taken along lines 7-7 of Figure
4.
Figure 8 is an enlarged, partially truncated view of one embodiment of the fuel metering
tube according to the invention.
Figure 9 is an elongated cross-sectional illustration taken along lines 9-9 of Figure
8'.
Figure 10 is a truncated top plan view of an alternative embodiment of the fuel metering
tube according to the invention.
Figures 11 through 13 illustrate rotation of the fuel metering tube respectively between
a lean mixture setting, and a rich mixture setting.
Figures 14 illustrates, in cross section, a modified embodiment of the invention.
Figure 15 illustrates a modification of the embodiment of Figure 14, showing another
form of the fuel metering system.
Figure 15a through 15c illustrate a partial cross-section taken along lines 15a -
15a of Figure 15, with Figures 15b and 15c showing rotation of the pressure detecting
tube.
Figure 16 illustrates a further modification of the embodiment of Figure 14, showing
yet another form of the fuel metering system.
Figure 17 illustrates a further modification of the embodiment of Figure 14, showing
a final form of the fuel metering system.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0026] A fluid mixing device according to the invention, in the form of a carburetor, is
shown in assembly fashion in Figure 1. Primary components of the carburetor include
a top plate 10, a bottom plate 12, and a throttle valve 14. Although the top plate
10 and bottom plate 12 are delineated as such, it should be obvious that the designations
"top" and "bottom" are for the purposes of explanation only, and the respective roles
of the plates 10 and 12 can be reversed as necessary. In addition, the top plate 10
has been shown in cross-section for the purposes of description, and would include
a second half complimentary to that shown in Figure
1.
[0027] The top plate 10 includes an air inlet 16. The bottom plate 12 includes an air-fuel
outlet 18 located in concentric registration with the air inlet 16. The inlet 16 and
outlet 18 are preferably of equal diameter.
[0028] When the carburetor is assembled, the throttle valve 14 is sandwiched between the
top plate 10 and the bottom plate 12 for sliding movement between the two plates.
The plates 10 and 12 are suitably fixed together as by means of a plurality of screws
20 passing through apertures 22 in the bottom plate 12 and engaging corresponding
threaded apertures 24 in the top plate 10.
[0029] Although, as indicated above, the throttle valve 14 is situated between the plates
10 and 12 for sliding movement; the throttle valve 14 is dimensioned for a close fit
in the aperture formed between the plates 10 and 12 when assembled. The throttle valve
14 may be formed of a material susceptible to forming a seal, such as Teflon,' while
the plates 10 and 12 may be formed of aluminum, steel or other relatively stiff material.
Other materials may be used as desired.
[0030] As best shown in Figure 1, the throttle valve 14 includes a throttleaperture 26.
The cross sectional dimension of the aperture26 is the same as the diameters of the
inlet 16 and outlet 18 so that if the inlet 16, opening 26 and outlet 18 are aligned,
an uninhibited throttle opening or bore is formed through the carburetor. At this
position, as described in greater detail below, air flow is maximum and, as is well
known, the carburetor is at its full throttle position.
[0031] As best shown in Figures 2 through 4, the position of the throttle valve 14 between
the sandwiched plates 10 and 12 is determined by means of a control rod 28. The rod
28 is secured within a bore 30 formed in the throttle valve 14 and passes through
an aligned aperture 32 formed in the sidewall of the top plate 10. A pin or set screw
34, passing through a hole 36 in the rod 28 and lodged within a hole 38 formed in
the throttle valve 14, secures the control rod 28 within the throttle valve 14.
[0032] For fuel metering, the carburetor includes a fuel metering tube 40 which passes longitudinally
through the entire throttle valve 14 and extends through apertures 42 and 44 at opposite
ends of the top plate 10. The throttle valve 14 includes a close-fitting longitudinal
aperture 46 through which the fuel metering tube 40 passes and upon which the throttle
valve 14 is mounted for sliding between the extreme locations shown in Figures 2 through
4. The longer bore of the longitudinal aperture 46 may include sealing rings or the
like (not illustrated) to assure a fluid-tight seal between the fuel metering tube
40 and the aperture 46.
[0033] The aperture 44 is threaded, as illustrated. A fuel connection nipple 48 is engaged
on the threads of the aperture 44 and is shaped for connection to an external fuel
source (not illustrated) in a well known manner not further described herein. The
fuel connection nipple 48 may include a sealing ring or some similar device to provide
a fluid tight seal between the nipple 48 and the fuel metering tube 40.
[0034] The fuel metering tube 40 is rotatable about its longitudinal axis to control the
fuel-air ratio. Rotation is controlled by means of an arm 50 attached to the end of
the fuel metering tube 40 opposite to that of the connection nipple 48. The arm 50
sealingly closes the tube 40 at its point of connection, and is controlled for rotation
by suitable means (not illustrated), such as a control cable which may be clamped
to the arm 50 through a bore 52 by a bolt 54.
[0035] Immediately adjacent the arm 50, a collar 56 is permanently secured to the fuel metering
tube 40. A keeper screw 58, threadedly secured within the top plate 10, engages a
circumferential channel 60 formed in the collar 56. Thus, the keeper screw 58 maintains
precise axial alignment of the fuel metering tube 40. By suitable adjustment of the
keeper screw 58, the axial position of the fuel metering tube 40 may be altered for
purposes described in greater detail below.
[0036] As best shown in Figures 1 and 4, the fuel. metering tube 40 includes a distribution
outlet 62 extending across the entire width of the throttle aperture 26 when the throttle
valve 14 is in the full throttle position. Thus, with the axial alignment of the fuel
metering tube 40 being fixed by the keeper screw 58, no matter what the position of
the throttle valve 14 between the top and bottom plates 10 and 12, fuel is dispensed
across the entire width of the effective throttle opening.
[0037] As shown in enlarged fashion in Figures 8 and 9, in this first embodiment, the distribution
outlet 62 is composed of a plurality of holes 64 spaced axially along one side of
the fuel metering tube 40. The holes 64 may be evenly spaced. However, if the internal
diameter of the fuel metering tube 40 is quite small, and if the fuel pressure is
low, the internal flow resistence created within the fuel metering tube 40 is sufficient
to reduce the flow to a large enough extent so that the fuel flow rate through the
rightmost holes 64 (Figure 8) is significantly more than that flowing through the
left-most holes. In order to avoid this result, the holes 64 may be grouped and those
in an area of less fuel pressure (and consequently, less fuel flow rate) can be grouped
closer together so that the fuel flow rate along the entire distribution outlet 62
remains essentially constant. As shown in Figure 8, the holes 64 have been gathered
in three groups 66, 68 and 70 in order to overcome the reduction of the fuel flow
rate over the length of the distribution outlet 62. Of course, as indicated above,
should the reduction of the fuel flow rate along the length of the distribution outlet
62 be minimal, the spacing of the holes 64 need only be constant or may be spaced
such that each hole is positioned at the center of equal air flow areas when the throttle
valve is in its open position.
[0038] Figure 10 illustrates an alternative embodiment of the distribution outlet, designated
as 62'. In this embodiment, the holes 64 are eliminated and instead the distribution
outlet 62' comprises an axial slot opening along one side of the metering tube 40.
In the same manner as grouping of the holes 64 in the distribution outlet 62, if there
is a fuel flow reduction within the fuel metering tube 40 from one end of the distribution
outlet 62' to the other, the slot of the distribution outlet 62' may be formed in
an increasing taper fashion, as illustrated, in order to maintain constant fuel outlet
flow through the distribution outlet 62'. Again, if there is a negligible fuel flow
reduction, tapering of the distribution outlet 62' is unnecessary and the outlet may
be formed as a longitudinal slot of constant dimension.
[0039] The fuel distribution outlet 62 may take other forms, depending on the fuel distribution
characteristics desired. A series of two or more circumferentially spaced outlets
can be used, and holes or slots for fuel distribution can be used in combination,
or can be replaced by equivalent outlet means. As an alternative, the distribution
outlet 62 may follow other than a straight pattern in order to alter fuel metering
capabilities along its length.
[0040] As is well known, depending on the position of the throttle valve 14 and therefore
the cross sectional dimension of the throttle opening through the carburetor, air
flow through the carburetor is controlled. With the throttle valve 14 in the position
illustrated in Figures 4, 5 and 7, maximum-air flow is permitted and therefore the
carburetor is at full throttle. With the throttle valve 14 at the position indicated
in Figures 2 and 6, the carburetor is at its throttle closed position. The location
shown in Figure 3 is a mid-throttle position. As shown in Figure 2, the maximum closure
of the throttle valve 14 is determined by a set screw 72. With the set screw 72 adjusted
to the position shown in Figure 2, a minimum air passageway 74 is formed. As shown
in the drawings, the dimension of minimum air passageway 74 can be increased or decreased
as desired by adjustment of the set screw 72. In fact, if desired, the minimum air
passageway 74 can be omitted completely, although such a situation is not normally
acceptable.
[0041] Also as shown in Figure 2, only a very small portion of the distribution outlet 62
extends into the minimum air passageway 74. If desired, a greater portion of the distribution
outlet can extend into the minimum air passageway 74 by adjustment of the keeper screw
58. Assuming that, in the position shown in Figure 2, a single hole 64 (Figure 8)
of the distribution outlet 62 extends into the minimum air passageway 74, by suitable
adjustment of the keeper screw 58, a greater portion of the distribution outlet 62
can appear in the minimum air passageway 74, allowing one or more additional holes
64 to inject fuel into the minimum air passageway. Thus, by adjustment of the set
screw 72 and the keeper screw 58, the dimensions of the minimum air passageway 74
are dictated, and also the fuel metering capacity at this minimum setting is determined.
[0042] In many carburetors, such as an aircraft carburetor of the nature of the invention,
fuel pressure entering the carburetor fuel metering section is esentially equal to
ambient pressure. Therefore, fuel is aspirated from the distribution outlet 62 of
the fuel metering tube 40 by pressure differences created within the effective air
passageway. In many situations, and in particular in an aircraft, the carburetor must
have the capability of reducing the fuel flow as increases in aircraft altitude reduce
the density of the air entering the air inlet 16 of the carburetor. Changes in the
air-fuel mixture are effected by rotation of the fuel metering tube 40, as best shown
diagrammatically in Figures 11 through 13. With the fuel metering tube 40 in the position
shown in Figure 11, the distribution outlet is aimed upstream directly toward the
air inlet 16, and the carburetor is in the "idle cutoff" position. When the fuel pressure
in the metering tube is regulated in such a way so as to be maintained approximately
equal to the total pressure of the air, the dynamic air- pressure within the air inlet
16 completely inhibits the flow of fuel, causing the engine to stop.
[0043] In the position shown in Figure 13, the distribution outlet 62 is turned at 90 degrees
to the airflow. This is the position for providing the richest possible air-fuel mixture
such as is normally required at low altitudes. In this position, the fuel flow from
the distribution outlet is being aspirated into the air passageway by the difference
in pressure between the fuel inside the fuel metering tube 40 and the static air pressure
outside of the distribution outlet 62 which is reduced below ambient pressure in accordance
with the Bernoulli equation.
[0044] To adjust the carburetor to a leaner air-fuel mixture as would be required at higher
altitudes, the fuel metering tube 40 is rotated to a mid-way orientation such as that
shown in Figure 12. In this position, the air pressure outside of the fuel distribution
outlet 62 is increased by a dynamic component of the velocity of the air entering
the air inlet 16. This reduces the differential between the static and dynamic pressures
which aspirates the fuel from the distribution outlet 62, and therefore reduces the
fuel flow rate from that of the orientation shown in Figure 13. Consequently, a leaner
fuel mixture is attained without fuel flow cutoff as shown in Figure 11.
[0045] Therefore, the invention achieves an even fuel distribution with precise air-fuel
mixing to enable the carburetor to control an engine no matter what ambient conditions
may be encountered. Not only does the throttle valve 14 control the air flow through
the carburetor, but also the throttle valve 14, when sliding along the fuel metering
tube 40 across the distribution outlet 62, maintains the air-fuel mixture constant
no matter what the throttle position, contrary to conventional carburetors. In addition,
by rotation of the fuel metering tube 40, the richness of the air-fuel mixture can
be precisely controlled to account for changes in ambient air density.
[0046] In some internal combustion engines it is necessary to inject additional fuel into
the throttle aperture 26 during periods of engine acceleration. Because fuel is available
directly at the outlet 62, acceleration enrichment is not normally required with the
present invention. If desired, however, the throttle valve 14 may include bores 76
and 78. Normally, as shown in Figure 2, a reservoir 80 formed between the plates 10
and 12 is flooded with fuel. If the throttle valve 14 is opened rapidly during a period
of high acceleration, some of the fuel in the reservoir 80 will pass through: the
bore 78 and be emitted directly into the throttle aperture 26. The remainder thereof
will pass through the larger bore 76 into a second reservoir 82 on the opposite side
of the throttle valve 14. The more rapidly the throttle valve is opened (right to
left in Figures 2 through 4), the greater the quantity of fuel which is forced through
the bore 78 into the throttle aperture 26. On the other hand, if the throttle valve
14 is withdrawn at a slow rate, very little, if any, fuel passes through the bore
78, the majority thereof passing through the bore 76 into the newly-formed reservoir
82. Thus, during periods of high acceleration, an additional quantity of fuel is injected
into the throttle aperture26.
[0047] An alternate method is available to provide acceleration enrichment if the fuel metering
tube 40 is provided with a fuel bleed orifice 84 in substitution for the bore 78.
In this configuration, a sudden throttle movement leftward causes the throttle plate
14 to force the fuel contained in the reservoir 80 through the bleed orifice 84 into
the metering tube 40 and out of the distribution outlet 62 into the .throttle aperture26.
[0048] It should be apparent that other forms of acceleration enrichment can be included
as well. In addition, rather than forming a bore 76 as illustrated in the drawings,
one or both of the sides of the throttle valve 14 abutting the top plate 10 can include
a groove extending from the reservoir 80 to the reservoir 82. Additionally, if the
carburetor is constructed such that fuel is absent from the reservoirs 80 and 82,
other means of injecting additional fuel in response to the speed of translation'
of the throttle valve 14 can be employed as well.
[0049] Figure 14 illustrates an alternative embodiment of the invention having modification
of the throttle valve' and fuel system leading to the fuel inlet tube 40. Other components
of the invention remain the same and therefore bear the same reference numerals. Since
these elements were described above, further description is omitted.
[0050] As illustrated, the throttle valve 14' in Figure 14 is truncated, omitting a portion
of the throttle valve 14 which is unnecessary. As shown, the throttle valve 14' includes
a throttle aperture26' having a diameter equal to that of the air-fuel mixture outlet
18 so that, in a full throttle open position (such as that illustrated in Figure 4),
there is no obstruction to flow by the throttle valve 14'.
[0051] In this embodiment, the invention includes a balancing regulator 90 operable to control
fuel pressure in the fuel inlet tube 40 to ambient pressure. The balancing regulator
90 has an inlet 92 for fuel under pressure. The inlet 92 leads to a nipple 94 which
may be connected to a source of fuel (not illustrated).
[0052] The inlet 92 is terminated by a fluid control ball valve 96 or by a conventional
needle valve and seat assembly (not illustrated). The valve 96 has an internal orifice
98 which may be closed by a pair of balls 100. An arm 102, pivotally connected in
its mid-section at 104 to the balancing regulator 90, has one end which bears against
the larger of the balls 100. The other end of the arm 102 bears against a biasing
compression spring 106 which in turn bears against a screw 108 threaded into the body
of the top plate 10. Depending on the compression strength of the spring 106, the
spring normally pivots the arm about the pivot 104, urging the balls 100 into the
orifice 98 to preclude fuel flow through the inlet 92 into the interior of the balancing
regulator 90 and from there into the fuel inlet tube 40. Fine adjustment of the compression
strength of the sprint 106 with the screw 108 to achieve this end is well-known.
[0053] The balancing regulator 90 also includes a movable diaphragm 110 having a central
contact 112 in alignment with one end of'the arm 102. The balancing regulator 90 also
includes an opening 114 to the ambient surroundings.
[0054] The metering system of the balancing
'regulator 90 operates in a well-known manner. Since the opening 114 is to the ambient
pressure which is usually equal to the airflow total pressure, the ambient pressure
normally urges the contact 112 against the arm 102, permitting fuel to enter the regulator
90 through the inlet 92. Not only does the entering fuel flow through the fuel inlet
tube 40 and exit through the distribution outlet 62, the fuel also bears against the
opposite side of the diaphragm 110 from that open to the ambient pressure experienced
through the opening 114. If the fuel pressure is higher than the ambient pressure,
the increased pressure of the fuel tends to urge the contact 112 away from the arm
102, permitting the spring 106 to pivot the arm about the pivot 104, urging the balls
100 into the closed position. Therefore, the diaphragm 110 always positions itself
as necessary to equalize the fuel pressure on the fuel side of the diaphragm with
the ambient air pressure on the air side of the diaphragm. Thus, the fuel pressure
in the inlet tube 40 is always maintained at approximately the same pressure as the
ambient air pressure surrounding the carburetor.
[0055] Figure 15 illustrates a modified version of the invention in which fuel flow is controlled
totally by air pressure and the fuel inlet tube 40 is fixed with the inlet 62 oriented
so as to sense static pressure, in this embodiment perpendicular to the direction
of air flow through the carburetor.
[0056] As seen in Figure 15, the opening 114 of the balancing regulator 90 is not opened
to ambient pressure. Rather, a conduit 116 leads from the opening 114 to a pressure
detecting tube 118 extending across the air inlet 16. The tube l18 must be immediately
adjacent the fuel distribution outlet 62, and is shown directly above the tube 40
in Figure 15. The detecting tube 118 includes an aperture 120 therein, thus permitting
the tube 118 to sense the air pressure in the air inlet 16. The tube 118 is axially
rotatable as shown in Figure 15 and in Figures 15a - 15c in order to permit altering
the circumferential location of the aperture and therefore vary the percentage of
the dynamic pressure that is sensed. ยท
[0057] Since the distribution outlet 62 of the fuel inlet tube 40 is fixed at an orientation
perpendicular to the air flow through the carburetor, the distribution outlet 62 experiences
only the static component of the total air pressure in the carburetor at its particular
location. So long as the fuel introduced into the inlet tube 40 is at a pressure greater
than the static pressure existing at the distribution outlet 62, fuel will flow from
the distribution outlet and be mixed with the incoming ambient air.
[0058] The pressure balancing function of the balancing regulator 90 causes the pressure
in the metering tube 40 to be equal to the pressure sensed by the pressure detecting
tube 118. With the orientation of the aperature 120 shown in Figure 15 and Figure
15a (open to the air flow), the aperture 120 detects the total pressure of the air
at this location. The balancing regulator adjusts the fuel pressure in the metering
tube 40 to equal the total pressure sensed by the aperture 120. Since the pressure
at the fuel outlet 62 is equal to the static pressure, fuel flow occurs through the
fuel outlet 62.
[0059] If, on the otherhand, the aperture 120 is oriented as shown in Figure 15b, the aperture
120 senses a lower pressure that'is equal to the static pressure plus a lesser dynamic
component that depends on the upstream orientation of the aperture 120. This lower
pressure is transmitted through the conduit 116 to the diaphram 110. The diaphram
110 positions itself such that the ball valve 96 admits fuel to the fuel side of the
diaphragm 110 at such a rate so as to make the fuel pressure in the metering tube
40 equal to the air pressure sensed by the aperture 120 in the pressure detecting
tube 118.
[0060] When the pressure sensing aperture is oriented as shown in Figure 15c, the resulting
pressure in the fuel metering tube 40 is equal to the static pressure existing at
the outlet 62. With the orientation shown in Figure 15c, no fuel would flow.
[0061] Figure 16 illustrates a modification of the system for injecting fuel into the carburetor.
A portion of the air inlet 16 of the top plate 10 is shown superimposed above the
cross-sectional illustration of the carburetor as depicted and described in Figure
14. In this embodiment, a first pressure transmitting tube 122 leads from the air
inlet 16 and joins a second pressure transmitting 124 leading from the mixture outlet
18. A third pressure transmitting tube 126 leads from the juncture of the tubes 122
and 124 to the opening 114 of the balancing regulator 90. As shown, the end 128,of
the tube 122 in the air inlet 16 faces upstream and therefore senses the total air
pressure in the air inlet 16. The tube 124 is introduced at the side of the mixture
outlet 18, and therefore detects the static pressure at that location. An adjustable
needle valve 130 is located in the tube 124 and may be adjusted to close the tube
124 completely, or permit any opening required.
[0062] Because the end 128 of the tube 122 is opened to the total pressure, and because
the tube 124 is opened to the lower static pressure, if the needle valve 130 is opened
slightly, a portion of the total pressure in the tube 122 is bled through the needle
valve 130 into the tube 124. This leaves a resultant differential pressure in the
tube 126, which is directed through the opening 114 to the interior of the balancing
regulator 90. Thus, by judicious adjustment of the needle valve 130, the differential
pressure experienced by the balancing regulator 90 may be adjusted as desired. Since
the distribution outlet 62 of the fuel inlet tube 40 is oriented perpendicular to
the flow direction, and therefore experiences only the static pressure of the flow,
the balancing regulator 90 is operated as described above and fuel is driven through
the outlet 62 by the difference between the differential pressure within . the tube
126 and the static pressure at the distribution outlet 62. So long as the differential
pressure is greater than the static pressure, fuel will flow.
[0063] Figure 17 illustrates another embodiment of the invention having modification of
the throttle valve and fuel system leading to the fuel inlet tube 40. Components which
have been described above bear the same reference numerals and perform the same functions.
Further description, therefore, is omitted. ,
[0064] In this embodiment, the invention includes' a fuel metering float regulator 140 operable
to maintain fuel pressure in the fuel inlet tube 40 at ambient pressure. float regulator
140 includes the fluid control ball valve 96 and associated component described above.
The arm 102 of the prior embodiments of Figures 14 through 16 is replaced with an
arm 142 which is pivotally connected in its mid-section at 144. One end of the arm
142 bears against the larger of the balls 100. The other end of the arm 142 is connected
to a float 146 maintained within a fuel reservoir 148 of the float regulator 140.
The float 146 is situated such that during normal operation, the level of the fuel
150 within the fuel reservoir 148 is sufficient to allow fuel to enter the fuel inlet
tube 40. If the pressure of the fuel 150 within the reservoir 148 is greater than
the air pressure experienced at the distribution outlet 62 of the inlet tube 40, fuel
will flow from the distribution outlet. Conversely, if the air pressure is the same
as or higher than the fuel pressure, no fuel will flow from the distribution outlet
62.
[0065] As shown diagrammatically, the fuel reservoir 148 includes an aperture 152 open to
the ambient surroundings. Therefore, the fuel 150 within the reservoir 148 is maintained
at ambient pressure.
[0066] The metering system of the float regulator 140 operates in a known manner. Since
the aperture 152 is opened to ambient pressure, and assuming fuel pressure in the
inlet 92 is greater than ambient pressure, fuel enters the reservoir 148 from the
inlet 92 and maintains a level permitted by the float 146. The fuel 150, at ambient
pressure, also enters the fuel inlet tube 40, and is present at the distribution outlet
62. With the distribution outlet aimed upstream in the orientation illustrated in
Figure 17, the total pressure is experienced. Since the total pressure equals the
ambient pressure, at the orientation illustrated, fuel flow through the outlet 62
will be prevented. However, if the fuel inlet tube 40 is rotated slightly, the pressure
experienced at the distribution outlet will be less than the total pressure. Thus,
fuel will flow from the distribution outlet 62. The fuel/air mixture is therefore
controlled by the rotational orientation of the fuel inlet tube 40, in the same manner
as described above with regard to prior embodiments.
[0067] In this embodiment of the invention, fuel will enter the reservoir 148 from the inlet
92 so long as the fuel in the inlet 92 is under pressure. Therefore, when an internal
combustion engine incorporating the invention is stopped, operation of the pump (not
illustrated) supplying fuel to the inlet 92 must also be stopped. The fuel 150 contained
within the reservoir 148 will, therefore, at maximum drain to a lower level where
no fuel enters the inlet tube 40.
[0068] The invention provides a novel, precise system for metering fluid flow and mixing
of two fluids. By appropriate orientation of the fuel outlet 62 of the fuel inlet
tube 40 in combination with regulated fuel pressure and appropriate adjustment of
the throttle valve 14, optimum fuel/air ratio can be provided over the full range
of engine power and operating environment.
[0069] Because no obstructions exist downstream of the fuel outlet, the carburetor according
to the invention is non-icing. This feature is quite advantageous particularly in
aircraft which operate at altitudes or temperatures where icing can occur in conventional
carburetors.
[0070] Conventional carburetors which are used in automotive applications require a choke
valve of some nature to provide extra richness for engine starting. No choke valve
is required in the present invention since the required richness for ,starting can
be obtained by the combination of the fuel inlet tube 40, throttle valve 14, and pressure
and outlet rate of the fuel within the inlet tube 40.
[0071] Acceleration enrichment is not normally required with the invention. In a conventional
carburetor, fuel is kept in a float reservoir at some distance from the fuel outlet,
and thus some finite period of time is required when additional fuel flow is needed.
In the present invention, additional fuel flow capability is always present at the
outlet 62.
[0072] With the exception of the embodiment of Figure 17, the invention can be used at any
attitude orientation, and also with the exception of the embodiment of Figure 17 can
be used in any condition of horizontal or vertical acceleration Conventional carburetors
having a float system for fuel metering require a substantially consistant orientation
to prevent fuel starvation or flooding in the carburetor.
[0073] Although the invention has been disclosed in the environment of a carburetor, it
should be evident that the novel fluid mixing and metering characteristics of the
invention may be employed ',in other applications requiring precise control of the
mixing the two fluids, either one of which may be liquid or gas.
1. A fluid mixing device comprising: a fluid passageway for a first fluid, an adjustable
throttle valve which has a throttle aperture which is so arranged in relation to the
passageway so as to form in the passageway a throttle opening of controllable cross-sectional
dimension, and a fluid metering system means for supplying a second fluid to the passageway
through a distribution outlet which extends across the passageway and the effective
length of which is determined by the cross-sectional dimension of the throttle opening,
and means for altering the proportionate flow of the second fluid through the distribution
outlet in relation to the flow of the first fluid in the passageway.
2. A mixing device according to claim 1 in which said fluid supply includes a normally
axially stationary metering tube extending across said throttle opening.
3. A mixing device according to claim 2 in which said distribution outlet is located
in said metering tube across said throttle opening.
4. A mixing device according to claim 3 in which said distribution outlet comprises
a plurality of apertures spaced axially along at least one side of said metering tube.
5. A mixing device according to claim 3 in which said distribution outlet comprises
at least one axial slot along one side of said metering tube.
6. A mixing device according to claim 2 in which said metering tube is positioned
in registration with said throttle valve and extends through a complementary longitudinal
aperture in said throttle valve, and said throttle valve is slidable upon said metering
tube to adjust the throttle opening and change the effective length of said distribution
outlet.
-7. A mixing device according to claim 2 including means to adjust the axial location
of said metering tube.
8. A mixing device according to claim 7 in which said throttle valve is adjustable
between limits to provide a maximum throttle opening and a minimum throttle opening,
and further including means to alter said minimum throttle opening.
9. A mixing device according to claim 1 in which said supply means comprises a normally
axially stationary metering tube having said distribution outlet extending along at
least one side thereof, and said means to alter comprises means to rotate said metering
tube about its longitudinal axis to change the circumferential location of said distribution
outlet.
10. A mixing device according to claim 1 in which said supply means comprises a fixed
metering tube having said distribution outlet extending along one side thereof, and
said means to alter comprises a pressure detecting tube in communication with said
first fluid, said detecting tube including means to sense a pressure of said first
fluid, and said means to alter further including means to control the pressure of
said second fluid at said sensed pressure of said first fluid.
11. A mixing device according to claim 10 in which said means to sense comprises an
inlet in one side of said detecting tube, said detecting tube being rotatable to change
the circumferential location of said inlet and thereby change the sensed pressure
of said first fluid.
12. A mixing device according to claim 10 in which said means to control comprises
a balancing regulator regulated by said sensed pressure, said balancing regulator
having an inlet for said second fluid, and including a fluid control responsive to
said sensed pressure and operable to permit flow of said second fluid through said
second fluid inlet at such a rate so as to cause equality of pressure between the
second fluid and the sensed pressure.
13. A mixing device according to claim 1 in which said means to alter comprises a
first pressure transmitting tube having one end extending into said first fluid oriented
so as to detect the total pressure thereof and a second pressure transmitting tube
having one end extending into said first fluid at said first fluid passageway oriented
so as to detect the static pressure thereof, said tubes being joined at their other
ends and having a third pressure transmitting tube leading therefrom, said second
pressure transmitting tube having valve means therein operable to permit a portion
of the total pressure in said first pressure transmitting tube to bleed into said
second pressure transmitting tube leaving a resultant differential pressure in said
third pressure transmitting tube, and said means to alter further including means
to control the pressure of said second fluid at said differential pressure.
14. A mixing device according to claim 13 in which said means to control comprises
a balancing regulator regulated by said differential pressure, said balancing regulator
having an inlet for said second fluid, and including a fluid control responsive to
said differential pressure and operable to permit flow of said second fluid through
said second fluid inlet at such a rate so as to maintain equality of pressure between
said second fluid and said differential pressure.
15. A mixing device according to claim 1 including a source of said second fluid maintained
at a pressure at least as great as the total pressure of said first fluid, and further
including means to control the pressure of said second fluid in said fluid supply
at a pressure approximately equal to the total pressure of said first fluid.
16. A mixing device according to claim 15 in which said means to control comprises
a balancing regulator having an inlet for said second fluid from said source, and
including a fluid control operable to permit flow of said second fluid through said
second fluid inlet at such a rate so as to maintain equality of pressure between said
second fluid and the.total pressure of said first fluid.
17. In a carburetor having an air passageway, a movable throttle valve having a throttle
aperture which is so . arranged in the air passageway so as to form a throttle opening
of controllable cross-sectional dimension, a fuel source for supplying fuel to the
air passageway for mixture with air passing therethrough, and a fuel metering system
having
a. a normally axially stationary fuel metering tube connected to said fuel source
and extending across said air passageway, said metering tube being positioned in registration
with said throttle valve and extending through a complementary lateral aperture in
said throttle valve such that said throttle valve is slidable upon said metering tube
with said metering tube extending across the throttle aperture,
b. a longitudinal fuel distribution outlet in said metering tube extending substantially
across the width of said air passageway, and
c. means to rotate said metering tube about its longitudinal axis to change the circumferential
location of said fuel distribution outlet and thereby alter the flow of fuel through
said fuel distribution outlet.