Fuel conservation means for internal combustion engines and the like

A device adapted to be interposed between the usual carburetor and manifold of an internal combustion engine, or the like, for receiving the fuel-air mixture from the carburetor and discharging same into the manifold, said device comprising three components or stages: a rotor member, a sonic vibrator, and a heated grid means. The rotor member is mounted in the flow stream of the fuel-air mixture and is rotated by the air intake for causing oscillation of the fuel-air mixture from the carburetor. The fuel-air mixture then enters the sonic vibration stage which causes a molecular mixing of the fuel with the air. The mixed fuel-air is then passed through the heated grid or screen, which not only straightens out the path of the flow stream of the fuel-air mixture, but also promotes vaporization of the fuel-air mixture impinging the screen, and receiving the heat by radiation. A magnetic force field is possibly established in the area of the screen or grid which magnetically affects the molecular structure of the hydrocarbon content of the fuel-air mixture to provide a more efficient power conversion of the fuel-air mixture.

BACKGROUND OF THE INVENTION 
1. Field of the Invention 
This invention relates to improvements in fuel conservation means and more 
particularly, but not by way of limitation, to a device adapted to be 
interposed between a carburetor and manifold of an internal combustion 
engine, or the like, for increasing the conservation of the fuel. 
2. Description of the Prior Art 
In the usual internal combustion engine, or the like, the fuel-air mixture 
normally moves through the carburetor directly into the manifold and to 
the combustion chamber for burning. The fuel and air are normally admitted 
into the carburetor and directed simultaneously into the manifold, with 
certain air to fuel ratios being considered optimum for achieving an 
efficient burning of the fuel-air mixture. For example, fourteen parts air 
to one part fuel is considered to be an optimum air to fuel ratio. 
However, with the normal present day carburetor mechanism the air and fuel 
are usually not sufficiently mixed prior to discharge into the combustion 
chamber, thus resulting in an inefficient burning of the fuel. This causes 
waste of the fuel and usually causes the discharge of pollutants into the 
atmosphere through the engine exhaust system. With the current and ever 
increasing concern with the shortage of fuels, and dangers of air 
pollution, it is becoming urgent to reduce fuel waste and reduce the 
exhaust of pollutants into the atmosphere. 
SUMMARY OF THE INVENTION 
The present invention contemplates a device which is particularly designed 
and constructed for conserving fuel during the operation of an internal 
combustion engine, or the like. The novel device is adapted to be 
interposed between the discharge or outlet side of a carburetor and the 
inlet or intake side of a manifold for receiving the fuel-air flow stream 
therethrough. The fuel-air mixture from the carburetor initially comes 
into contact with a rotor means and the force of the flow stream causes 
the rotor to rotate for stirring the flow stream and agitating the 
fuel-air mixture. Sonic reed or fin means is operably connected with the 
rotor means for simultaneous rotation therewith, and as the flow stream 
passes around or through the area of the sonic blade or reed sonic 
vibrations are impressed on the flow stream for acting thereon. The flow 
stream is then directed through a heated screen or grid means, around 
which a magnetic force field is possibly established. The grid means 
serves to straighten out the flow path of the flow stream, and the 
magnetic force field affects the molecular structure of the fuel and air 
mixture, particularly the hydrocarbon components thereof, which apparently 
promotes a more efficient power conversion of the fuel and air mixture. Of 
course, it is preferable that the heating of the screen or grid means be 
of a low order to avoid any accidental flashing of the fuel-air mixture 
passing therethrough. In addition, it is preferable that the screen or 
grid means comprises a pair of substantially identical grid elements 
spaced apart and rotationally orientated with respect to each other for 
providing a grid pattern for passage of the flow stream therethrough with 
a minimum of air restriction, or to prevent any excessive air restriction.

DESCRIPTION OF THE PREFERRED EMBODIMENTS 
Referring to the drawings in detail, reference character 10 generally 
indicates a fuel conservation device for use with internal combustion 
engines (not shown) or the like, and comprises an outer housing 12 having 
a central passageway 14 extending longitudinally therethrough. Whereas the 
housing 12 may be of substantially any desired construction, as shown 
herein the housing 12 is sectional and comprises a first sleeve member 16 
having one open end 17 and outwardly extending oppositely disposed flanges 
18 and 18a provided at the opposite end thereof. A second sleeve 19 is 
secured in substantial axial alignment with the sleeve 16 by a collar 20 
and is provided with one open end 21 disposed in the proximity of the open 
end 17 and oppositely disposed outwardly extending flanges 22 and 22a at 
the opposite end thereof. The flanges 18-18a and 22-22a are provided with 
bores 24 and 26, respectively, with the bores 24 of the flanges 18-18a 
being substantially axially aligned with the bores 26 of the flanges 
22-22a for a purpose as will be hereinafter set forth. 
An annular shoulder 28 is provided on the inner periphery of the sleeve 16 
spaced from the open end 17 thereof for receiving a grid means 28 thereon. 
The grid means 28 is secured in position on the shoulder 28 by the collar 
20 in a manner as will be hereinafter set forth. A spider member or 
apertured disc 30 is disposed against the uppermost end of the collar 20 
as viewed in FIG. 1, and an annular shoulder 32 provided on the inner 
periphery of the sleeve 19 rests on the ring or disc 30 for retaining the 
ring in position against the collar 19. 
Whereas the collar 20 may be of substantially any well known construction 
for securing the sleeves 16 and 19 in end to end relationship, as shown 
herein substantially one-half the outer periphery of the collar 20 is 
tapered radially outwardly in a direction toward the longitudinal center 
thereof as shown at 34, and the remaining portion of the outer periphery 
of the collar 20 is tapered radially inwardly toward the end thereof as 
shown at 36 in FIG. 1. The inner periphery of the sleeve 16 between the 
shoulder 28 and the open end 17 thereof is preferably of a tapered 
configuration complementary to the tapered portion 34 of the collar 20 for 
snugly receiving the collar 20 thereagainst. In addition, the inner 
periphery of the sleeve 19 between the shoulder 30 and the open end 21 
thereof is preferably of a tapered configuration complementary to the 
tapered portion 36 of the collar 20 for snugly receiving the collar 20 
thereagainst. Of course, suitable bolts (not shown) may be inserted 
through the mutually aligned pairs of bores 24 and 26 for securing the 
sleeves 16 and 19 together and clamping the ring 36, collar 20 and grid 
means 28 therein. 
The spider or perforated plate 30 is provided with a central bore 38 for 
receiving a hub 40 therethrough. A rotor member or propeller 42 is 
suitably journalled in the hub 40 in any well known manner (not shown) and 
is provided with a shaft 44 which extends through and beyond the hub 40. A 
blade or read 46 is secured to the outer end of the shaft 44 in any 
suitable manner for rotation simultaneously with the rotor 42. The reed or 
blade 46 is preferably constructed from a suitable spring steel, 
preferably approximately five thousanths of an inch in thickness, but not 
limited thereto, and the plane of the ead 46 is preferably substantially 
perpendicular to the longitudinal axis of the shaft 44 whereby the reed 46 
is rotated in the plane of its own surface during rotation of the rotor 
42. In addition, a plurality of spaced apertures 48 (FIG. 3) are provided 
in the reed 46, said apertures preferably being of a diametric size 
corresponding to the usual number "80" drill bit, but not limited thereto. 
Of course, the reed 46 is installed or disposed downstream of the rotor 
42, as clearly shown in FIG. 1. and it is to be understood that the sonic 
reed 46 may be stationary, or retained against rotation, if desired. 
The grid means 28 preferably comprises a pair of substantially identical 
grid-type discs 50 preferably spaced slightly aprt by suitable spacer 
means (not shown) in order to preclude excessive restriction to the flow 
stream moving therethrough. Each disc 50 comprises an annular outer ring 
52 (FIG. 4) having a single strand of Ni-chrome wire 54 or the like of a 
suitable diametric size and following a back-and-forth pathway across the 
open central portion of the rings 52, with the loops or segments of the 
wire 54 at the turning points thereof being molded or otherwise secured to 
the ring 52. In addition, the portions of the wire 54 spanning the open 
central portion of the ring 52 are preferably substantially mutually 
parallel. The opposite ends of the wire 54 extend beyond the outer 
periphery of the rings 52 as clearly shown in FIG. 4, with one end 56 
emerging from one surface of the ring 52 and the opposite end 58 emerging 
from the opposite surface thereof. In the assembly of the grid means 28, 
one of the discs 50 is disposed in axial alignment with the other of the 
discs 50, but with a rotational orientation between the discs 50 such that 
the wires 54 of one disc are substantially perpendicularly disposed with 
respect to the wires 54 of the other disc. The ends of the wire 54 which 
emerge from the common sides or surfaces thereof, or the surfaces facing 
one another, are connected in any well known manner, and the connected 
ends and free ends are suitably connected with an electrical source (not 
shown), such as the electrical system of an automobile wherein the 
internal combustion engine (not shown) with which the device 10 is to be 
utilized is installed. Of course, it will be apparent that the opposite 
ends 56 and 58 of the connected discs 50 may be connected with the 
electrical source, and the common wires which are connected between the 
discs 50 will electrically connect the discs 50 in the circuit. 
It is to be understood that the grid 28 may be of an ultimate substantially 
unitary construction in that the rings 52 of the complementary discs 50 
may be cemented or otherwise secured together subsequent to the forming of 
the wires 54 therein whereby in essence the outer rings 52 form a single 
annular ring (not shown) having a pair of mutually perpendicularly 
arranged wire grid portions 54 in spaced relation in the central portion 
thereof. 
Whereas the housing 12 as shown herein is of a sectional construction, it 
is to be noted that the outer housing 12 may be of a unitary construction, 
having a central bore or passageway extending longitudinally therethrough 
wherein the rotor 42, sonic reed 46 and grid means 28 may be suitably 
installed. 
The device 10 as shown in FIGS. 1, 2 and 3 is particularly designed and 
constructed for use in combination with a single barrel carburetor (not 
shown) and may be installed between the discharge side of the carburetor 
and the intake side of the associated manifold (not shown). The device 10 
is installed in such a way that the rotor or propeller 42 is upstream from 
the grid means 28 with regard to the flow of the fuel-air mixture from the 
carburetor to the manifold. The carburetor and manifold function in the 
normal manner therefor, and as the fuel-air mixture is pulled into the 
manifold from the carburetor, the flow stream moves across the rotor 42, 
transmitting rotation thereto. The rotation of the rotor 42 stirs the flow 
stream for an agitation thereof, and as the flow stream continues to move 
across the sonic reed 46, sonic vibrations are impressed on the flow 
stream. The reed 46 may be either electrically or mechanically induced for 
impressing the sonic vibrations on the flow stream. 
The flow stream then moves across the grid means 28 wherein the path of 
travel of the stream is straightened and the fuel-air mixture is heated. 
The portion of the flow stream striking the heated wires 54 is 
substantially vaporized, and the remaining portion of the flow stream is 
heated by radiation. Possibly the flow stream is acted upon the magnetic 
force field surrounding he wires 54. This force field apparently acts on 
the molecular structure of the fuel-air mixture, particularly the 
hydrocarbon components thereof, which results in a more efficient power 
conservation of the fuel-air mixture than otherwise possible. 
Under test conditions the increased efficiency of fuel conservation with 
use of the device 10 has been found to be considerable. With Dynamometer 
testing the results showed an increase in mileage per gallon of 
approximately 53.59 per cent, and an increase of two in the engine horse 
power. In actual road testing, the mileage per gallon was increased by 
45.08 per cent. The advantages of such an increased efficiency are 
apparent. 
Referring now to FIGS. 5 and 6, a modified fuel conservation device 60 is 
shown which has been particularly designed and constructed for use in 
combination with a four barrel carburetor (not shown). The device 60 
comprises a plate 62 adapted for disposition over the intake opening 64 of 
a suitable manifold 66 and having a plurality of apertures 68 for 
alignment with similar apertures or bores (not shown) provided in the 
manifold 66 wherein the plate 62 may be secured to the manifold 66 by 
suitable bolts, or the like (not shown). Of course, it is preferable to 
interpose a suitable gasket 67 between the plate 62 and the manifold 66. 
Spaced bores 70, 72. 74 and 76 are provided in the plate 62 in substantial 
alignment with the usual bores 78 of the manifold 66. It is preferable to 
provide an opening 80 between the bores 70 and 76, and a similar opening 
82 between the bores 72 and 74, but not limited thereto. A fuel-air 
mixture handling element 84 is suspended within each manifold bore 78 from 
the plate 62 and since the elements 84 are substantially identical, only 
one will be set forth in detail herein. 
The element 84 comprises an annular support ring 86 suspended from the 
plate 62 by an arm 88. The arm 88 may be integral with the plate 62, or 
may be secured thereto in any suitable manner, as desired. In inwardly 
directed annular shoulder 90 is provided on the inner periphery of the 
ring 86 for receiving the grid means 28 thereagainst, and an annular 
groove 92 is provided in the inner periphery of the ring 86 spaced from 
the shoulder 90 for receiving a suitable snap ring or lock washer 94 
therein for retaining the grid means 28 securely in position against the 
shoulder 90. A hub member 96 is spaced from the ring 86 and supported in 
substantial axial alignment therewith by an arm 98 which is secured to or 
integral with the arm 88. A rotor 100 of any suitable type is journalled 
in the hub 96 in any well known manner for free rotation about its 
longitudinal axis, and is provided with a shaft 102 which extends through 
and beyond the hub 96 as particularly shown in FIG. 6. The sonic reed or 
blade 46 is secured to the outer extremity of the shaft 102 in any 
suitable manner for rotation simultaneously therewith. 
The fuel-air mixture is pulled into the manifold 66 from the carburetor 
(not shown) in the usual manner, and the rotors 100 of the elements 84 are 
disposed directly in the flow stream of the fuel-air mixture entering the 
manifold. The moving flow stream transmits rotation to the rotors 100, 
which stir the flow stream for an agitation thereof. The flow stream then 
enters the area surrounding the sonic reeds 46 which impress a sonic 
frequency on the flow stream. The fuel-air mixture then presses through 
the grids 28 which heat the flow stream and possibly magnetically affect 
the molecular structure of the fuel-air mixture while straightening out 
the flow path of the fuel-air mixture. The heated grid means 28 also 
substantially vaporizes the fuel-air mixture. The fuel-air mixture thus 
treated produces a greatly increased conservation efficiency as well as 
increased engine operating efficiency. 
It will be readily apparent that the invention may be utilized with 
substantially any type carburetor and manifold combination, from single 
barrel carburetors to multiple barrel carburetors, with great fuel 
conservation during operation of the associated engine, or the like. 
From the foregoing it will be apparent that the present invention provides 
a novel fuel conservation device comprising three essential and basic 
stages: a rotor stage wherein the fuel-air mixture flow stream is stirred 
for an agitation thereof, a sonic frequency stage wherein sonic frequency 
is impressed on the flow stream, and a heated grid stage wherein the flow 
stream is heated for a substantial vaporization thereof and possibly 
magnetically affected as well as the straightening of the flow path of the 
fuel-air mixture leaving the manifold. The novel device is simple and 
efficient in operation and economical and durable in construction. 
Whereas the present invention has been described in particular relation to 
the drawings attached hereto, it should be understood that other and 
further modifications, apart from those shown or suggested herein, may be 
made within the spirit and scope of this invention.