Method and Apparatus for Preparation and Control of an Air-Fuel Mixture

1. In a method for the preparation and control of an air-fuel mixture by fuel atomization using a high-velocity gas as an atomizing agent, said gas being at a pressure higher than ambient pressure and being present in an amount from a few percent to tens of percent of the air-fuel mixture supplied to the engine which continuously indues fuel, the amount of the induced fuel being proportional to the pressure of said gas, controlling said pressure at least by engine speed and load, so that the mixture ratio provides maximum effective pressure in the range of engine full loads, a minimum consumption of fuel and a minimun amount of toxic components in the exhaust gases in the range of engine partial loads, while concurrently continuously atomizing and homogenizing the fuel, introducing the mixture thus prepared into the engine air intake upstream of the throttle, mixing said mixture in the manifold with air induced by the engine for supplying the charge to the engine cylinders, and during coasting conditions when the braking effect of the engine is utilized and when the throttle is closed a negative pressure downstream of the throttle is utilized for cancelling the delivery of compressed gas to the multi-stage atomizer thereby interrupting the admission of fuel; said fuel being atomized and homogenized in multi-stage atomizer nozzles of fixed flow parameters, the atomization being effected by streams of gas under controlled pressure whereby induction of air and feed of fuel is effected simultaneously and under precise control conditions; during idling of the engine when the throttle is closed and when the demand for fuel is small and the degree of atomization is low the difference of pressure existing above and below the throttle is utilized to homogenize further the air-fuel mixture by causing the previously separated high-velocity streams of mixture to collide and expand; said multi-stage atomizer having stages in at least one of which said gas under controlled pressure is used for fuel atomization while in at least one other stage a gas of different parameters is used for additional fuel atomization; said throttle being formed with a symmetrical arrangement of throttle elements enabling substantially axial flow of mixture, the improvement wherein: said gas is compressed air supplied without significant pressure pulsations and in a volumetrical amount proportional to the mass characteristic of the charge induced by the engine as a function of the parameters of atmospheric air, speed of the engine and suitable recesses in a sliding surface of a displacement pump, dividing said compressed air into at least two streams in a definite ratio, one of said streams serving for supplying and sucking the amount of fuel as determined by said flow parameters to effect atomization of the fuel, the second of said streams being subjected to momentary- and constant-corrections of flow parameters serving for successive atomization and homogenization of the mixture, for the desired correction of discharge as well as for preventing secondary coagulation of atomized fuel, said streams of compressed air being correlated so that change of flow parameters in one stream produces an equivalent change of flow parameters in the other stream, the control of the flow parameters in said first stream from engine start through idling and partial loads up to full loads of the engine being dependent on negative pressure downstream of the throttle, whereas enrichment of the mixture at engine full load is achieved by mechanically opening the valve through the accelerator pedal, said momentary correction increasing the flow parameters in said first stream and enriching the mixture, said constant change of the flow parameters in the second stream serving for compensation of manufacturing tolerances and degree of wear of apparatus elements.

2. A method as claimed in claim 1, wherein the multiplied streams of compressed air used for control of the air-fuel ratio ensure automatic pressure corrections in the course of said control depending upon the varying atmospheric conditions.

3. A method as claimed in claim 2, wherein the flow ratio between the open nozzles of said multi-stage atomizer supplying the first and second stream is from 10:90 to 30:70.

4. A method as claimed in claim 2, wherein said pressure pulsation of compressed air is eliminated by automatically opening suitable recesses provided in the sliding surface of said displacement pump.

5. A method as claimed in claim 2, wherein pulsation of the negative pressure controlling the valve is eliminated by throttling the flow in a passage connecting a pneumatic actuator with the engine intake manifold.

6. A method as claimed in claim 2, wherein said compressed air used for supplying the fuel from the float chamber is introduced on the upstream side of a reduced portion of a passage connecting the valve with the side nozzles of the multi-stage atomizer.

7. In an apparatus for the preparation and and control of an air-fuel mixture provided with a multistage atomizer installed in an air intake manifold of an engine upstream of the throttle thereof, a float chamber containing fuel connected to said multi-stage atomizer, means including a passage for supplying said multi-stage atomizer with a gas at a pressure higher than ambient pressure, said multi-stage atomizer including a diffuser at the end thereof opening towards the engine air intake manifold above the throttle whereat the mixture of fuel and gas is mixed with air induced by the engine to produce a charge for the engine cylinders, means for controlling the parameters of the gas supplied through the passage to the apparatus and a valve installed in said passage for correction of the flow parameters of the gas supplied to the multi-stage atomizer, said valve being pneumatically coupled with the air intake manifold downstream of the throttle to respond to negative pressure and being mechanically linked with the accelerator pedal in series with the throttle, said throttle comprising symmetrically opening elements having a shape co-operatively corresponding to the shape of the cross-section of the air intake manifold, said elements together forming an idling atomizer including, in series, a nozzle situated coaxially with the stream of flowing mixture, a port coaxially situated under said nozzle, and a staged nozzle for expanding the mixture, said multi-stage atomizer including a mechanical element whose flow parameters are constant, the fuel being induced and simultaneously being delivered at a continuous regulated pressure to side nozzles of said multi-stage atomizer from the float chamber, said float chamber being connected through a further passage to the first said passage, wherein selected stages of said multi-stage atomizer are connected with the first said passage of said compressed gas, and other stages connected with the further passage through which a gas of other properties may be delivered, the improvement comprising: a source of said gas which is compressed air, said source including a displacement pump driven by the engine, said displacement pump having recessess in a sliding surface for obtaining volumetrical characteristics proportional to the mass characteristic of the charge induced to the engine and for preventing pressure pulsation, said displacement pump being connected through a passage directly to an apparatus where said passage is divided into at least two passages for the compressed air, said first passage including a valve, and after said valve said first passage having a reduced portion, said first passage being connected with the float chamber upstream of said reduced portion, said first passage being connected with side nozzles of the multi-stage atomizer downstream of said reduced portion, said valve in said first passage being operated by a pneumatic actuator, said pneumatic actuator being connected to the air intake manifold downstream of the throttle, said valve being operatively connected to the accelerator pedal in series with the throttle to be opened by said pedal, said second passage being connected to a central nozzle which communicates through ducts to a concentric slot nozzle, said second passage also being connected to ejection ports connected to the side nozzles near the outlets thereof, said multi-stage atomizer including rotatably shaped elements and seals dividing said first and second passages and means in said second passage for varying the cross-section of the central nozzle, the latter said means including a needle threadably and resiliently mounted and coupled to a control cable for facilitating start of a cold engine.

8. An apparatus as claimed in claim 7, wherein the multi-stage atomizer includes elements which are rotatably shaped.

9. An apparatus as claimed in claim 7, wherein said recesses in the cylindrical sliding surface of the displacement pump are directed towards the upstream side of the blades within an angular range and are inserted before the air inlet to the pump and between the air inlet and outlet.

10. An apparatus as claimed in claim 7, wherein the passage supplying said pneumatic actuator includes a portion for throttling the flow.

11. An apparatus as claimed in claim 7, wherein said float chamber is connected at one side to the source of fuel and at a second side to respective side nozzle for primary atomization of the multi-stage atomizer to supply multi-fuel mixture to the internal combustion engine, including fuels forming water emulsions or solutions.