WO1996029510A1

WO1996029510A1 - Method for supplying fuel to a combustion engine, and combustion engine

Info

Publication number: WO1996029510A1
Application number: PCT/NL1996/000118
Authority: WO
Inventors: Frederikus Hendrikus Gerardus Uytdewilligen; Raymond Wentink
Original assignee: Tumic Research Limited
Priority date: 1995-03-20
Filing date: 1996-03-20
Publication date: 1996-09-26
Also published as: US5934230A; EP0839270A1; AU5124996A

Abstract

The invention relates to a method for supplying fuel to a combustion engine (1) which has an air inlet (6) provided with a gas valve and an output shaft (4) and wherein a fuel line (13) in which a fuel supply device is arranged debouches into the air inlet (6). The method comprises of providing a pump (10) with an adjustable, substantially continuous flow rate for the fuel supply device, determining the position of the gas valve, determining the rotation speed of the shaft (4), ascertaining herewith the required fuel flow rate and adjusting the pump (10) accordingly. The invention further relates to a combustion engine (1) of which the fuel supply is controlled as according to the above specified method.

Description

METHOD FOR SUPPLYING FUEL TO A COMBUSTION ENGINE, AND COMBUSTION ENGINE

The invention relates to a method for supplying fuel to a combustion engine which has an air inlet provided with a gas valve and an output shaft and wherein a fuel line in which a fuel supply device is arranged debouches into the air inlet.

The invention relates more particularly to a method in which the fuel supply device is of the injection type. It is known to use the pressure in the inlet conduit as control parameter to regulate the quantity of fuel for injection. In that case a sensor is used which generates a control signal proportional to the inlet pressure. Another known control is based on measuring the quantity of air flowing through the air inlet.

Both known control systems have a considerable time constant due to the delay of the necessary sensors.

The invention now has for its object to provide a method for supplying fuel which enables very rapid control such that this is suitable for fast-running engines, such as two-stroke racing engines which can have a rotation speed of up to 18,000 rpm.

This object is achieved with the method according to the invention by providing for the fuel supply device a pump with an adjustable, substantially continuous flow rate, determining the position of the gas valve, determining the rotation speed of the shaft, ascertaining herewith the required fuel flow rate and adjusting the pump accordingly. Both the gas valve position and the rotation speed can be determined with a very small time constant. The required fuel flow rate can be calculated for instance with a suitable algorithm. Preferably however, the method of claim 2 is applied. A high processing speed can be hereby achieved. The matrix can be configured by calculation. The method of claim 3 is preferably applied however. It is of course also possible herein to use a self-learning method, wherein the values stored in the matrix are gradually optimized during operation of the engine on the basis of simultaneously performed measurements with the said lambda probe.

A further refinement of the method according to the invention is achieved with the steps of claim 4. As for instance the air pressure, air temperature and air humidity vary, modified fuel flow rates can be provided so that a desired optimum operation is obtained under all operating conditions.

The step of claim 5 is preferably applied particularly in the case of fast-running engines such as racing engines. Due to the "predictive" control a time constant for the control practically equal to zero can be realized. The combustion engine will thus herein obtain the optimum fuel supply at virtually any given moment, both during constant and greatly varying operating conditions.

The invention likewise relates to and provides a combustion engine as characterized in claim 6.

The step of claim 7 is preferably applied therein.

In the fully open position of the gas valve the intake air passes through the valve completely unimpeded, so that the cylinder can be filled with a maximum fuel/air mixture. During partial load the transverse channel of the valve body lies at an angle to the channel of the air inlet wherein edges of the valve body protrude in the channel of the air inlet. This results in very strong vortices which ensure good mixing of the injected fuel with the through-flowing air. This is of particular importance in the present invention because the fuel is continuously injected, while at lower rotation speeds the intake air flow has a pulsating component and the air speed is therein lower. Due to the specific embodiment of the gas valve very good mixing of the injected fuel with the combustion air is also achieved under these conditions.

The pump is preferably a gear pump. This provides a very uniform output which is proportional to the rotation speed. A suitable driving of the engine can be achieved with the step of claim 10. The direct current electric motor can be controlled very precisely with per se known electronic control units.

A further development of the invention is characterized in claim 11. Because the gas valve is not directly moved by the hand or foot-operated control member, it is possible through the control means to realize at all times an optimum adjustment of the gas valve for the momentary air flow and the momentary fuel flow rate and thus an optimal mixing of the fuel with the air. When full power is demanded from zero load and the control member is moved into the fully open position, a poor mixing of the fuel and air would occur in the case of a direct coupling because of the initially still low air speed.

The invention is further elucidated with reference to the annexed figures.

Figure 1 shows schematically in partial section a combustion engine with a fuel supply embodied according to the method of the invention.

Figure 2 shows a sectional detail as according to arrow II in figure 1.

The engine 1 shown in figure 1 is of the two-stroke type. This engine 1 comprises a cylinder 2 in which a reciprocating piston 3 is arranged. The piston 3 drives via a connecting rod 5 the crankshaft 4 mounted in the engine block. The engine further comprises an air inlet 6 into which debouch fuel supply means to be described further.

Since the engine, as stated, is of the two-stroke type, the fuel/air mixture drawn in from the air inlet is sucked into the crankcase 9 of engine 1 during the upward stroke of piston 3. At the end of the downward operating stroke of piston 3 the latter leaves clear the flushing channel 8 whereby the entrained fuel/air mixture from crankcase 9 can enter cylinder 2 via flushing channel 8. In the subsequent upward stroke of piston 3 the mixture is compressed and ignited, whereafter a downward operating stroke of piston 3 occurs once again. Close to the end of the downward stroke of piston 3 the outlet 7 is left clear whereby combustion gas can escape via this outlet 7. Immediately thereafter the top part of piston 3 again passes over the washing channel 8 whereby fresh mixture is supplied and the cycle is repeated.

For the supply of the fuel in the air 15 a pump 10 is applied according to the invention which has an adjustable, substantially continuous flow rate. The fuel is thus not injected in pulsating manner in accordance with the movements of the piston but in one continuous jet.

The pump 10 is arranged in a fuel line 13 which leads from a fuel tank 12 to a vaporizer 14 debouching into the air inlet 6.

As shown more particularly in figure 2 , the gas valve in the shown preferred embodiment is embodied as a valve body 17 with a revolution surface. The axis of symmetry of valve body 17 defines an axis which intersects the channel 20 of the air inlet and around which valve body 17 is rotatable. The valve body 17 has a transverse channel 21 which, in the fully open position of the valve, forms one continuous whole with channel 20, so that the air 15 can pass through the valve without any obstruction. In the partially open position as shown in figure 2, edges of the valve body 17 protrude into channel 20 whereby the entrain air 15 is set into strong vortices. The fuel injected by the vaporizer 14 is well mixed with the air due to these vortices, so that it can vaporize well and form a uniform mixture with the air.

In this preferred embodiment the pump 10 is driven by a direct current electric motor which is controlled by the control device 22 via a control line 28.

The control device 22 generates via control line 28 a control signal to the motor 11 which depends on a number of parameters, in particular the position of the gas valve 17 and the rotation speed of the shaft 4 of the engine.

The position of the gas valve is determined with sensor 16 and supplied to the control device 22 via control line 24. The rotation speed of shaft 4 is determined with sensor 23 and supplied to the control device 22 via signal line 25.

Instead of determining the rotation speed using a separate sensor 23 a determination of the rotation speed co-acting with the ignition signal can of course also be used.

In the embodiment shown here, in addition to determination of the rotation speed and determination of the gas valve position, a further determination of several parameters of the air 15 is applied. A sensor 16 for this purpose is connected via a signal line 27 to the control device 22. The quantities for determining with sensor 26 comprise for instance the absolute pressure of the air 15 and the temperature and humidity thereof.

The control device 22 comprises a central processing unit which processes the signals supplied via the lines 24, 25 and 27 and on the basis thereof generates the control signal to be supplied to the motor 11, so that an optimum fuel supply associated with the measured values is generated. Generating of the control signal preferably takes place in that the control device 22 comprises a memory member in which a matrix of gas valve positions, shaft rotation speeds and associated fuel flow rates is stored. The processing unit can thus determine very rapidly on the basis of the matrix which fuel flow rate is associated with the measured gas valve position and the measured rotation speed and control the motor 11 accordingly. The signal from sensor 26 can herein be used as correction signal with which the determined value is adjusted in the one or other direction.

The gas valve 17 is preferably controlled by a control motor (not shown) which is regulated by the control device 22 in accordance with the shaft rotation speed, the gas valve position and the position of a hand or foot-operated control member (not shown) . Thus can be prevented that due to too rapid an operation of the gas valve 17 an incomplete mixing of the fuel with the combustion air 15 occurs, as noted above.

It is noted that the invention is not limited to use in a one cylinder two-stroke engine as depicted in figure 1. It is however the case that in a high-speed two-stroke engine the intake air flow is practically continuous, and thus includes little or no pulse component, so that the conditions for mixing of this air with the continuously supplied fuel is optimal. However, with a sufficient volume of the air inlet conduit or when different cylinders operating out-of-phase are connected to the same air inlet, suitable air flow conditions will also occur wherein the invention can be effectively applied.

Claims

1. Method for supplying fuel to a combustion engine which has an air inlet provided with a gas valve and an output shaft and wherein a fuel line in which a fuel supply device is arranged debouches into the air inlet, comprising of providing a pump with an adjustable, substantially continuous flow rate for the fuel supply device, determining the position of the gas valve, determining the rotation speed of the shaft, ascertaining herewith the required fuel flow rate and adjusting the pump accordingly.

2. Method as claimed in claim 1, wherein the required fuel flow rate is determined on the basis of a pre-configured matrix in which various gas valve positions and shaft rotation speeds are related to an associated fuel flow rate suitable for a desired operating mode of the engine.

3. Method as claimed in claim 2, wherein the matrix is at least partially configured by including therein values wherein the oxygen content of exhaust gases determined with a lambda probe arranged in an outlet of the engine has an optimal value.

4. Method as claimed in claim 1 or 2, wherein at least one parameter, such as the absolute pressure of air flowing through the air inlet, is determined and the determined fuel flow rate is corrected accordingly.

5. Method as claimed in any of the foregoing claims, wherein the speed of change in at least the shaft rotation speed is determined and the pump is adjusted such that it generates a fuel flow rate corresponding with a shaft rotation speed such as will prevail, based on the speed of change, for a predetermined time duration.

6. Combustion engine comprising at least one cylinder, a reciprocally moveable piston therein which can drive an output shaft via a transmission, an air inlet which is connected to the cylinder and in which is arranged a gas valve, fuel supply means debouching into the air inlet and comprising a pump with an adjustable, substantially continuous flow rate, control means for controlling the pump, sensors connected to the control means for at least the shaft rotation speed and the gas valve position, wherein the control means are programmed such that they control the pump in the manner as claimed in any of the foregoing claims.

7. Combustion engine as claimed in claim 6, wherein the air inlet comprises a channel of a determined section and the gas valve comprises a valve body with a revolution surface rotatable in accordance with an axis intersecting the channel, which valve body is provided with a transverse channel which in an open position of the gas valve forms one continuous whole with the channel and wherein the fuel supply means comprise a vaporizer debouching into the transverse channel.

8. Combustion engine as claimed in claim 6 or 7, being a two-stroke engine.

9. Combustion engine as claimed in any of the claims 5-8, wherein the pump is a gear pump.

10. Combustion engine as claimed in any of the claims 5-9, wherein the pump comprises a direct current electric motor.

11. Combustion engine as claimed in any of the claims 5-10, wherein the gas valve is moved by a control motor which is regulated by the control device in accordance with the shaft rotation speed, the gas valve position and the position of a hand or foot-operated control member.