METHOD AND APPARATUS FOR DOSING A GASEOUS FUEL

Abstract: A method for supplying a gaseous fuel (4) to a combustion engine (3) is described, wherein a required fuel flow is calculated, an actual fuel flow is measured, and a fuel flow control signal is adapted if a difference between the required and actual fuel flow is detected. Te fuel flow may be measured using a differential pressure measurement. The fuel flow control signal and associated actual fuel flow may be stored in a continuously updated memory. The invention also provides apparatus for carrying out this method, comprising a pulse width modulation valve (9) arranged in a fuel line (7), fuel flow measurement means (45, 50) arranged downstream of the valve (9), and means for generating a control signal for the valve (9). The control signal generating means are supplied with feedback from the flow measurement means (45, 50) and comprise a continuously updated table (52) for storing control signals and associated fuel flows.

Description: METHOD AND APPARATUS FOR DOSING A GASEOUS FUEL The invention relates to a method for dosed supply to a combustion engine of a fuel which is gaseous in ambient conditions, by determining the rotation speed and the load of the engine, calculating a fuel flow per unit of time required at the determined rotation speed and the determined load, converting the required fuel flow per unit of time into a control signal for opening and/or closing a fuel valve arranged between a fuel container and the engine, and transmitting the control signal to the valve. Such a method is known, for instance from the US Patent No. 5,150,685. In the known method the starting point is a com¬ bustion engine provided with an electronically controlled petrol injection system. An injection signal for the petrol injectors is herein calculated by the electronic control on the basis of measured values of a number of operating para¬ meters of the engine such as rotation speed, accelerator pedal position and quality of the exhaust gases. This petrol injection signal is then read and converted to an injection signal for an LPG injector by correcting the petrol injecti- on signal for the differences in the desired mixture ratio between petrol and LPG. The LPG injection signal is finally fed to an LPG injector of the pulse width modulation type which opens and closes with an opening duration and frequen¬ cy controlled by the injection signal. The LPG flow dosed by the valve is in principle directly proportional to the frequency and the length of the pulse actuating opening of the valve. In practice this known method is found neverthe¬ less to have a number of drawbacks. The quantity of LPG flowing through the valve as a function of the opening duration and frequency does not for instance show any linear relation, while this relation can moreover differ from valve to valve as a result of unavoidable tolerances in the manufacture of the valves. Variations also occur during use of the valve as a result of wear. The consequence is that the known method results in practice in an unsatisfac¬ tory and non-reproducible dosaging behaviour. The invention therefore has for its object to pro¬ vide a method of the described type, wherein the above mentioned drawbacks do not occur. This is achieved according to the invention in that the fuel flow per unit of time flowing through the valve is detected, the detected flow is compared to the required fuel flow and the control signal for the valve is adapted on the basis of a difference be- tween the required and the detected fuel flow. Through feedback of the actually dosed fuel flow irregularities in the dosing behaviour of the valve and errors in the actuati¬ on thereof can be corrected simply and quickly. Preferably applied variants of the method accor- ding to the invention are described in the dependent claims 2-6. The invention also relates to an apparatus for performing the above described dosing method. Such an appa¬ ratus is characterized according to the invention by a container for the fuel, at least one fuel supply line con¬ necting the container to the engine, controllable means arranged in the supply line for dosing the fuel, means connected for signal generation to the fuel dosing means for calculating a desired fuel flow for dosage per unit of time, means connected in flow direction beyond the fuel dosing means to the fuel supply line for detecting the actually dosed fuel flow per unit of time, and feedback means connec¬ ting the detecting means to the dosing means. Due to the presence of the feedback means connected to the dosing means a rapid and precise response of the engine to pressing down of the accelerator pedal can be ensured under all conditi¬ ons. Preferred embodiments of the dosing apparatus ac¬ cording to the invention form the subject-matter of the dependent claims 9-15. The invention is now elucidated in the light of a number of embodiments, wherein reference is made to the annexed drawing in which corresponding components are desig¬ nated with the same reference numerals, and in which: fig. 1 shows a partly cut away, schematic view of a combustion engine with a petrol injection system and an injection system for fuel which is gaseous under ambient conditions; fig. 2 shows a schematic diagram of the dosing system with feedback according to the invention; fig. 3 is a diagram showing the relation between the actuation and flow-through of a pulse width modulation valve; fig. 4 shows a preferably applied actuating pulse for operating the first dosing valve of the injection device according to the invention; fig. 5 shows a schematic view of a circuit for generating the actuating pulse shown in fig. 4; fig. 6 is a diagram showing the idealized and actual relation between the opening duration of a pulse width modulation valve and the fuel quantity per unit of time flowing therethrough; fig. 7 is a partly sectional schematic view of a multipoint injection system; fig. 8 shows a section of a one-way valve used in the system of fig. 7; and fig. 9 shows a view corresponding with fig. 7 of an alternative multipoint injection system. An apparatus 1 (fig. 1) for dosed supply to a com¬ bustion engine 3 provided with an electronic control system 2 of a quantity of fuel 4 that is vaporous in ambient condi- tions is provided with at least one injection nozzle 6 arranged in an air intake channel 5 of the engine 3. The injection nozzle 6 is connected over a supply line 7 to a fuel container 8 in which the fuel 4 is stored under a pressure such that it is in liquid state. Incorporated in the supply line 7 are dosing means 9 which are connected over a first control line 21 to the control system 2 and controllable thereby. Also incorporated in supply line 7 is a closing valve 23 which is connected over a second control line 22 to the engine control system 2 and controllable thereby. Finally, detecting and feedback means 11 connected to the control system 2 are arranged in the supply line 7. The air intake channel 5 connects an air intake aperture 24 to at least one cylinder 25. Arranged in usual manner in intake channel 5 is a rotatable throttle valve 26 which is connected to the accelerator pedal or throttle and which regulates the feed of combustion air to cylinder 25. In the embodiment shown the combustion engine 3 is a conven- tional four-stroke Otto engine with one or more cylinders 25 in which moves in each case a piston 27 arranged on a crank¬ shaft (not shown) , with inlet and outlet valves 29 respecti¬ vely 30 actuable by camshafts 28. In a combustion chamber 31 formed by piston 27 and cylinder 25 is arranged a sparking plug 32 which is connected to a distributor 33. Gases burnt in the combustion chamber 31 leave engine 3 through an outlet channel 34 in which is arranged a so-called lambda sensor 35. The operating temperature of engine 3 is control¬ led by means of a cooling system in which a cooling liquid 36 is circulated by a pump 37 and generates the absorbed heat in a radiator 38. The engine 3 is further provided with an injection device 17 for a fuel such as petrol which is liquid in ambient conditions. This device 17 is provided with one or more injection nozzles 18 debouching into the air channel 5 in the vicinity of the inlet valve 29. The petrol injection device 17 is connected over a third control line 39 to a separate electronic control system (not shown) and is con¬ trollable thereby. In order to control the LPG injection the system 2 makes use of different input signals. For this purpose the engine control system 2 is connected over a first input line 40 to the distributor 33 which generates a signal correspon¬ ding to the rotation speed of the engine and is connected over a second input line 41 to a cooling liquid temperature sensor 42. The control system 2 is also connected over a third input line 43 to the lambda sensor 35. In addition the control system 2 can be further connected to sensors (not shown) which measure the position of the throttle valve 26, the quantity (mass or volume) of air supplied through intake channel 5 and the temperature of the air. The gas injection device 1 comprises means 10 ar- ranged between the injection nozzle and the fuel container 8 for causing evaporation of the fuel 4. The evaporating means 10 comprise in usual manner a housing 44 in which two cham¬ bers 12,14 separated by a diaphragm 13 are formed. The chamber 12 forms the actual evaporating chamber, while chamber 14 is a reference pressure chamber which is connec¬ ted over a conduit 56 to the part of the fuel supply 7 located downstream of the dosing means. The temperature of the evaporator 10 is controlled by a conduit system arranged in the wall of the evaporator housing 44 and connected to the engine cooling system. The supply of evaporated fuel to the injector 6 is regulated by the dosing means 9 under the control of the engine control system 2. The quantity of fuel to be supplied per unit of time depends inter alia on the engine load, the supplied air mass, the engine rotation speed, the engine temperature and the pressure and temperature of the fuel. These parameters are all measured and fed to the engine control system 2 which calculates therefrom a control signal for the dosing means 9. The gas dosing means 9 take the form of a so- called pulse width modulation valve. In such a valve a closing member is continuously moved reciprocally between an end position in which it leaves a passage fully open and an end position in which it fully closes the passage. The closing member has no intermediate position. The valve is actuated by a pulse-shaped energizing signal, wherein "high" and "low" of the pulse-shaped signal correspond with the two end positions of the closing member. In contrast to a pro¬ portional valve where the volume flow through the valve depends on the extent to which a passage is opened, the volume flow in a pulse width modulation valve depends on the time that the passage is fully opened, thus, in the case of a valve which is closed in non-energized state, on the time the control signal is "high" and the valve energized. If the pulse frequency is high enough, a pulse width modulation valve provides over a determined period the same flow pat¬ tern 68 as a proportional valve (fig. 3). In the injection device according to the invention the control signal generated by the control system 2 has a frequency having a fixed relation to the rotation speed of the engine 3. Because the pulse duration can be controlled very precisely by means of a suitably chosen circuit, an accurate dosing of the vaporous fuel is achieved. At a frequency of 50 Hz (which corresponds with a rotation speed of 3,000 r.p.m.) the gas injection signal can for instance be varied in 40,000 steps from "high" over the whole pulse period (valve fully open) to "low" over the whole pulse period (valve fully closed) . As the engine rotation speed increases the pulse period decreases, whereby the number of possible control steps also decreases, but within the engine speed range used in practice the accuracy of control is always amply sufficient. In order to limit the power consumption and heat generation during actuation of the pulse width modulation valve 9, use can be made for controlling the valves of a pulse-shaped control signal 20 which rapidly reaches a peak value 69 (fig. 4) and subsequently falls back to a lower level 70, wherein the closing member is however still held in its end position leaving open the aperture. The pulse front 71 must preferably run as straight as possible in order to ensure as linear a movement of the closing member as possible. For this purpose the pulse front can be made slightly flatter relative to the normal, logarithmic, curved path designated in dashed lines with 72 by precise adjust¬ ment of the actuating current. Such a pulse shape can be obtained from the block-shaped control signal 20 shown in fig. 3 by means of the circuit 73 shown in fig. 5. The line of the dosed quantity of fuel per unit of time shown in fig. 3 as a function of the pulse width and frequency assumes a linear relation between the quantity of fuel dosed each time the valve 9 is opened and the duration of opening (fig. 6) . As a result inter alia of mass inertia effects of the moving parts of the valve 9, the tolerances during the process of manufacturing the valve and the wear thereof during its lifetime, the actual relation between the opening duration of the valve and the quantity of fuel flowing therethrough each time it is opened will be approxi¬ mated rather by the curve 60, the line of which will vary from valve to valve and which can moreover vary for one particular valve during its lifetime. Because of this irre- gular line of the curve 60 a separate program would have to be written for actuation of each dosing valve 9 which would in addition have to be repeatedly adapted during the lifeti¬ me of the valve 9. In order to prevent this, feedback means 16 (fig. 2) are included in the dosing system according to the present invention. The feedback means 16 are connected to detecting means 11 arranged in the fuel supply line 7. The detecting means 11 comprise a pressure sensor 45 and a temperature sensor 50. Pressure sensor 45 is a so-called differential pressure sensor which determines the pressure difference between a pressure measurement hole 46 located in front of a throttle and a pressure hole 47 located behind the throttle. At each fuel pulse dosed by the valve 9 this pressure difference reaches in each case a maximum value which is recorded and sampled in a block 48. The sampled differential pressure values are transmitted further to a block 49 where they are corrected on the basis of a tempera¬ ture measured by sensor 50 and subsequently integrated in order to thus determine an equivalent value of the actually dosed fuel flow per unit of time converted to standard conditions. Because the valve 9 doses the fuel 4 in pulses and, also in the case of small dosed fuel flows, the maximum pressure difference thus occurs in the line (and thus the maximum flow speed of the fuel) , albeit for a shorter time than with greater fuel flows, the differential pressure measurement can also provide in the case of small fuel flows a very accurate determination of the actual dosed quantity of fuel per unit of time. The detected quantity of fuel per unit of time is stored together with the associated value for the time the valve 9 is opened (the control signal supplied to the valve 9) in a table 52, wherein the preceding value of the fuel flow detected at this opening duration is overwritten. The table 52 thus always contains the last known relation be¬ tween the opening duration of valve 9 and the quantity of fuel dosed per unit of time. The control system 2 can hereby always directly retrieve from this table 52 the opening duration associated with a demanded fuel flow. The control system 2 further comprises means for calculating the requi¬ red fuel flow from the measured engine parameters. These calculating means are connected over a signal line 53 to a block 54 in which the quantity of fuel required per unit of time is converted to a control signal which represents the required opening duration of valve 9. For this purpose the block 54 is connected to table 52. In addition the control signal for the required fuel flow 55 is compared in the block 54 with the signal of the detected fuel flow 53 and on the basis thereof a corrected control signal is generated which is fed via line 57 to a block 15, where it is conver¬ ted into a current which is transmitted via a line 58 to the pulse width modulation valve 9. For engines with a plurality of cylinders use can be made of multipoint injection, for which purpose the fuel supply line 7 can debouch downstream of the dosing valve 9 in a distributor block 61 where the air-fuel flow is divided into a number of parts which correspond with the number of cylinders 25 and which are guided through separate feed conduits 67 to the cylinders. The distributor block 61 comprises an upper part 62 with central aperture 66 into which debouches the main fuel line 7, a lower part 63 which is in gastight connection to the upper part 62 and onto which the separate conduits 67 are connected, and a middle part 64 with a flow distribution housing 65 arranged the¬ rein. In order to prevent the danger of so-called "backfire" (burning of the fuel-air mixture in the intake and/or the fuel supply line) , a non-return or one-way valve 75 is arranged in each conduit 67. This non-return valve 75 (fig. 8) comprises a lower housing 76 and an upper housing 77. The lower housing 76 defines a chamber 78 and the upper housing 77 defines a chamber 79 which is connected to the environment via an opening 80 in the upper housing 77. Further arranged in lower housing 76 is a connecting channel 82 which extends over practically the whole height of lower housing 76 and in which is fixed an outlet nipple 81. The opening of the channel 82 debouching into the space 78 is closed by a diaphragm 83 arranged between lower housing 76 and upper housing 77. As long as the pressure in the vicinity of the non-return valve 75 which also prevails, through opening 80, in the chamber 79 of the upper part 77, is greater than the pressure in the fuel supply line 67, the channel 82 remains closed, whereby the danger of backfire is prevented. In an alternative embodiment of a multipoint injection a pulse width modulation valve 9 is arranged in each separate fuel line (fig. 9) . This embodiment is more expensive but also more accurate. Although the injection system according to the invention is described above as LPG injection system, it is equally suitable for other fuels, for instance natural gas, which are vaporous under ambient conditions. For this purpo¬ se only the fuel container 8 and supply lines 7 as far as the evaporating means 10 have to be adapted to the pressure necessary to keep such a fuel liquid. When this pressure is very high, as is the case with natural gas (200 bar instead of the pressure of 8-10 bar required for LPG) , a pressure reducing valve can further be connected between the evapora¬ ting means 10 and the fuel container 8. Possible further adaptations relate only to the control program. The injecti¬ on system according to the invention therefore offers a greatly increased flexibility compared with conventional injection systems. Because the injection system according to the invention makes use of the fuel flow per unit of time as control quantity, the control program is in principle inde¬ pendent of the dosing valve 9 used, since the relation between the actually dosed fuel flow and the associated control signal will in any case always be present in table 52. *****

Claims: CLAIMS 1. Method for dosed supply to a combustion engine (3) of a fuel (4) which is gaseous in ambient conditions, by determining the rotation speed and the load of the engine (3) , calculating a fuel flow per unit of time required at the determined rotation speed and the determined load, converting the required fuel flow per unit of time into a control signal for opening and/or closing a fuel valve (9) arranged between a fuel container (8) and the engine, and transmitting the control signal to the valve (9) , characte- rized in that the fuel flow per unit of time flowing through the valve (9) is detected, the detected flow is compared to the required fuel flow and the control signal for the valve is adapted on the basis of a difference between the required and the detected fuel flow. 2. Method as claimed in claim 1, characterized in that the valve (9) is a digital valve and the fuel flow per unit of time through the valve is determined by the opening duration and frequency of the valve (9) . 3. Method as claimed in claim 2, characterized in that the fuel flow per unit of time through the valve (9) is detected by measuring a pressure difference in a line con¬ necting the fuel valve (9) and the engine (3) . 4. Method as claimed in claim 3, characterized in that the pressure difference is measured periodically and the measured values of the pressure difference are sampled and integrated. 5. Method as claimed in claim 3 or 4, characteri¬ zed in that a temperature is measured in the line (7) con¬ necting the fuel valve (9) and the engine (3) and the measu- red value of the pressure difference is converted on the basis of the measured temperature to a fuel flow under determined standard conditions. 6. Method as claimed in any of the foregoing claims, characterized in that the control signal for the valve (9) and the fuel flow per unit of time detected the¬ rein are stored collectively in each case in a table which can be overwritten and at a following calculation of the required fuel flow the control signal required for this purpose is read from the table. 7. Apparatus (1) for dosed supply to a combustion engine (3) of a fuel (4) which is gaseous in ambient condi- tions, evidently intended for performing of the method as claimed in any of the foregoing claims. 8. Apparatus (1) as claimed in claim 7, character¬ ized by a container (8) for the fuel, at least one fuel supply line (7) connecting the container (8) to the engine (3), controllable means (9) arranged in the supply line (7) for dosing the fuel, means (16) connected for signal genera¬ tion to the fuel dosing means (9) for calculating a desired fuel flow for dosage per unit of time, means (45,50) connec¬ ted in flow direction beyond the fuel dosing means (9) to the fuel supply line (7) for detecting the actually dosed fuel flow per unit of time, and feedback means (11) connec¬ ting the detecting means (45, 50) to the dosing means (9). 9. Apparatus (l) as claimed in claim 8, character¬ ized in that the dosing means (9) comprise at least one digital valve. 10. Apparatus (1) as claimed in claim 9, characte¬ rized in that the valve (9) is a pulse width modulation valve. 11. Apparatus (l) as claimed in claim 9 or 10, characterized in that the detecting means (45,50) comprise at least one differential pressure sensor (45) and integra¬ ting means (49) connected thereto. 12. Apparatus (l) as claimed in claim 11, charac¬ terized in that the detecting means (45,50) comprise a temperature sensor (50) connected to the integrating means (49). 13. Apparatus (1) as claimed in any of the claims 8-12, characterized in that the feedback means (11) comprise a table (52) which can be overwritten and which represents the relation between a control signal generated to the dosing means (9) and the detected fuel flow per unit of time. 14. Apparatus (1) as claimed in any of the claims 8-13, characterized in that the engine (3) comprises a plurality of cylinders (25) , a separate fuel supply conduit (67) is connected to each cylinder (25) and a dosing valve (9) is incorporated in each separate conduit (67) . 15. Apparatus (1) as claimed in any of the claims 8-13, characterized in that the engine (3) comprises a plurality of cylinders (25) , a separate fuel supply conduit (67) provided with a non-return valve (75) is connected to each cylinder (25) and the dosing means comprise a valve (9) arranged in a main fuel supply line (7) and a distributor block (61) placed downstream thereof and connected to the separate feed conduits (67) . *****

Inventors: BRINK ALFRED VAN DE, VAN DE BRINK, ALFRED
Applicants: AUTOGASTECHNIEK HOLLAND BV, BRINK ALFRED VAN DE, AUTOGASTECHNIEK HOLLAND B.V., VAN DE BRINK, ALFRED
Application year: 1995
Main classification: F02D41
IPC codes: F02D19